NASA

Technical

Paper

3287/REV1

February 2001

National Aeronautics and

Space Administration

Thermodynamic Data for

Fifty Reference Elements

Bonnie J. McBride

Glenn Research Center

Cleveland, Ohio

Sanford Gordon

Sanford Gordon and Associates

Cleveland, Ohio

Martin A. Reno

Heidelberg College

Tiffin, Ohio

Table of Contents

Summary ................................................................................................................................................................... 1

Introduction .............................................................................................................................................................. 1

Symbols .................................................................................................................................................................... 1

Standard States, Reference States, and Fundamental Constants .............................................................................. 2

Sources for Thermodynamic Functions .................................................................................................................... 2

Empirical Equations for Fitting the Thermodynamic Functions .............................................................................. 3

Assigned Enthalpy Values ........................................................................................................................................ 3

Heats of Formation and Equilibrium Constants ....................................................................................................... 3

Least-Squares Fit ...................................................................................................................................................... 4

Tables ....................................................................................................................................................................... '4

Concluding Remarks ................................................................................................................................................ 5

References ................................................................................................................................................................ 6

Table 1.--.S_ ml_,t,, l'hascs, Reference Codes, Temperature Ranges, References, and Notes ................................ 7

Table ll.--Thcrm,_l> namic Functions at 298.15 K .................................................................................................. 12

Table II1. I -- _clc, led Thermodynamic Functions for Ag(cr,_) .............................................................................. 14

Table 111.2 -- '_,t'lt'Lled Thermodynamic Functions for Al(cr,/?) ............................................................................... 15

Table !11.3 -- '_cl¢,tcd Thermodynamic Functions for Ar ....................................................................................... 16

Table III.4 --%clcctcd Thermodynamic Functions for B(13,_e) ................................................................................. 18

Table lli.5.--.";clcclcd Thermodynamic Functions for Ba(cr,t e) .............................................................................. 20

Table Ill.6._Sclectcd Thermodynamic Functions for Be(o_,/3,t e) ............................................................................ 22

Table IlI.7.--Selected Thermodynamic Functions for Br2(cr,f) ............................................................................. 24

Table III.8.--Selected Thermodynamic Functions for C(gr) ................................................................................... 26

Table III.9.--Selected Thermodynamic Functions for Ca(oc, fl, t_) ............................................................................ 28

Table III. 10.--Selected Thermodynamic Functions for Cd(cr,_) ............................................................................ 30

Table III. 1l.--Selected Thermodynamic Functions for C12 .................................................................................... 31

III
Table III. 12.--Selected Thermodynamic Functions for Co(_,]3,e) .......................................................................... 32

Table 111.13.--Selected Thermodynamic Functions for Cr(cr, e) ........................................ -.................................... 33

Table I11.14.--Selected Thermodynamic Functions for Cs(cr, f) ............................................................................. 34

Table III. 15.--Selected Thermodynamic Functions for Cu(cr,f) ............................................................................ 35

Table II1.16.--Selected Thermodynamic Functions for D 2 ..................................................................................... 36

Table III. 17.--Selected Thermodynamic Functions for Electron Gas ..................................................................... 38

Table III. 18.--Selected Thermodynamic Functions for F 2...................................................................................... 40

Table III. 19.--Selected Thermodynamic Functions for Fe( o_,y, 6,_) ........................................................................ 41

Table llI.20.--Selected Thermodynamic Functions for Ge(cr,e) ............................................................................ 43

Table II1.21.--Selected Thermodynamic Functions for H 2 ..................................................................................... 44

Table III.22.--Selected Thermodynamic Functions for He ..................................................................................... 46

Table III.23.--Selected Thermodynamic Functions for Hg(cr,_ _)............................................................................ 48

Table IlI.24.--Selected Thermodynamic Functions for I2(cr,e) .............................................................................. 49

Table III.25.--Selected Thermodynamic Functions for K(cr,_) .............................................................................. 51

Table III.26.--Selected Thermodynamic

Table III.27.---Selected Thermodynamic

Table III,28.--Selected Thermodynamic

Table III.29.--Selected Thermodynamic

Functions for Kr ..................................................................................... 52

Functions for Li(cr,e) ............................................................................. 54

Functions for Mg(cr, f) ........................................................................... 55

Functions for Mn(ce,/3,y,S,e) ................................................................... 57

Table IlI.30.--Selected Thermodynamic Functions for Mo(cr, e) ........................................................................... 58

Table III.31 .--Selected Thermodynamic Functions for N 2 ..................................................................................... 59

Table III.32.--Selected Thermodynamic Functions for Na(cr,e) ............................................................................ 61

Table III.33.--Selected Thermodynamic Functions for Nb(cr,_?) ............................................................................ 62

Table III.34.---Selected Thermodynamic Functions for Ne ..................................................................................... 63

Table III.35.--Selected Thermodynamic Functions for Ni(cr, e) ............................................................................. 65

Table III.36.--Selected Thermodynamic Functions for 02 ..................................................................................... 66

Table III.37.--Selected Thermodynamic Functions for P(cr,white,e) ..................................................................... 68

Table III.38.--Selected Thermodynamic Functions for Pb(cr,t _) ............................................................................. 69

iv
Table III.39.--Selected Thermodynamic Functions for Rblcr,/:') ............................................................................ 70

Table III.40.--Selected Thermodynamic Functions for S(o_,/3,_f) ............................................................................ 71

Table III.41. Selected Thermodynamic Functions for Si(cr,(') ............................................................................. 72

Table llI.42.--Selected Thermodynamic Functions for Sn(cr,/?) ............................................................................. 73

Table III.43. Selected Thermodynamic Functions for Srta,/3,_) ...................................................................... 74

Table III.44.--Selected Thermodynamic Functions for Ta(cr,¢) ............................................................................. 75

Table III.45.--Selected Thermodynamic Functions for Th(a,]3,_) .......................................................................... 76

Table III.46.--Selected Thermodynamic Functions for Ti(a,/_,f) ................................................................... 77

Table III.47. Selected Thermodynamic Functions for U(a,6,y,f) ......................................................................... 78

Table III.48.--Selected Thermodynamic Functions for V(cr,f) ....................................................................... 79

Table III.49.--Selected Thermodynamic Functions for W(cr,t °) .................................................................... 80

Table III.50.--Selected Thermodynamic Functions for Xe ..................................................................................... 81

Table II1.51.--Selected Thermodynamic Functions for Zn(cr,f) ............................................................................ 83

Table III.52.--Selected Thermodynamic Functions for Zr(a,/3,f) .......................................................................... 84

Table IV.--Enthalpy and Gibbs Energy Input for PAC91 (EFdata) .................................................................. 85

Table V.--Format for 9-Constant Functional Form ..................................................................................... 123

Table VI.--Coefficients for the 9-Constant Functional Form ................................................................................. 124

Table VII.--Format for the 7-Constant Polynomial Form (Old Format) ................................................................ 135

Table VIII.---Coefficients for the 7-Constant Functional Form ............................................................................... 136

Table IX. 1.--Thermodynamic Functions From Coefficients for Ag(cr,t _) .............................................................. 143

Table IX.2. Thermodynamic Functions From Coefficients for Al(cr,/?) ......................................................... 144

Table IX.3. Thermodynamic Functions From Coefficients for Ar ....................................................................... 145

Table IX.4. Thermodynamic Functions From Coefficients for B(/3,f) ................................................................. 147

Table IX.5.--Thermodynamic Functions From Coefficients for Ba(cr,¢) .............................................................. 148

Table IX.6. Thermodynamic Functions From Coefficfents for Be(c_,/_,e) ............................................................ ld9

Table IX.7.----Thermodynamic Functions From Coefficients for Br2(cr,¢) ............................................................. 150

Table IX.8.--Thermodynamic Functions From Coefficients for C(gr) ................................................................... 151
TableIX.9. Thermodynamic FunctionsFromCoefficientsforCa(a,fl, f) .................................................... 152

Table IX. 10.--Thermodynamic Functions From Coefficients for Cd(cr,(') ............................................................ 153

Table IX. 11.--Thermodynamic Functions From Coefficients for CI2 .................................................................... 154

Table IX. 12.--Thermodynamic Functions From Coefficients for Co(a, fl,() ...................................................... 155

Table IX. 13.--Thermodynamic Functions From Coefficients for Cr(cr,e) .................................................. 156

Table IX. 14.--Thermodynamic Functions From Coefficients for Cs(cr,() .................................................... 157

Table IX. 15.--Thermodynamic Functions From Coefficients for Cu(cr, f) ............................................................ 158

Table IX. 16.--Thermodynamic Functions From Coefficients for D 2 ..................................... 159

Table IX. 17.---Thermodynamic Functions From Coefficients for Electron Gas ............................................... 161

Table IX. 18.--Thermodynamic Functions From Coefficients for F2 ...................................................................... 163

Table IX. 19.--Thermodynamic Functions From Coefficients for Fe(a, _,S,e) ........................................................ 164

Table IX.20.--Thermodynamic Functions From Coefficients for Ge(cr,_) ............................................................ 165

Table IX.21 .--Thermodynamic Functions From Coefficients for H 2 ..................................................................... 166

Table IX.22.--Thermodynamic Functions From Coefficients for He ..................................................................... 168

Table IX.23.--Thermodynamic Functions From Coefficients for Hg(cr,f) ............................................................ 170

Table IX.24. Thermodynamic Functions From Coefficients for I2(cr, f) .............................................................. 171

Table IX.25. Thermodynamic Functions From Coefficients for K(cr,f) .............................................................. 172

Table IX.26.--Thermodynamic Functions From Coefficients for Kr ...................................... 173

Table IX.27.--Thermodynamic Functions From Coefficients for Li(cr,e) ............................................................. 175

Table Ix.28.--Thermodynamic Functions From Coefficients for Mg(cr,f) ........................................................... 176

Table IX.29.--Thermodynamic Functions From Coefficients for Mn(a, fl,_,6,_) ................................................... 177

Table IX.30.--Thermodynamic Functions From Coefficients for Mo(cr,e) ........................................................... 178

Table IX.3 l.--Thermodynamic Functions From Coefficients for N 2 ..................................................................... 179

Table Ix.32.--Thermodynamic Functions From Coefficients for Na(cr, e) ............................................................ 181

Table IX.33. Thermodynamic Functions From Coefficients for Nb(cr,_) ............................................................ 182

Table IX.34.--Thermodynamic Functions From Coefficients for Ne ........................................ 183

Table Ix.35.--Thermodynamic Functions From Coefficients for Ni(cr,f) ............................................................. 185

vi
TableIX.36.--Thermodynamic FunctionsFromCoefficientsforO2..................................................................... 186

TableIX.37.--Thennodynamic FunctionsFromCoefficientsforP(cr,white,f) ..................................................... 188

TableIX.38.--Thermodynamic FunctionsFromCoefficientsforPb(cr,(_) ............................................................. 189

TableIX.39.--Thermodynamic FunctionsFromCoefficientsforRb(cr,(3............................................................ 190

Table IX.40.--Thermodynamic Functions From Coefficients for S_c_,/3,_) ............................................................ 191

Table IX.41 .--Thermodynamic Functions From Coefficients for Si(cr,e) ............................................................ 192

Table IX.42.--Thermodynamic Functions From Coefficients for Sn(cr, f) ......................................................... 193

Table IX.43.--Thermodynamic Functions From Coefficients for Sr(a, fl,_) ........................................................... 194

Table IX.44.--Thermodynamic Functions From Coefficients for Ta(cr,f) .......................................................... 195

Table IX.45.--Thermodynamic Functions From Coefficients for Th(ot, fl,_) .......................................................... 196

Table IX.46. Thermodynamic Functions From Coefficients for Ti(a,/3,() ........................................................... 197

Table IX.47.--Thermodynamic Functions From Coefficients for U(a,/3,7,e) ..................................................... 198

Table IX.48. Thermodynamic Functions From Coefficients for V(cr,() .............................................................. 199

Table IX.49.--Thermodynamic Functions From Coefficients for W(cr,_) ............................................................. 200

Table IX.50.--Thermodynamic Functions From Coefficients for Xe ................................................................. 201

Table IX.51 .--Thermodynamic Functions From Coefficients for Zn(cr,() ............................................................ 203

Table IX.52. Thermodynamic Functions From Coefficients for Zr(a, fl,/_) ......................................................... 204

Table X.--Least-Squares Fitting Differences With the 9-Constant Functional Form ............................................ 205

Figure l.---Comparison of Selected (Labeled Original) Cp Values Given in Table III With Values

Calculated From the 9-Constant Coefficients Given in Table VI ......................................................................... 220

vii

Summary

This report is a compilation of thermodynamic functions of

50 elements in their standard reference state. The functions

are C;, {H°(T) - n°(0)}, S°(T), and - {G°(T) - H°(O)} for

the elements Ag, AI, Ar, B, Ba, Be, Br2, C, Ca, Cd, C12, Co,

Cr, Cs, cu, F2, Fe, Ge, H 2, He, Hg, 12, K, Kr, Li, Mg, Mn,

Mo, N 2, Na, Nb, Ne, Ni, O 2, P, Pb, Rb, S, St, Sn, Sr, Ta, Th,

Ti, U, V, W, Xe, Zn, and Zr. Deuterium D 2 and electron gas

e- are also included. The data are tabulated as functions of

temperature as well as given in the form of least-squares

coefficients for two functional forms for C/_ with integration

constants for enthalpy and entropy. One functional form for

C/_ is a fourth-order polynomial and the other has two

additional terms, one with T -I and the other with T -2. The

gases At, D2, e-, H 2, He, Kr, N2, Ne, 02, and Xe are tabulated

for temperatures from 100 to 20 000 K. The remaining gases

CI2 and F2 are tabulated from 100 to 6000 K. The polynomial

functional form for C_ for all these gases is split into the two

temperature intervals of 200 to 1000 K and 1000 to 6000 K.

The second functional form for Cff has an additional interval

from 6000 to 20 000 K for the gases tabulated to 20 000 K.

The fits are constrained so that the properties match at the

common temperature endpoints. The temperature ranges for

the condensed species vary with range of the data, phase

changes, and shapes of the C/_ curves.

Introduction

This report contains thermodynamic functions for 50

chemical elements plus electron .gas and deuterium in their

standard state. The functions presented are C_, {H°(T)

- H°(0)}, S°(T), and - {G°(T) - H°(0)}. This report is

being published primarily to document part of the data currently

being used in several NASA Lewis computer programs:

PAC91 (ref. 1), CET89 (refs. 2 and 3), GCKP84 (ref. 4),

CEA, and LSENS. CEA and LSENS are the newest Lewis

codes for chemical equilibrium and kinetics, respectively, and

are currently being documented. Selection of thermodynamic

data for the elements is important inasmuch as these elements

serve as a reference set from which all other species are

formed. The reactions of formation and their corresponding

equilibrium constants can then be specified unambiguously.

Several earlier references exist which contain

thermodynamic dala for the elements (e.g., refs. 5 and 6).

Some of the data in these references are obsolete and in other

cases the data do not extend to sufficiently high temperatures.

Most of the data for this report were selected from nine recent

references. Data for the monatomic gases and electron gas

were calculated by means of the PAC91 computer program.

Data for all species were processed by the PAC9! program to

obtain several tables for each species. Tables are given for

(1) the selected thermodynamic functions, (2) coefficients for

two functional forms for Ct° which were generated by PAC91

(usually the result of a least-squares fit), (3) thermodynamic

functions generated from these coefficients, (4) enthalpies

and Gibbs energies (EF data) used by PACgl to calculate

heats of formation and Iogl0K values for other compounds,

and (5) maximum and average differences between the selected

data and the fitted data. Plots are also given tbr C ° versus iJ

temperature for the selected data as well as for the fitted data

calculated from one of the functional forms.

In general, the data are given without additional discussion

inasmuch as the details of the selection, smoothing, averaging,

interpolating, extrapolating, and other processing of the source

data are covered adequately in the source references. In a few

cases some additional discussion is given.

Symbols

ai

b 1

b2

c;

c2

a°(T)

0003 - Ho(o)

GO(T) - Ho(298.15)

polynomial coefficients used in eqs.

(J) to (3)

integration constant defined by eq. (2)

integration constant defined by eq. (3)

heat capacity at constant pressure for

standard state

second radiation constant

either {GO(T) - H°(0)} + H°(O) or

{GO(T) - HO(298.15)} + H°(298.15)

Gibbs energy at temperature T relative

to enthalpy at 0 K for standard state

Gibbs energy at temperature Trelative

to enthalpy at 298.15 K for

standard state

NASA/TP-3287/REV 1 1
H°(O)

H°(298.15)

H°(_

//0(7) -//o(298.15)

afH°(T)

h

K

k

me

N

qi

R

r

So/R

So(T)

T

U

Gibbs energy of formation of a

substance at temperature T from its

reference elements in their standard

state

chemical energy at 0 K for standard

state

assigned enthalpy at 298.15 K for

standard state (equal to

AIH°(298.15))

either {H°(T) - n°(0)} + H°(O) or

{He(T) -//o(298.15)} +/-/°(298.15)

sensible enthaipy at temperature T

relative to 298.15 K for standard state

enthalpy of formation (heat of

formation) of a substance at

temperature T from its reference

elements in their standard state

Planck's constant

equilibrium constant

Boltzmann constant

electron mass

principal quantum number for atomic

species

temperature exponents in eq. (1)

universal gas constant

number of coefficients ai in eq. (1)

Sackur-Tetrode constant

entropy at temperature T for standard

stale

temperature, K

atomic mass unit used for the

calculation of molar masses,

u = 1/12 mass 12C

Standard States, Reference States, and

Fundamental Constants

The symbols and definitions follow the recommendations

of reference 7. All data in this report are for elements in their

standard state. For gases, this is ideal gas at standard pressure

of 105 Pa (1 bar). For condensed species, the standard state

is the pure crystalline or liquid substance at the same standard

pressure. All thermodynamic properties are standard molar

quantities.

The reference states of the elements are indicated in table I.

Generally they are taken to be the thermodynamically stable

state at 298.15 K. For those elements which are gases at

298.15 K and a pressure of 1 bar, the entire temperature range

is taken to be gaseous. For species that are condensed at

298.15 K, the entire range is taken to be condensed with

transitions between various phases such as between solid and

liquid phases.

Most of the properties are given in the International System

of Units (SI); that is, the temperatures are in Kelvin (K),

energies in joules (J), and pressures in pascals (Pa). Sometimes

the values are made dimensionless by dividing them either by

the gas constant R or RT. The fundamental constants were

taken from reference 8 and are as follows:

Quantity

Molar gas constant

Sackur-Tetrode constant:

For po.,--100 _)0 Pa=] bar

For po=]01 325 Pa=]atm

Second radiation constant, hc/k

Electron mass

Symbol Value Units

R 8,31451_70) .... J/(moI-K

SolR -1.151693(21)

So/R -1.64856(21)

c 2 .0t438769(12) mK

nte 0.000548579903( 13 ) u

These constants were used in PAC91 (ref. 1) in calculating

the thermodynamic functions for the monatomic gases. The

atomic weights were taken from reference 9. These weights

are given in atomic mass units (u) based on 12C = 12 u. Some

of the thermodynamic functions taken from the literature were

calculated with values of R and Sackur-Tetrode constants

different from those selected for this report. In this event,

corrections were made to these thermodynamic functions to

adjust for the differences in these values. In the case of the

Sackur-Tetrode constant, corrections were made to entropy

and Gibbs energy values for calculations that were made

using I atm for the standard state pressure rather than 1 bar.

Sources For Thermodynamic Functions

Except for the monatomic gases and electron gas, the

thermodynamic functions C_, _H°(T) - H°(0)}, and S°(T)

were taken from nine recent compilations of data (refs. 10 to

18). The specific references for each element are given in

table ! where the elements are listed alphabetically by chemical

symbol. PAC91 (ref. 1) was used to calculate the functions for

monatomic gases.

Generally the data for the diatomic gases were taken from

references 13 to 16, group IIA metals from reference 18, a

few metals from references 15 and 16, the remaining metals

from references 10 to 12, and graphite from reference 17.

Some of the details are given in the notes at the end of table I.

The electronic levels given in references 19 to 21 were used

by the PAC91 program to calculate thermodynamic functions

for the noble gases He, Ne, At, Kr, and Xe to 20 000 K. For

the first four of these gases, some of these levels were

eliminated by the temperature cutoff method (TEMPER in

ref.1) and some levels were added by the FILL option in

reference 1 These four gases have a nearly constant C ° to at

• F

least 6000 K. For Xe, however, only those levels for principal

quantum number 5 were used including levels supplied by the

2 NASA/TP-3287/REV 1
FILL technique. ThereasonfortreatingXedifferentlyfrom

theothernoblegasespertainstoresultsobtainedfromthe

least-squares fit. Asdiscussedinthesection, Least-Squares

Fitonlyonetemperatureintervalisusedtofit dataforgases

from6000to20000K.Forthefirstfournoblegases, errors

resultingfromtheleast-squares fit of datacalculatedwith

temperaturecutoffmethodareacceptablysmall.However,

thiswasnotrueforXe.Severalternatemethodsofrestricting

thenumberof electroniclevelswereexaminedwiththe

selectionofn = 5 being the most satisfactory for acceptably

small least-squares errors to 10 00t3 K. (See C/_ plots in fig. 1

and least-squares fitting errors in table X.)

Empirical Equations for Fitting the

Thermodynamic Functions

A convenient way to store the thermodynamic data

for many individual species for use with computer programs

is in the form of coefficients associated with equations that fit

the data. The following dimensionless form was chosen for

this report:

C o r

= Z aiTqi

R

i=1

(1)

Two sets of qi values were used in this report. One set

is used by references 2 and 3 where r = 5 and the qi values

are 0, I, 2, 3, and 4. The second set has two additional terms

(r = 7), one with qi = -1 and one with qi = -2. (See the

section Least-Squares Fit for an additional discussion of

thesc equations.)

Enthalpy and entropy are related thermodynamically

to Cp'/R as follows:

n ° (T) _-_bl+._G ar (2)

RT T RT

S°(T) = b2 + dT

R

(3)

where b I and b2 are integration constants. These are two

additional constants (or coefficients) to the five or seven

coefficients in equation (1). The form used in references 2 and

3 will be referred to as the seven-coefficient set (r = 5 + b I + b2)

and the equations given in table V will be referred to as the ninecoefficient set.

Assigned Enthalpy Values

For some applications, such as discussed in reference 2, it

is convenient to combine sensible enthaipy and energies of

chemical and physical changes into one numerical value. An

arbitrary base may be adopted for assigning absolute values

to the enthalpy of various substances inasmuch as only

differences in enthalpies are measurable. For this report, as

well as references 1 to 4, the arbitrary base selected was a

value of zero at 298.15 K for the reference elements.

Thus, for the assigned reference elements:

A.fH°(298.15) = H°(298.15) = 0 (4)

And, in general, for all species:

H°(298.15) = AfH°(298.15) (5)

H°(T) = H°(298.15)+{H°(T)-H°(298.15)} (6)

Heats of Formation and Equilibrium

Constants

Heats of formation and logt0 K for a species are

calculated as a function of temperature for the formation of

the species from the elements in their assigned reference state.

The following is an example of how these properties can be

calculated for CO(g) at I000 K:

AfH°(1000) = H°(1000)CO(g)- H°(1000)C(gr)

- 1H°(1000)O2 (g)

2

(7)

Ata ° (10o0): a °0000)CO(g)- C°(1000)C(gr)

1

- --CO(1000)O2(g)

2

(8)

By definition,

lOgl0 K =

-A/G°(T)

2.3025851 RT

(9)

NASA/TP-3287/REV 1 3
Least-Squares Fit

For most of the elements in this report, the coefficients

in equations (1) to (3) were obtained by means of a leastsquares fit. PAC9] (ref. 1) was used to obtain the coefficients.

For the gases the temperature intervals for both functional

forms are fixed. These intervals are 200 to 1000 K and 1000

to 6000 K for the seven-constant form (i.e., the fourth-order

polynomial for Cff used in the past). The nine-constant form

given in table V uses these same intervals plus an additional

interval from 6000 to 20 000 K for all gaseous elements

except F2 and CI2. For the condensed species, each phase has

its own set of coefficients. The seven-constant form uses

either one or two intervals for each phase with endpoint limits

according to the transition points. Two intervals are used

when the temperature range for a phase includes the 1000 K

breakpoint. The nine-constant functional form has a flexible

number of brcakpoints in order to fit the selected data more

accurately.

Generally the functions C_/R, H°(T)/R, and S°(T)/R were

fit simultaneously. The fit was constrained to match the

functions exactly at 298.15 K. Thus, the least-squares

coefficients reproduce heats of formation at 298.15 K exactly.

For temperature intervals that do not contain T=298.15 K, the

fit was constrained to give the same functional values at the

common temperature point for any contiguous intervals. When

phase transitions occur, the fit was constrained so that the

difference in Gibbs energy is zero between the phases.

For some elements and some temperature intervals, however,

coefficients were not obtained by means of the PAC91 leastsquares fit. These exceptions were as follows:

(1) The inert gases and electron gas--Ar, He, Kr, Ne, Xe,

o for electron gas is constant for the entire and e-. Cp

temperature range and is constant to some high temperature

for the inerts. For Ar, He, and Ne data, the least-squares fit

was done only for the interval above 6000 K. For Kr and Xe

data, the fit was done for the two intervals above 1000 K.

(2) Some species where the C/7 equations are given in the

original reference- Ba, Be, Mg, Ca, Sr, Pb, S, and Sn. Except

for Be(f), for which (..po was taken to be a constant from

reference 12, group I1A elements data (Be, Mg, Ca, Sr, and

Ba) were generated from the equations in reference 18. Only

the data for the alpha phases were refit because of the

discontinuities at 298.15 K in reference 18. Equations for the

liquid phases of Pb, S, and Sn were taken directly from

references 15 and 16.

o is given as a

(3) For 29 elements in the liquid state. Cp

constant in the references from which the data are taken.

The temperature intervals for the coefficients, whether they

were obtained from a PAC91 least-squares fit or other sources,

are given in table 1. The format and coefficients for the nineconstant functional form arc given in tables V and VI,

respectively, and for the seven-constant functional form in

tables VII and VIII, respectively. Table X gives information

for the PAC91 fits only. It lists the maximum and average

errors for the nine-constant fit. The two additional terms in

the nine-constant functional form generally give approximately

an order of magnitude improvement in the error of the fit. See

the Tables section for definitions and a discussion of this

information. Plots of C ° for the selected data as well as the

data calculated using t_e the nine-constant functional form

are given in figure 1.

Tables

There are nine tables of data. The order of the elements in

each table is alphabetical by chemical symbol. Two of these

tables are each subdivided into 52 subtables of thermodynamic

functions for the 52 species (50 elements plus deuterium and

electron gas) for a schedule of temperatures. These two tables

are table Ili, which contains thermodynamic functions selected

from the cited references, and table IX, which contains

thermodynamic functions generated from fitting these

functions. Data from table 111will be referred to as selected

tables or data and data from table IX will be referred to as

coefficients tables or data.

Table i summarizes some information concerning each of

the 52 species. This information consists of the name, chemical

symbol, state, reference code, atomic or molecular weight,

temperature ranges covered by the coefficients, references

from which the thcrmodynamic data were taken, and letters

indicating additional comments at the end of the table. Most

of the data given in the selected tables start at temperatures

lower than the low end of the temperature range of the fitted

data. Since the elements constitute the reference set of species

from which all other species are formed, their heats of

formation are all zero and are not tabulated. The reference

code is a six-character code associated with each set of

coefficients to indicate the major source of the data. The

numbers indicate the date of the reference and the letters

indicate the sourcc as follows: CODA (CODATA, refs. _11

and 12); L (NASA Lewis Research Center, ref. 1); J (JANAF,

ref. 10); TPIS (Thermodynamic Properties of Individual

Substances, refs. 13 to 16); SRD (Standard Reference Data,

ref. 18); and X (TeXas, ref.17). For J and X, the date is

associated with the individual species as given in the selected

reference: for example, J 6/83 indicates JANAF data dated

June 1983.

Table I1 tabulates the molecular weights and summarizes

values of the thermodynamic functions at T = 298.15 K.

These functions include {H°(298.15) - H°(0)}, Ct_, and

S°(298.15). Most of the least-squares fitting was constrained

.to fit these values at 298.15 K. In this event, these values are

the same for both the selected and coefficients data.

Table III contains the selected data for the 52 species.

Generally the temperature schedules are every 100 K with

some inserted temperatures for 298.15 K, transition points,

4 NASA/TP-3287/REV 1
and, in some cases, lower temperatures. The thermodynamic

functions are in SI units and include C_, {H°(T) - H°(0)},

S°(T), -{G°(T) - H°(O)}/T, H°(T), and -G°(T)/T. Heats of

formation and Iogl0K values were not included in the table

since these values are zero for reference elements by definition.

Plots of the C ° data are given in figure 1

p

Table IV gives the enthalpy and Gibbs energy data in

dimensionless form and in the format required by the PAC91

computer program described in reference 1. These data are

referred to as EFdata in that reference and are used to calculate

heats of formation and iogl0 K of species formed from the

elements. In table IV, data for each reference element are

preceeded by a header record containing some relevant

information about that element. For example, the header for

the first element in table IV (Ag) contains the following

information:

Code Meaning

EFDA

AG1S

CODA89

H0/R

- 690.9607

MP

1235.0800

NT

63

EFdata record

element name, Agj(s)

code for data reference

M°(o)/n

value for above

melting point

value for the melting point, K

number of temperatures for this element

value for above

In each data record following the header card, the six

values given are for a temperature, followed by its value of

H°(T)/RT and -G°(T)/RT, and the next temperature, followed

by its value of H°(T)/RT and -G°(T)/RT.

Table V gives the format for the coefficients in the nineconstant functional form (eqs. 0) to (3) with r = 7).

Table VI lists the set of coefficients having the format of

table V. In this report gaseous species have a temperature

interval break point at 1000 K. For gaseous species with data

given to 20 000 K, there is an additional break point at 6000 K.

For condensed species, in addition to break points at phase

transitions, additional interval break points have been selected

to reduce differences between the fitted and selected data.

Plots of C_ values from this table are given in figure 1.

TableVII gives the format for the coefficients in the sevenconstant functional form (eqs.(l) to (3) with r = 5).

Table VIII lists the set of coefficients having the format of

table VII. The seven constants include five constants for a

fourth-order polynomial for Cfl and two integration constants.

This is the form used for many years in several NASA Lewis

computer programs (refs. 2 to 4). These data are in the "old"

format required by these programs and described in reference 2.

When the temperature range embraces 1000 K, there is always

a break point at 1000 K and there are always two intervals for

this format. Most older data were constrained to match the

selected data at the 1000 K break point. However, for this

report the data are constrained to fit the selected data at

298.15 K and to match at the break points.

Table 1X is similar to table 1II in that it contains tables of

thermodynamic functions for the 52 species. The data for

table IX, however, were calculated from the coefficients listed

in table VI, the nine-constant functional form given in table V.

The temperature schedule is always from 200 K in 100 K

intervals to the maximum temperature of the equations. There

are temperatures inserted for 0, 298.15, and transition points.

The thermodynamic functions are in SI units and include C_,

{H°(T) - H°(0)}, S°(T), -{G°(T) - H°(O)}/T, H°(T), and

-G°(T)/T.

Table X summarizes the maximum, average, and leastsquares errors between the fitted and the selected data for

each temperature interval. Only data where the coefficients

were obtained from a PAC91 least-squares fit are listed. There

are two sets of errors: (1) the selected value minus the calculated

value and (2) a relative error, which is this value divided by

the selected value. The least-squares error is the root mean

square of errors. Errors are labeled MAX ERR, AVER ERR,

and LST SQ ERR. The relative errors are labeled MAX REL

ERR, AVER REL ERR, and REL LST SQ ERR. Both sets are

given for C°/R, {H°(T) -H°(O)}/RT, S°(T)/R, and -{G°(T)

- H°(O)}/_?T. See the section Least.Squares Fit for a

discussion of the constraints. The maximum relative error for

C_/R is labeled MAX REL ERR CP/R. Note that most errors

are less than _ percent. The exceptions are the alpha phase of

iron Fe(et) above the iambda transition and the noble gases

Ar, Kr, and Xe above 10 000 K.

Concluding Remarks

Tables of thermodynamic functions are presented for 50

elements plus electron gas and deuterium in their standard

reference state. Selection of these data for the elements is

important inasmuch as the elements serve as a reference set

from which all other species are formed. The tables are given

for (1) the selected thermodynamic funcitons, (2) coefficients

for two functional forms for C/_ and (3) thermodynamic

functions generated from coefficients for one of the functional

forms. Plots are also given for C/_ versus temperature for

(1) and (3). This report should prove useful as a compilation

of thermodynamic data of the elements as well as providing

documentation for some of the data currently used in a number

of NASA Lewis computer programs.

NASA/TP-3287/REV 1 5
References

!. McBride, B.J.; and Gordon, S.: Computer Program for Calculating and

Fitting Thermodynamic Functions. NASA RP-1271, 1992.

2. Gordon, S.; and McBride, B.J.: Computer Program for Calculation of

Complex Chemical Equilibrium Compositions, Rocket Perfi_rmance,

Incident and Reflected Shocks, and Chapman-Jouguet Detonations.

NASA SP-273, 1976.

3. Gordon, S.; and McBride, B.J.: Finite Area Combustor Theoretical

Rocket Performance. NASA TM-100785, 1988.

4. Bittker, D.A.; and Scullin, V.J.: GCKP84-General Chemical Kinetics

Code for Gas-Phase Flow and Batch Processes Including Heat Transfer

Effects. NASA TP-2320, 1984.

5. Stall, D.R.; and Sinke, G.C.: Thermodynamic Properties of the Elements. American Chemical Society, Washington, DC. 1956.

6. Hultgrcn, g., et al.: Selected Values of Thermodynamic Properties of

Metals and Alloys. John Wiley & Sons, Inc., New York, 1963.

7. Cox, J.D.: Notation for Statcs and Processes, Significance of the Word

Standard in Chemical Thermodynamics, and Remarks on Commonly

Tabulated Forms of Thermodynamic Functions. Pure Appl. Chem.,

vol..54, no. 6, 1982, pp. 1239-1250.

8. Cohen, E.R.; and Taylor, B.N.: The 1986 CODATA Recommended

Values of the Fundamental Physical Constants. L Res. NBS, rot. 92,

no. 2, Mar-Apr. 1987, pp. 8.5-95.

9. IUPAC Commission on Atomic Weights and Isotopic Abundances,

Atomic Weights of the Etements 1985. Pure Appl. Chem., vol. 58,

no. 12, 1986, pp. 1677-1682.

10. Chase, M.W. Jr., et al.: JANAF Thermochcmical Tables. Third Ed., Pts.

I. & 2. American Institute of Physics, New York, 1986.

! 1. Garvin, D.; Parker, V.B.; and White, H.J., Jr.: CODATA Thermodynamic

Tables. Hemisphere Publishing Corp., New York, 1987.

12. Cox, J.D.; Wagman, D.D.; and Medvedev, V.A.: CODATA Key Values

for Thermodynamics. Ilcmispherc Publishing Corp., 1989.

13. Gurvich, L.V., et al.: Thermodynamic Properties of Individual Substances.

Vol. 1, Pts. 1 & 2. Nanka, Moscow, USSR, 1978.

14. Gurvich, L.V.,etal.: Thermodynamic Propertiesoflndividual Substances.

Vol. IV, Pts. 1 & 2. Nauka, Moscow, USSR, 1982.

15. Gurvich, L.V.; Veyts, l.V.;and Alcock, C.B.: Thermodynamic Properties

of Individual Substances. Fourth Ed.. Vol. I, Pts. I & 2. Hemisphere

Publishing Corp., New York, 1989.

16. Gurvich, L.V.; Veyts, I.V.; and Alcock, C.B.: Thermodynamic Properties

of Individual Substances. Fourth Ed., Vol. 2, Pts. 1 & 2. Hemisphere

Publishing Corp., New York, 1991.

17. TRCThermodynamicTables- Hydrocarbons. Thermodynamics Research

Center, The Texas A&M University System: College Station, Texas,

1983 issue.

18. Alcock, C.B., et al.: Thermodynamic Properties of the Group IIA

Elements. To be published in J. Phys. Chem. Ref. Data, 1992.

19. Moore, C.E.: Atomic Energy Levels. Vol. i. Department of Commerce,

National Bureau of Standards, G.P.O., 1971.

20. Moore, C.E.: Atomic Energy Levels. Vol. I1. Department of Commerce,

National Bureau of Standards, G.P.O., 1971.

21. Moore, C.E.: Atomic Energy Levels. Vol. III. Department of Commerce,

National Bureau of Standards, G.P.O., 1971.

6 NASA/TP-3287/REV 1
TABLE I. - SYMBOLS, PHASES, REFERENCE CODES, TEMPERATURE RANGES, REFERENCES, AND NOTES

Table Element Symbol Phase Refer- Molec- Temperature Refer- Notes

ence ular range,K ence

code d weight (9-Cons. Coeffs.)

1 Silver Ag(cr) Cubic Crystal CODA89 107.8682 200.000 1235.080 12 a

Ag(_) Liquid CODAgO 1235.080 8000.000 12 a,b

2 Aluminum Al(cr) Cubic Crystal COBA89 25.981539 200.000 933.610 12

AI(_) Liquid CODA89 g33.610 6000.000 12 b

3 Argon Ar Oas b fi/88 3g.g48 200.000 I000. 000 19 b,c

1000.000 6000.000 19 b,c

6000.000 20000. 000 19 c

4 Boron B (O) Beta Crystal J 6/83 10.811 200.000 600.000 I0 e

600.000 2350.000 I0 e

B(_ liquid J 6/83 2350.000 5000.000 10 b

5 Barium Ba(cO Alpha Crystal Sflb 92 137.327 80.000 298.150 18 s,f,_

298.150 1000.000 18 s,m

Ba(O Liquid SRD g2 I000.000 6000.000 18 b

6 Beryllium Be(a) Alpha Crystal SRD 92 9.012182 I00,000 298.150 18 s,f,m

298.150 1543.000 18 s,m

Be(O) Beta Crystal SRD 92 1543.000 1563.000 18 s,m

Be(O Liquid SRD g2 1563.000 6000.000 12 b

7 Bromine Br2 (cr) Rhombic Crystal TPIS89 159.808 200.000 265.900 15 a,f

Br2(_ Liquid TPIS89 265.900 332.503 15 a,u

332,503 6000.000 10 b

8 Carbon C(gr) Graphite X 4/83 12.011 200.000 600.000 17 f

600.000 2000.000 17 g

2000.000 5000.000 17 g

g Calcium Ca(u) Alpha Crystal SRD 92 40.078

Ca(B) Beta Crystal SRD 92

Ca(O Liquid S_ g2

I0 C:utaxue Cd(cr) Hexagonal Crystal CODA89 112.411

Cd(_ Liquid CODA89

11 Chlorsne CI: Gas TPIS89 70.9054

12 Cobalt Co(a) Alpha Crystal J 9/67 58.9332

Co(D) Beta _ Lambda J g/87

Co(D) Beta _ Lm_bda J g/67

Co(_ Liquid J 0/67

200.000 298.150 18 s,f

298.15 716.000 18 s

716.000 1115,000 18 s,m

II15.000 6000,000 18 b

100.000 504,258 12 a,i

594.258 6000,000 12 b

200.000 1000.Q00 15 p

1000.000 6000.000 15 p

200.000 500.000 10 e

500.000 700.I00 10

700.100 800.000 I0

800.000 1394,000 I0

1394.000 1400.000 10 a

1400.000 1768.000 10

1768.000 6000.000 10 b,h

NASA/TP-3287/REV 1 7
TABLE I.-Continued.

Tabh Element Symbol Phase Refe_

ence

coded

Molec=

ular

weight

Temperature

ran&e,K

(9-Cons.Coeffs.)

ReferenceNotes

13

14

15

16

17

18

19

2O

21

22

23

24

25

26

Chromium

Cesium

Copper

Deuterium

Electron

Or(cr)

Or(cr)

Or (@

Cs(cr)

Os (,9

Cu(cr)

Cu (_

D_

Crystal _ Lambda J 6/73 51.9961

Crystal k Lambda J 6/73

Liquid J 5/73

Cubic Crystal CODA89 132.90543

Liquid CODA89

Cubic Crystal CODA8g

Liquid CODA8g

Gas TPI889

Gas L 6/88

Fluorine F2 Gas TPIS89

Iron

Germanium

Hydrogen

Fe (a)

Fe(a)

Fe(y)

Fe(_

Fe(O

Ce(cr)

63.546

4.02820

0.0005486

37.9968064

Alpha _ Lambda J 3/78 55.847

Alpha _ Lambda J 3/78

Gamma Crystal J 3/78

Delta Crystal J 3/78

Liquid J 3/78

Cubic Crystal TPISgl 72.61

Ge(@ Liquid TPIS91

Helium

Mercury

Iodine

Potassium

Gas TPIB78

LlO/90 He Gas

Hg(cr) Tetragonal Cryst. J12/61

Hg (R) Liquid 212/61

h (cr) Rhombic Crystal TPIS89

Liquid TPI889

Cubic Crystal CODA89

Liquid CODA89

X(cr)

K(0

Krypton Kr Cas LIO/gO

2.01588

4.002602

200.69

253.80894

39.0983

83.80

200.000 311.500 10 e

311.500 1000.000 10 e

1000.000 2130.000 I0 a

2130.000 6000.000 i0 a,b

I00.000 301.590

301.590 i000.000

lO00.O00 2000.000

200.000 1358.000

1358.000 6000.000

200.000 1000.000

1000.000 6000.000

6000. 000 20000.000

200.OO0 I000.000

I000.000 6000.000

6000.000 20000.000

200.000 i000.000

I000.O00 6000. 000

200.000 500.000

500.000 800.000

800.000 1042.000

i042.000 I184.000

1184.000 1665.000

1665.000 1809.000

1809.000 6000.000

200.000 400.000

400.000 1211.400

1211.400 6000.000

200.000 i000.000

I000.000 6000.000

6OOO. OOO 20000. 000

200.000 I000.000

I000.000 6000.000

6000. 000 20000.000

I00.000 234.290

234.290 600.000

6O0.0OO 2000.000

200.000 386.750

386.750 6000.000

2O0.0O0 336.860

336.860 2200.000

12

12

12

12

12

15

15

15

8

8

8

15

15

i0

10

10

I0

I0

10

I0

a

a,b

P

P

P

j,b

j,b

j,b

P

P

e

e

g

a,

a,b

16

16 a

16 a,b

13 f,k,p

13 p

13 1,p

lg b,c

19 b,c

19 c

10

10

10

15 f

15 b

12 a

12 a

e,i

2OO.OOO 1000. 000 20 b,c

1000.000 6000.000 20 b,c

6000.000 2OOO0. OOO 20 c

8 NASA/TP-3287/REV 1
TABLEI.- Continued.

Table Element Symbol Phase Reference

coded

Molecular

weight

Temperature

range,K

(9-Cons.Coeffs.)

Reference

Notes

27 Lithium

28 Magnesium

29 Manganese

30 Molybdenum

31 Nitrogen

32 Sodium

Li(or)

Li (0

Mg(cr)

Mn (a)

Mn (0)

Nn (Y)

Mn (5)

Mn (_)

t(0(cr)

Cubic Crystal TPIS82

Liquid TPIS82

Hexagonal Crystal SRD 92

Liquid SRD 92

Alpha Crystal J 9/67

Beta Crystal J 9/67

Oamma Crystal J 9/67

Delta Crystal J 9/67

Liquid J 9/67

Crystal J 3/78 95.94

Mo(0 Liquid J 3/78

N2 Gas TPIS78

33 Niobium Nb(cr)

34 Neon

Cubic Crystal CODA89

Liquid CODA89

6.941

24.3050

54.93805

28.01348

22.989768

Crystal J12/73 92.90638

Nb (O Liquid J12/73

Ne Gas LlO/gO

35 Nickel Ni(cr)

Ni(cr)

Ni(_

36 Oxygen 02

37 Phosphorus

38 Lead

20.1797

Crystal _ Lambda J12/76 58.69

Crystal _ Lambda J12/76

Liquid J12/76

Gas TPIS89 31.9988

Crystal(White) TPIS89

Liquid TPIS89

Cubic Crystal TPISgl

Liquid TPIS91

39 Rubidium

P(cr)

P (@

Pb(cr)

Pb (0

Rb(cr)

Rb (_

Cubic Crystal CODA89

Liquid CODAS9

30.973762

207.2

85.4678

200.000 298.150

298.150 453.690

453.690 6000.000

100.000 298.150

298.150 923.000

923.000 6000.000

200.000 980.000

980.000 1361.000

1381.000 1412.000

1412.000 1519.000

1519.000 6000.000

14 g

14

14

18 s,f,m

18 s,=

18 b

10 _,e,f

10 a

I0

10

10 b

200.000 I000.000 I0 e

1000.000 2200.000 I0

2200.000 2896.000 I0 a,o

2896.000 6000.000 10 a,b,o

200.000 1000.000 13 n,p

1000.000 6000.000 13 n,p

6000.000 20000.000 13 n,p

200.000 371.010 12 a

371.010 2300.000 12 a

200.000 1000.000 10

I000.000 2000.000 10

2000.000 2750.OO0 10 a

2750.000 6000.000 10 a,b

200.000 1000.000 19 b,c

lO00.O0O 6000.000 19 b,c

6000.000 20000.000 19 c

200.000 400.000

400.000 631.000

631.000 1200.000

1200.000 1728.000

1728.000 6000.000

I0 e

i0

I0

I0 a,o

10 h,h,o

200.000 I000.000 15 g ,p

I000.000 6000.000 15 p

6000.000 20000.000 15 p

lg5.400 317.300 15 a,q

317.300 6000.000 ]5 a,b

200.000 600.650 16

600.650 3600.000 16 m

100.000 312.470 12 r

312.470 1000.000 12

1000.000 2100.000 12

NASA/TP-3287/REV 1 9
TABLE I. - Continued.

Table Element Symbol Phase Reference

code d

_olecular

weight

Temperature

range,K

(_Cons.Coeffs.)

ReferenceNotes

4O

41

42

43

44

45

46

47

48

49

5O

Sulfur

Silicon

Tin

Strontium

Tantalum

Thorium

Titanium

Uranium

S (=)

S (P)

S (7

si(cr)

si (@

Alpha Crystal TPIS89

Bsta Crystal TPIS89

Liquid TPIS8@

Cubic Crystal TPZS@I

Liquid TPIS91

Sn(cr) Tetragonal Cryst. TPIS91

Sn(_ Liquid TPISgl

Sr(_ Alpha Crystal SRD 92

Sr(p) Beta Crystal SRD 92

Sr(_ Liquid SRD 92

Ta(cr) Crystal J12/72

Ta(@ Liquid J12/72

Th (a)

Th (IS)

Th (_)

Ti(_

Alpha Crystal CODA89

Beta Crystal CODA89

Liquid CODA89

32.066

28.0855

118.710

87.62

180.9479

232.0381

Alpha Crystal CODAg9 47.88

Ti(_) Beta Crystal CODA89

Ti(_ Liquid CODA89

Alpha Crystal CODA89

Beta Crystal CODA89

Ga=ma Crystal CODA80

Liquid CODA8O

U (a)

U(P)

U(y)

U(@

Vanadium V(cr) Crystal J 6/73

Tungsten

Xenon

V(@ Liquid J 6/73

W(cr) Crystal J 6/66

W(_ Liquid J 6/66

Xe Cu L12/91

238.0289

50.0415

183.85

131.29

200.000 368.300

368.300 388.360

388.360 428.150

428.150 432.250

432.250 453.150

453.150 717.000

717.000 6000.000

2OO.000 298.150

298.150 16g0.000

1690.000 6000.000

200.000 505.118

505.118 4700.000

IOO.O00 298.150

298.150 820.000

820.000 1041.000

1041.000 6000.000

15 s

15 s

15 s,m

15 , s,m

15 s,m

15 s,m

15 b

16 g

16

16 b

16 a,s

16 a,m,s

18 s

18 s

18 s,m

18 b

200.000 1000.000 10 a,e

1000.000 2000.000 10

2000.000 3258.000 10 a

3258.000 6000.000 10 a,b

200.000 1650.000 12

1650.000 2023.000 12 a,h

2023.000 6000.000 12 a,b,h

200,000 900.000

900.000 1156.000

I156.000 1944.000

1944.000 6000.000

12

12

12 a

12 a,b

200.000 942.000 12 a

942.000 1049.000 12 a,b

1049.000 1408.000 12 b,h

1408.000 4000.000 12

2O0.000 600. OOO

600.000 1400. 000

1400.000 2190.000

2190.000 6000.000

10

1O

10 a,o

i0 a,b,o

2OO.O00 I000.000 I0

1000.000 2600.000 10

2600.000 3200.000 10

3200.OO0 3680.000 10 a

3680.000 6000.000 10 a,b

200.000 I000.000 21 t,b

i000.000 6000.000 21 t

6000.000 20000.000 21 t

10 NASA/TP-3287/REV 1
TABLE 1.- Concluded.

Table Element Symbol Phase Refer- Mo]ec- Temperature Refer- Notes

ence ular range, K ence

code d weight (9-Cons. Coeffs.)

51 Zinc Zn(cr) Hexagonal Crystal CODA8g 65.39 200.000 692.730 12 a

Zn(_ Liquid CODA89 692.730 6000.000 12 a,b

52 Zirconium Zr(a) Alpha Crystal J 6/79 91,224 200.000 I135.000 I0

Zr(_) Beta Crystal J 6/79 1135.000 2125.000 I0 a

Zr(_ Liqu£d J 6/70 2125.000 6000.000 I0 a,b

aVMues of the functions at temperatures where there are phase transitions or enthalpies of transition were adjusted so functions at the transition

temperature and higher round to match the original reference.

b C ° is constant in this interval.

P

¢PAC91 computer program (ref. 1) was used to calculaZe the functions using method TEMPER to cut off higher electronic levels and the FILL

option to fill in predicted but as yet unobserved electronic levels.

dSix-churscter code is associated with each set of coefficients to indicate the major source of the data. Letters indicate the reference while the

numbers indicate the date of the reference. The letter codes are as fo]lows: CODA (CODATA, refs. 11 and 12); L {Lew]s, ref. 1), J {JANAF,

ref. 10); SRD (Standard Reference Data, r_. 18}; TPIS {Thermodynamic Properties of Individual Substances, refs. 13 to 16); and X (TeXas,

ref. 17). Thus, CODA89 refers to CODATA, 1989 (ref. 12), For J and X, the date is associated with the individual species as given with the

data. For L the date refers to the date of the calculation.

eSome daGa at intermediate temperatures were obtained from Malcolm Chase by private communication.

IFor this species thermodynamic functions in the selected data of table HI as well as the EF data in table IV are given to temperatures lower than

the fitted temperature range.

gSelected date. are interpolated to obtain data at intermediate temperatures in order to obtain an improved least-squares fit,

bAn attempt was made to adjust some of the values so the data would round to values that match the original reference. However a few values

are still off in the last figure.

iLeast-squares fit was started at 100 K rather than 200 K because the fit was just about as good,

JPACgl computer program (ref. 1) was used to calculate the functions assuming ground stnte only and a statistical weight of 2. The electron mass

was t_en to be 0,00054858 from reference 8.

kData for T = 50 K and T = 150 K were taken from reference 17, June 20, 1986. Data for 250 and $50 K were taken from reference 10, March

1977.

IC; values are the same in a newer reference {ref. 151 but the enthalpies and entropies are more consistent with the C °p values at high

temperatures in the older reference.

mEquations for C ° were taken from the reference.

p

aValues at 150 K was obtained by interpolation mad adjustment. Values of 250 and 350 K were taken from reference 10, The H°(T)- H°(0) values

at very high temperatures were adjusted to be more consistent with C ° and S°{T) values.

P

°Heat of transition used differs slightly f_om the one given in the reference probably because of rounding when converting from calories to joules.

PReference data were calculated with a value for gas constant R different from the value R = 8.$1451 J/tool K used in this report. Adjustment

to R = 8.31451 results in some of the tabulated data differing in the last figure from the reference data.

q C ° value at 300 K was incorrect in the original reference. It was corrected for this report,

p

rc; value at 250 K was taken from reference I0. H°(25O)-H°(0) and S°(250) were obtained by numer/cal integration.

SFunctious calculated from equations given in the original reference with possibly some adjustments in the integration constants, either for

consistency between phases or to match property values given.

tpACgl computer program {ref. 1) was used to c_dculate the thermodynamic functions using the electronic levels given for the principal quantum

numbers 4 and 5 with FILL to include missing electronic levels for principal quantum number _.

uS1ight inconsistency exbsts in the data at the melting point of Br 2 in the table given in reference 15. This is reflected in tables HI and IX in this

report.

NASA/TP-3287/REV 1 11
TABLE II. - THERMODYNAMIC FUNCTIONS AT 298.15 K

Table Element Symbol Phase Atom {H°(298.15)-H°(O)} C ° S°(298.15)

hum- J/tool P J/mol/K J/mot-K

ber

1 Silver

2 Aluminum

3 Argon

4 Boron

5 Barium

6 Beryllium

7 Bromine

8 Carbon

9 Calcium

I0 Cadmium

11 Chlorine

12 Cobalt

13 Chromium

14 Cesium

15 Copper

16 Deuterium

17 Electron

18 Fluorine

19 Iron

20 Germanium

21 Hydrogen

22 Helium

23 Mercury

24 Iodine

25 Potassium

Ag(cr) Cubic Crystal 47 5745.000 25,350 42.550

Al(cr) Cubic Crystal 13 4540.000 24.200 28,300

Ar Gas 18 6197.428 20.786 154,847

B(_) Beta Crystal 5 1214.000 11.315 5.834

Ba(cr) Crystal 56 6906.992 28.110 62.352

Be(a) Alpha Crystal 4 1942.068 16.443 9,503

B_2 (0 Liquid 35 24520.000 75.680 152.210

C(gr) Graphite 6 1053.500 8.528 5.734

Ca(a) Alpha Crystal 20 5782.945 25.750 42.536

Cd(cr) Hexagonal Crystal 48 6247.000 26.020 51.800

C12 Gas 17 9181.110 33.949 223.082

Co(a) Alpha Crystal 27 4771.000 24,802 30.067

Cr(cr) Crystal 24 4057.000 23.434 23.618

Cs(cr) Cubic Crystal 55 7711.000 32,210 85,230

Cu(cr) Cubic Crystal 29 5004.000 24.440 33.150

D_ Gas 8569.103 29.195 144.960

c- Gas 6197.428 20.785 20.979

Gas 9 8825.106 31.304 202.792

Feta) Alpha Crystal 26 4507.000 25.094 27.321

Ge(cr) Cubic Crystal 32 4636.360 23.222 31.090

H2 Gas 1 8468.102 28.836 130.681

He Gas 2 6197.428 20.786 126.154

Hg(_) Liquid 80 9343.000 27.978 76.028

12 (cr) Rhombic Crystal 53 13196.000 54.440 116.139

K(cr) Cubic Crystal 19 7088.000 29.600 64.680

12 NASA/TP-3287/REV 1
TABLE If.- Concluded.

Table Element Symbol Phase Atom

number

(H°(298.15)-Ii°(0)} C °

J/mol P

J/mol-K

s°(29S.lS)

J/mol/K

26 Krypton

27 Lithium

28 Magnesium

20 Manganese

30 Molybdenum

31 Nitrogen

32 Sodium

33 Niobium

34 Neon

35 Nickel

36 Oxygen

37 Phosphorus

38 Lead

30 Rubidium

40 Sulfur

41 Silicon

42 Tin

43 Strontium

44 Tantalum

45 Thorium

46 Titanium

47 Uranium

48 Vanadium

49 Tungsten

50 Xenon

51 Zinc

52 Zirconium

Kr

Li(cr)

Ug(cr)

Un(_O

_o(cr)

_a(cr)

Nb (cr)

Ne

Ni(cr)

02

P(cr)

Pb(cr)

Rb(cr)

S m)

Si(cr)

Sn(cr)

Sr (a)

Ta(cr)

Th (a)

Ti (a)

U (a)

V(cr)

W(cr)

Xe

Zn(cr)

Zr (a)

Gas 36

Cubic Crystal 3

Hexagonal Crystal 12

Alpha Crystal 25

Crystal 42

Gas 7

Cubic Crystal 11

Crystal 41

Gas I0

Crystal 28

Gas 8

Crystal(Whlbe) 15

Cubic Crystal 82

Cubic Crystal 37

Alpha Crystal 16

Cubic Crystal 14

Tetragonal Crystal 50

Alpha Crystal 38

Crystal 73

Alpha Crystal 90

Alpha Crystal 22

Alpha Crystal g2

Crystal 23

Crystal 74

Gas 54

Hexagonal Crystal 30

Alpha Crystal 40

6197.428 20.786 164.086

4632.000 24.860 29.120

4979.161 24.775 32.535

4994.000 26.299 32.010

4585.000 23.933 28.805

8670.104 29.124 191.610

6460.000 28.230 51.300

5241.000 24,694 36.464

6197.428 20.786 146.330

4786.000 25.987 29.870

8680.104 29.378 205.149

5360.000 23.824 41.090

6870.000 26.650 64.800

7489.000 31.060 76.780

4412.000 22.690 32.070

3217.471 19.789 18.810

6323.000 27.112 61.180

6558.289 26.830 54.909

5681.000 25.295 41.471

6350.000 26,230 51.830

4824.000 25.060 30.720

6364.000 27.685 50.200

4640.000 24.806 28.g36

4073.000 24.295 32.660

6197.428 20.788 169.886

5657.000 25.390 41.630

5497.000 25.202 38.869

NASA/TP-3287/REV 1 13
TABLE lit 1 - SELECTED THERMODYNAMIC FUNCTIONS FOR Ag(cr,@

T C° H°CO-H°(O) S°(D -{O°(T)-H0(_}_ H°m _°03ff T

K J/n_kK kJ/m_ J/moI-K J/moI-K kJ/mol J/moI-K K

0 0.000 0.000 0.000 0.0O0 -5.765 IHFINITE 0

100 20.100 1.042 17.120 6.700 -4.703 66,150 I00

200 24.160 3,308 32,660 16.120 -2,437 46.865 200

298.15 25.350 5,765 42.550 23.281 0,000 42.550 298.15

300 25.356 5.792 42.707 23.400 0.0_7 42.550 300

600 25.791 8.347 50.056 29.188 2.602 43.551 600

500 26.365 10.955 55.871 35.961 5.210 45.451 500

600 26.992 13.622 60.733 38.030 7.877 47.605 600

700 27.645 16.354 66.962 01.579 10.609 69.786 700

800 28.312 19.152 68.677 66.737 15.407 51.918 800

900 28.987 22.017 72.051 47.588 16.272 53.971 900

I000 29.667 24.949 75.140 50.191 19.Z0_ 55.956 1000

1100 30.350 27,950 78.000 52.591 22.205 57.814 1100

1200 31.035 51.019 80.670 54.821 25.276 59.608 1200

cr 1235.08 31.276 32.112 81.568 55.567 Z6.367 60.219 1235.08

1235.08 33.400 63.]12 90.674 55.567 37.367 60,219 1235.08

1300 33.400 45.281 92.185 57.354 59.536 61.773 1300

1400 33.400 68.621 96.660 59.931 42.876 64.035 1400

1500 35.400 51.961 96.964 62.324 46.216 66.154 1500

!600 33.400 55,301 99.120 64.557 69.556 68.148 1600

1700 33,600 58.641 101.165 66.650 52,896 70,030 1700

1800 33.400 61.981 103.054 68.620 56.236 71.812 1800

1900 33.400 65.321 10_.860 70.681 59.576 73.506 1900

2000 35.600 68.661 106.573 72.245 62.916 75.115 2000

2100 33.400 72.001 108.203 73.917 66.256 76.652 2100

2200 33.400 75,361 109.756 75.511 69.596 78.122 2200

2300 33.600 78.681 111.241 77.032 72.936 79.550 2300

2400 33._00 82.021 112.663 78.687 76+276 80,881 2400

2500 33.400 85.361 114.026 79.882 79.616 82.180 2500

2600 53.400 88.701 115.336 81.220 82.956 85.430 2600

2700 33.400 92.041 116,597 82.507 86,296 84.635 2700

2800 35.600 95.381 117.811 83.747 89.636 85.798 2800

2900 33.400 98.721 118.983 84.942 92.976 86.9?3 2900

3000 33.400 102,061 120.116 86.095 96,316 88.010 3000

3100 33,_00 105.401 121,211 87.211 99.656 89.066 3100

3200 35.000 108.761 122.271 88.290 102.996 90.085 5200

3300 35.400 112.081 123.299 89.335 106.336 91.076 3300

3400 33.400 115.421 126.296 90.369 109.676 92.038 3400

5500 33.400 118.761 125.266 91.333 113.016 92.974 5500

_600 33,400 122.101 126.205 92.288 116.356 95.884 3600

3700 33._00 125.661 127.120 93.217 119.696 96.770 3700

5800 35.400 128.781 128.011 96.121 125.036 95.633 3800

3900 33._00 132.121 128.879 95.001 126.376 96.675 3900

4000 33.400 135.461 129.724 95.859 129.716 97,295 4000

_100 35.400 138.801 130.549 96.695 135.056 98.096 6100

_200 33.400 162.141 131.356 97.511 236.396 98.879 6200

_300 33._00 165.681 132,140 98.307 139.736 99.643 4500

_00 3_ _00 168.821 152.908 99.085 165.076 100.590 6600

4503 3_._00 152.161 133.656 99.865 146.616 101.121 6500

_603 5_&00 155.501 136.392 100.588 169.756 101,837 6600

_700 33 _00 158.841 135.111 101.315 153.096 102.557 6700

_0O 3_._00 162,181 135.814 102,026 156,636 103.223 6800

_qO0 35,_00 165.521 136.502 102,723 159,776 103.895 4900

5000 5_._00 168.861 137.177 103.405 163.116 106.554 5000

5100 33.400 172.201 137.839 104.076 266.656 105.200 5100

5200 33,600 175.541 138.487 104.729 169.796 105.836 5200

5300 33.600 178.881 139.123 105.572 175.136 106.656 5300

5600 35.400 182,221 139.768 106.003 176.476 107.067 5600

5500 33.400 185.561 140.361 I06.622 179.816 107.667 5500

5600 33.400 188.901 140.962 107.230 185.156 108.256 5600

5700 33.400 192.241 141.556 107.827 186.696 108.835 5700

5800 33.600 195.581 142.134 108.614 189.856 109.406 5800

5900 33.600 198.921 142.705 108.990 195.176 109.964 5900

6000 33.400 202.261 143.267 109.557 196.516 110.516 6000

14 NASA/TP-3287/REV 1
TABLE )11.2• SELECTED THERMODYNAMIC FUNCTIONS FOR Al(cr,#)

T C° Ho(T).HO(0) so(.D .{GOC0.HO(0)}_ Ho(T) .G°('DG T

K J/m_-K kJ/mol J/moI-K J/mo6K kJ/rnol JIm_-K K

0 0.000 0.000 0,000 0,000 -4.540 INFINITE 0

I00 12.996 0.485 6.983 2.133 -4.055 47.533 I00

200 21.340 2.284 19,140 7.720 -2.256 30.420 200

298.15 24.200 4.540 28,300 13.073 0,000 28,300 298.15

300 24.234 4.585 28.450 15.167 0,045 28,300 300

400 25.735 7.088 35.639 17.919 2.548 29.269 400

500 26.911 9.721 41.511 22.069 5.181 31.149 500

600 28.043 12.468 46.517 25.737 7.928 33,304 600

700 29.345 15.336 50.934 29.025 10.796 35.511 700

800 31.006 I_.349 54.956 32.020 15.809 57.695 800

900 33,210 21.555 58.729 34.779 17.015 39.823 900

cr 9 3.61 54.105 22.686 59.963 35.664 18.146 40.527 933.61

; -31;50"- 33h6 ;;7;;; ...... 93 ;6;

1000 31.750 35.494 73.605 38.111 30.954 42.651 1000

1100 31.750 38.669 76.631 41.478 34.129 _5.605 1100

1200 31.750 41.844 79.394 44.524 37.304 48.307 1200

1300 31.750 45.019 81.935 47.305 40.479 50.797 1300

1400 31,750 48.194 8_,288 49.86_ 43.654 53.107 1400

1500 31.750 51.369 86.479 52.233 _6.829 55.259 1500

1600 31.750 54.54_ 88.528 54.438 50,004 57.275 1600

1700 31.750 57.719 90.452 56.500 53.179 59.171 1700

3_00 31.750 60.894 92,267 58.437 56.35_ 60.960 1800

1900 31.750 64.069 93.984 60.263 59.529 62.653 1900

2000 31.750 67.244 95.612 61.990 62.704 6_.260 2000

2100 31.750 70.419 97.162 63.629 65.879 65.791 2100

2200 31.750 73.594 98.639 65.187 69.054 67,250 2200

2300 31.750 76.769 100.050 66,672 72,229 68.646 2300

2400 31.750 79.944 101.401 68.091 75.Q04 69.985 2400

2500 31.750 83,119 102.697 69.450 78.579 71,266 2500

2600 31.750 86.294 103.942 70.753 81.754 72._99 2600

2700 31.750 89._69 105,141 72.004 84.929 73.686 2700

2800 31.750 92.644 106.295 73.208 88.104 74.830 2800

2900 31.750 95.819 107.410 74.369 91.279 75.934 2900

3000 31.750 98.994 108.486 75.488 94,454 77.001 3000

3100 31.750 102.169 109.527 76.569 97.629 78.034 3100

3200 31.750 105.344 110.535 77.615 100.804 79.034 3200

3300 31.750 108.519 111.512 78.628 103.979 80.003 3300

3_00 31.750 111.694 112.460 79.609 107.154 80.944 3400

3500 31.750 114.869 113.380 80.561 110.329 81.858 3500

3600 31.750 118.044 114.275 81.485 113.504 82.746 3600

3700 31,750 121,219 115.145 82.383 116.679 83.610 3700

3800 31.750 12_.394 115.99] 83.256 119.854 84.451 3800

3900 31.750 127.569 116.816 84.106 123.029 85.270 3900

4000 31,750 130.744 117.620 84,934 126.204 86.069 4000

_io0 31.750 133.919 I18.40_ 85.741 129.379 86.848 4100

4200 31,750 ]37.094 ]19.169 86.528 152.554 87.608 4200

4300 31.750 140.269 119.916 87_295 135.729 88.351 4300

4_00 31.750 143.444 120,646 88.045 138.904 89.077 4400

4500 31.750 146.619 121.359 88.777 142.079 89.786 4500

4600 31.750 149.794 122,057 89.493 145.25_ 90.480 4600

4700 31.750 152.969 122.740 90.194 I_8.429 91.159 _700

4800 31.750 156.144 123.409 90.879 151.604 91.82_ 4800

_900 31.750 159.319 124.063 91.549 15_.779 92.476 4900

5000 31.750 162.494 124.705 92.206 157.954 95.11_ 5000

5100 31.750 165.669 125.333 92.849 161.129 93.739 5100

5209 31.750 168.844 125.950 93.480 164.304 94.353 5200

5300 31.750 172.019 126.555 94.098 167._79 94.955 5300

5400 31.750 175.194 127.148 94.705 170.654 95.546 5400

5500 31.750 178.369 127.731 95.300 173.829 96.126 5500

5600 31.750 181.544 128.303 95.884 177.004 96.695 5600

5700 31.750 184.719 128.865 96.458 180.179 97.254 5700

5800 31.750 187.894 129.417 97.021 183.354 97.804 5800

5900 31.750 191.069 129.960 97.575 186.529 98.345 5900

6000 31.750 194.244 130.493 98.119 189.704 98.876 6000

NASA/TP-3287/REV 1 15
TK

0

I00

200

298

300

400

5O0

600

700

8O0

9O0

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

52O0

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

,15

TABLE 1ft.3,- SELECTED THERMODYNAMIC FUNCTIONS FOR Ar

C° H°(T).H°(0) S°(T) -{GOO).H°(O)}_ H°(T)

Jln_K kJ/rnol J/moi-K J/mot-K kJ/mol

0.000 0.000 0.000 0.000 -6.197

20.786 2.079 132.139 111.353 -4.119

20.786 4.157 146.547 125.761 -2.040

20.786 6.197 154.847 134.060 0.000

20.786 6.236 154.975 134.189 0.038

20.786 8.315 160.955 140.169 2.117

20.786 10.393 165.593 144.807 4.196

20.786 12.472 169.383 148.597 6.274

20.786 14.550 172.587 151.801 8.353

20.786 16.629 175.363 154.577 10.432

20.786 18.708 177.611 157.025 12.510

20.786 20.786 180.001 159.215 14.589

20.786 22.865 ]81.982 161.196 16.667

20,786 24.944 183.791 163.005 18.746

20.786 27.022 185.455 164.669 20,825

20.786 29.101 186.995 166.209 22.903

20.786 31.179 188.429 167.643 24.982

20.786 33.258 189.771 168.985 27.061

20.786 35.337 191.031 170.245 29.139

20.786 37.415 192,219 171.433 31.218

20.786 39.494 193.343 172.557 33.296

20.786 41.573 194.409 173.623 35.375

20.786 43.651 195.423 174.637 37.454

20.786 45.730 196.390 175.604 39.532

20.786 47.808 197.314 176.528 41.611

20.786 49.887 198.199 177.413 43.690

20.786 51.966 199.048 178.261 45.768

20.786 54.044 199.863 179.077 47.847

20.786 56.123 200.647 179.861 49.926

20.786 58.202 201.403 180.617 52.004

20.786 60.280 202.133 181.346 54.083

20.786 62.359 202.837 182.051 56.161

20.786 64.437 203.519 182.733 58.240

20.786 66.516 204.179 183.393 60.319

20.786 68.595 204.819 184.032 62.397

20.786 70.673 205.439 184.653 64.476

20.786 72.752 206.042 185.255 66.555

20.786 74.831 206.627 185.841 68.633

20.786 76.909 207.197 186.410 70.712

20.786 78.988 207.751 186.965 72.790

20.786 81.066 208.291 187.505 74.869

20.786 83.145 208.817 188.031 76.948

20.786 85.224 209.331 188.544 79.026

20,786 87.302 209.831 189.045 81.105

20.786 89.381 210.321 189.534 83.184

20.786 91.460 210.798 190.012 85.262

20.786 93.538 211.266 190.479 87.341

20.786 95.617 211.722 190.936 89.419

20.786 97.695 212.169 191.383 91._98

20.786 99.774 212.607 191.821 93.577

20.786 101.853 213,036 192.249 95.655

20.786 103.931 213.456 192.669 97.734

20.786 106.010 213.667 193.081 99.813

20.786 108.089 214.271 193.485 101.891

20.786 110.167 214.667 193.880 103.970

20,786 112.246 215,055 194.269 106.048

20.786 114.325 215.437 194.650 108.127

20.786 116.403 215.811 195.025 110.206

20.786 118.482 216.179 195.393 112.284

20.786 120.560 216.541 195.754 114.363

20.786 122.639 216.896 196.110 116.442

20.786 12_.718 217.245 196.459 118.520

20.786 128.875 217.927 197.141 122.677

20.786 133.032 218.587 197.801 126.835

20,786 137.189 219.227 198.440 130.992

20.786 141.347 219.847 199.061 135.149

20.787 145.504 220.450 199.663 139.307

20.787 149.661 221.035 200.2_9 143.464

20.787 153.819 221.605 200.818 147.621

20.787 157.976 222.159 201.373 151.779

20,788 162.134 222.699 201,913 155.936

20.789 166.291 223.225 202.459 160.09_

J/m_.K

INFINITE

173 327

156 748

154 847

154 847

155 662

157 202

158.926

160.655

162.324

163.911

165.413

166.830

168.169

169.436

170.636

171.775

172.858

173.890

174.876

175.819

176.722

177.588

178.421

179.223

179.995

180.740

181.460

182.156

182.830

183.483

184.117

184.732

185.329

]85,910

186,476

187.026

187.562

188.085

188.596

189.094

189.580

190.056

190.521

190.976

191.421

191.856

192,283

192,702

193.112

193.514

193.909

194.296

194.676

195.050

195.417

195.777

196.132

196.480

196.823

197.160

197.492

]98.140

198.769

199.379

199.972

200,549

201.110

201.656

202.188

202.707

203.21_

TK0

100

200

298.15

3O0

400

500

600

700

80O

900

1000

llO0

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

16 NASA/TP-3287/REV1
TABLE fit3. - Cor_udect

T C° H°_) "H°(0) S°(T) "{G°(T)'H°(0)}K

K J/m_-K kJ/mol J/mol-K J/moI-K

8200 20.790 170.449 223.739 202.952

8400 20.792 174.607 224.260 203.653

8600 20.796 178.766 224.729 203.962

8800 20.797 182,925 225.207 206.420

9000 20.802 187.085 225.674 204.887

9200 20.807 191.246 226.132 205.344

940D 20.815 195.408 226.579 205.791

9600 20.826 199.572 227.018 206.229

9800 20.837 203.738 227.647 206.658

10000 20.848 207.904 227.868 Z07.078

10500 20.900 218.560 228.886 208.092

11000 20.981 228.806 229.860 209.059

11500 21.106 239.322 230.795 209.986

12000 21.275 249.904 231.696 210,870

12500 21.511 260.582 232.567 211.721

15000 21.866 271.411 233.417 212.539

13500 22.299 282.442 234.249 213.527

iq000 22.882 293.725 235.070 214.089

14500 23.546 305.245 235.878 214.826

15000 24.276 317.011 236.674 215,540

15500 25.245 329.315 237.481 216.235

16000 26.450 342.230 238.301 216.911

16500 27.859 355.799 239.136 217.572

17000 29.367 369.892 259.976 218.217

17500 30.985 384.696 240.832 218.850

18000 31.768 398.206 241.580 219.457

18500 33,687 614.558 242.476 220.067

19000 55.495 431.259 243.362 220.665

19500 36.527 G66.638 264.165 221,261

20000 37.320 461.844 244.895 221.802

HO(T)

kJ/tool

164.252

168.610

172.568

176.728

180.888

185.048

189.210

193.374

197.560

201.707

212.162

222.609

233.126

243.707

254.385

265.213

276.245

287.528

299.048

310.813

323.117

336.033

349.601

363.694

578.496

392.009

408.361

425,041

440.441

455.647

.O°F0/T

J/moI-K

203.708

204.191

204.663

205,124

205.576

206.018

206.450

206.87_

207.290

207,697

208,682

209,623

210.523

211.387

212.216

213.015

213,787

216.532

215.254

215.953

216.636

217.299

217.948

218.582

219.206

219.802

220.402

220.991

221.559

222.112

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

lOSO0

110o0

11500

12000

12500

13000

13500

16000

16500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

Z0000

NASA/TP-3287/REV 1 17
TABLE IliA, . SELECTED THERMODYNAMIC FUNCTIONS FOR B(8,J)

T C°,., H°Fr')-H°(O) S°(T)

K J/rn_l-K kJ/m_ _rnol-K

0 0 000 0.000 0.000

100 i _076 0. 024 0. 308

110 1.421 0.037 0.426

130 2.250 0.073 0.728

150 3,227 0,127 1,117

160 3.755 0.162 1.342

180 4.859 0.248 1.848

200 5.998 0.357 2.419

210 6.571 0.420 2.725

250 7,708 0.563 3.374

250 8,821 0,728 4,063

260 9.363 0.819 4.619

290 10,916 1.123 5.526

298.15 11,315 1.214 5,834

300 11,405 1.235 5.904

310 11.878 1.351 6,286

330 12,77_ 1.598 7.057

350 15.654 1.862 7.854

400 15.693 2.598 9.796

_50 17.361 3.425 11.74Z

500 18,722 4.529 13,644

550 19,843 5.294 15,485

600 20.778 6.310 17.251

650 21.569 7.369 18,946

700 22.249 8,465 20.570

750 22.840 9.592 22.125

800 23.361 10.748 23.617

850 23.826 11.928 25,047

900 24.245 13,129 26.421

950 24,627 14,351 27.742

1000 24.978 15.592 29.014

1050 25.303 16,849 30.241

1100 25.606 18.122 31.625

1150 25.891 19.409 32.570

1200 26,161 20.710 33.677

1250 26,418 22.025 34,751

1300 26.665 23.352 35.792

1350 26.898 24.691 36.802

1400 27.125 26.042 37.785

1450 27.344 27.403 38,740

1500 27.557 28.776 39,671

1550 27.764 30.159 40.578

1600 27.966 51.552 41.463

1700 28.356 34.369 _3.170

1750 28.546 35.791 43.995

1800 28.732 37.223 44.801

1850 28,916 38.664 45,591

1900 29.097 40.115 46.365

1950 29.275 41.574 47.123

2000 29.452 45.042 _7.866

2050 29.626 44.519 68.596

2100 29.799 _6.005 49,312

2150 29.970 _7.499 50.015

2200 30.140 49.002 50.706

2250 30.308 50.513 51.385

2300 30.475 52.033 52.053

ff 2350 30.641 55.560 52.710

-(o°cr).H°(O)}_

J/m_-K

D.DO0

0,068

0.090

0.166

0.270

0 330

0 470

0 654

0 725

0 926

1 151

1 269

1 654

1 762

1 787

1 928

2 215

2 514

3 299

4 131

4 986

5 858

6 734

7 609

8 477

9 336

lO 182

11 014

11,833

12.636

13,622

14,194

14.950

15.693

16.419

17.131

17.829

18.512

19,184

19,841

20,487

21,121

21.743

22.955

23.543

24.122

24.692

25.252

25.803

26.565

26.879

27.405

27.922

28.432

28.935

29.450

29.919

H°('r) _°0")_ T

kJ/m_ J/mol-K K

-1.214 INFINITE 0

-1.190 12,208 i00

-1.177 ii,126 110

-1.141 9.505 130

-1.087 8.364 150

-I.052 7.917 160

-0,966 7.215 180

-0.857 6,704 200

-0.794 6.506 210

-0.651 6.204 230

-0.486 6.007 250

-0.395 5.938 260

-0,091 5.840 290

0.000 5.834 298

0.021 5.834 300

0.137 5.844 310

0.384 5.893 330

0.648 5.983 350

1.384 6.354 400

2.211 6.829 450

3.115 7.414 500

4.080 8.065 550

5.096 8.758 600

6,155 9.477 650

7.251 10.211 700

8.378 10.954 750

9.534 11.700 800

10,714 12.442 850

11,915 13.182 900

15.137 13.91_ 950

14,378 14.636 I000

15.635 15.351 1050

16.908 16.054 1100

18.195 16.748 1150

19,496 17.430 1ZOO

20.811 18.102 1250

22.138 18.765 1300

23,477 19.412 1350

24.828 20.051 1400

26.189 20.679 1450

27.562 21.296 1500

28.945 21.904 1550

30.538 22.502 1600

33.155 25.667 1700

34.577 24.237 1750

36.009 24.796 1800

37.450 25.568 1850

38.901 25.891 1900

40.360 26,426 1950

41.828 26,952 2000

43.305 27.472 2050

44.791 27.985 2100

46.285 28.487 2150

47,788 28,984 2200

49.299 29.474 2250

50,819 29.958 2300

52.346 30.435 2350

.15

t 2350 31.750 103.768 74.075 29,919 102.554 30.435 2350

2400 31.750 105.355 74.744 30.845 104,141 31.351 2400

2500 31.750 108.530 76,040 32.627 107.316 33.113 2500

2600 31.750 111.705 77.285 34.321 110.491 34.788 2600

2700 31.750 114,880 78.485 35.935 115.666 36.384 2700

2800 31.750 118.055 79.638 37.475 116.841 37.909 2800

2900 31.750 121.230 80.752 38.948 120.016 59.367 2900

3000 31.750 124.405 81.828 40.360 125.191 40.765 3000

3100 31.750 127.580 82.869 41.714 126,366 42.106 3100

3200 31.750 130.755 83.877 43.016 129.541 43.396 3200

3300 31.750 133.930 84.854 44.269 132.716 4_.637 3300

3400 31.750 137.105 85.802 45.477 135.891 45.834 3400

3500 31.750 140.280 86.723 46.643 139.066 46.989 3500

3600 31.750 143.455 87.617 47.768 142.241 48.106 3600

3700 31.750 146.630 88.487 48.857 145.416 49.185 3700

3800 31.750 149.805 89.334 49.911 148.591 50.231 3800

3900 51.750 152.980 90.158 50.933 151.766 51.244 3900

_000 31.750 156.155 90.962 51.923 15_.941 52.227 4000

18 NASA/TP-3287/REV 1
T

K

4100

4200

4500

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

C°

J/t_l-K

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31,750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

31.750

TABLE IliA.• CoNclude¢l.

Ho(T).HO(o) So(F) .{GO(T).Ho_)}K Ho(-('_ _°('I")K T

kJ/mot J/moI-K Jtmot-K kJ/mol J/m_K K

159.330 91.746 52.885 158.116 53.181 4100

162.505 92.511 53.820 161.291 59.I09 9200

165.680 93.258 54.728 164.466 55.010 4300

168.855 93.988 55.612 167.641 "55.888 4400

172.030 94.702 56.473 170.816 56.743 4500

175.205 95.400 57.312 173.991 57.575 4600

178.380 96.083 58.129 177.166 58.388 4700

181.555 96.751 58.927 180.341 59.180 4800

184.730 97.406 59.706 183.516 59.953 4900

187.905 98,047 60.466 186.691 60.709 5000

191.080 98.676 61.209 189.866 61.447 5100

194.255 99.292 61.936 193.041 62.169 5200

197.430 99.897 62.646 196.216 62.875 5300

200.605 100.491 63.341 199.391 63.566 5400

203,780 101.073 64.022 202.566 64.243 5500

206.955 I01,645 64.689 205.741 64.906 5600

210.130 102.207 65.342 208.916 65.555 5700

213.305 102.759 65.983 212.091 66.192 5800

216.480 103.302 66.611 215.266 66.816 5900

219.655 I03,836 67.227 218.441 67.429 6000

NASA/TP-3287/REV 1 19
TABLEIlL5 . SELECTED THEF_tODYNAMtC FUNCTIONS FOR Ba(cr,I)

T cO H°('T)°H°_) S°(T) °{G°('T)-H°(0)}_ H°(T) -G°('1")_ T

K _(_K kJ/mol J/mokK J/mo_.K kJ/mo_ J/mot-K K

0 0.000 0.000 0.000 0.000 -6.907 INFINITE 0

20 9.249 0.059 _.069 1.139 -6.848 3_6._88 20

30 15.017 0.183 9.021 2.932 -6.72_ 233.165 30

40 18.474 0,352 13.85_ 5.066 -6.555 177.741 40

50 20.611 0.548 18.225 7.269 -6.359 1_5.409 50

60 21.907 0.761 22.108 9._25 -6.146 124.542 60

70 22.728 0.984 25.550 11.488 -5.923 110.159 70

80 23.435 1.215 28.629 13.441 -5.692 99.779 80

90 23.904 1.452 31.418 15.286 -5.455 92.031 90

I00 24.280 1.693 33.956 17.028 -5.214 86.098 100

120 24.861 2.185 38.437 20,233 -_.722 77.791 120

140 25.313 2.686 42.305 23.116 -4.221 72,_52 140

160 25.695 3.197 _5.710 25,732 -3,710 68,900 160

180 26.038 3.71q 48.757 28.124 -3.193 66.496 180

200 26,363 4,238 51.517 30.527 -2.669 64.862 200

220 26.686 q.768 54.045 32.370 -2.139 63.766 220

2_0 27.016 5,305 56.381 34,275 -1.602 63.054 240

260 27.36_ 5.849 58.557 36.060 -1,058 62.625 260

280 27.740 6.400 60.598 37.741 -0,507 62.408 280

298.15 28.110 6.907 62.352 39.186 0.000 62.352 298.15

300 28.141 6.959 62.526 39.329 0.052 62.353 300

350 28.988 8.387 66.928 42.964 1.480 62.698 350

400 29.835 9.858 70.854 46.209 2.951 63.477 400

450 30.682 11.371 74._17 49.148 4,_6_ 6_.497 450

500 31.529 .12.926 77.693 51.8_1 6.019 65.655 500

600 33.224 16.164 83.592 56.652 9.257 68.164 600

700 34.918 19.571 88.8_0 60.882 12,664 70.749 700

800 36.612 23.147 95.613 64.679 16.240 73.313 800

900 38.306 26.893 98.023 68.142 19.986 75.817 900

cr 1000 _0.000 30.808 102.147 71.339 23.901 78.246 1000

...... ;;7;;; ...... ..... ...... ...... ;;7;;; ...... ......

1100 _0.000 42,658 113.809 75.029 35.751 81.308 1100

1200 40.000 46.658 117.290 78.408 39.751 8_.164 1200

1300 _0.000 50.658 120.492 81.52_ 43,751 86.837 1300

1400 40.000 54.658 123.456 84.414 47.751 89.348 lq00

1500 40.000 58.658 126.216 87.110 51.751 91.715 1500

1600 40.000 62.658 128.797 89.636 55.751 93.955 1600

1700 40,000 66.658 131.222 92.011 59.751 96,07_ 1700

1800 40.000 70.658 133,509 94.254 63.751 98.091 1800

1900 40.000 74.658 135.671 96.377 67.751 100.013 1900

2000 40.000 78.658 137.723 98.394 71.751 101,847 2000

2100 40.000 82.658 139.675 100.313 75,751 103.602 2100

2200 40.000 86,658 1_1.535 102.1_5 79.751 105.285 2200

2300 _0.000 90.658 143.313 103.897 83.751 106.900 2300

2400 40.000 9_.658 145,016 105.575 87.751 108.453 2400

2500 40.000 98.658 146.649 107.185 91.751 109.948 2500

2600 _0,000 102.658 148.218 108.734 95.751 111.390 2600

2700 40.000 106.658 1_9.727 110.224 99.751 112.782 2700

2800 40.000 110.658 151.182 111.661 103.751 114.128 2800

2900 40.000 11_.658 152.586 113.048 107.751 115.430 2900

3000 40.000 118.658 153.942 11_.389 111.751 116.691 3000

3100 40.000 122.658 155.253 115.686 115.751 117.914 3100

3200 40.000 126.658 156.523 116.942 119.751 119.101 3200

3300 40.000 i30.658 157.754 118,161 123.751 120.254 3300

3400 40.000 134.658 158.948 119.343 127.751 121.37_ 3400

3500 40.000 138.658 160.108 120.491 131.751 122.464 3500

3600 40,000 1_2.658 161.234 121.607 135.751 123.526 3600

3700 40.000 146.658 162.330 122.693 139.751 124.560 3700

3800 40.000 150,658 163.397 123.750 143.751 125.568 3800

3900 40.000 15_.658 16_.436 124.780 147,751 126.551 3900

_000 40.000 158.658 165.449 125.784 151.751 127.511 4000

_100 _0.000 162.658 166.437 126.764 155.751 128.448 4100

4200 40.000 166.658 167._00 127.720 159.751 129.36_ 4200

_300 40.000 170.658 168.342 128.654 163.751 130.260 4300

4400 40.000 174.658 169.261 129.566 167.751 131.136 4400

4500 40.000 178.658 170.160 130.458 171.751 '131.993 4500

_600 40.000 182.658 171.039 131.331 175,751 132.832 _600

4700 40.000 186.658 171.900 132.185 179.751 133.655 4700

4800 qO.O00 190.658 172.742 133.021 183.751 134.460 _800

4900 _0.000 194.658 173.566 133.8_0 187.751 135.250 4900

5000 40.000 198.658 174.375 134.643 191.751 136.024 5000

20 NASA/TP-3287/REV 1
TABLE lU.5,- Concluded.

T C° H°_ "H°(0) S°_ "{G°(T)'H°(0}}K

K J/m_-K kJ/mol J/m_-K J/moI-K

5100 40.000 202.658 175.167 135.430

5200 40.000 206,658 175.943 136,201

5500 40.000 210.658 176.705 136.958

5400 40.000 21_.65B 177,453 1371701

5500 qO,O00 218.658 178.187 138.431

5600 40.000 222.658 178.908 139.147

5700 _0.000 226.658 179.616 139.851

5800 40,000 230,658 180.311 140.543

5900 40.000 234.658 180,995 141.223

6000 40.000 23B.&58 181.667 141,891

H°(T)

k_mot

195.751

199.751

203.751

Z07.751

211.751

215.751

Z19.751

223,751

227.751

231.751

_moI-K

136.784

137.530

138.262

138.951

139,687

140,381

141,063

141,734

142.593

143.042

T

K

5100

5200

5500

5406

5500

5600

5700

5800

5900

6000

NASA/I'P-3287/REV 1 21
T

K

0

4O

50

6O

70

8O

90

100

120

140

160

180

Z00

220

240

260

280

298.15

3O0

350

400

45O

5OO

6OO

700

80O

9OO

1000

1100

1200

1300

1400

1500

a 1543

C °

J/n_K

0.000

0.089

0.191

0.309

0.509

0.818

1.251

1.738

3.216

4.910

6.652

8.364

10.003

11.546

12.978

14.291

15.478

16 443

16 473

18 521

19 965

21 061

21 943

23.336

24.463

25.458

26,584

27.274

28.147

29.015

29.885

30.762

31.649

32.035

TABLE111.6- SELECTED THERMODYNAMIC FUNC'rlONS FOR Be(a,8.#)

H°(T)-H°(0) S°(T) -{G°('r)-H°(O)}K

_/m_ _m_-K J/mokK

0.000 0.000 0.00O

0.001 0.025 0.007

0.002 0.057 0.014

0.005 0.101 0.024

0.009 0.162 0,039

0.015 0.249 0.060

0,025 0.369 0.087

0.041 0.529 0.123

0.090 0.971 0.225

0.171 1.593 0.574

0.286 2.362 0.573

0.437 3.245 0.820

0,620 _.212 i.II0

0.836 5.238 1.438

1.081 6.305 1.799

1.354 7.397 2.188

1.652 8,500 2.599

1.942 9.503 2.989

1.972 9.604 3.029

2.851 12.308 4.163

3.815 14.880 5.343

4.841 17.297 6.539

5.917 19.564 7.729

8.184 23.693 10.053

10.576 27.377 12.269

13.073 30.710 14.369

15.665 33.762 16.357

18.348 36.588 18.240

21.119 39.229 20.030

23.977 41.715 21.734

26.922 44.072 23.363

29.955 46.319 24.923

33.075 48,471 26.421

34.444 49,371 27.048

HoG

_lmol

-1.942

-1.941

-1.940

-1.937

-1.933

-1 927

-1 917

-1 901

-i 853

-1 771

-1 656

-i 506

-I 322

-I lO6

-0.861

-0.588

-0.290

o,000

0.030

0.909

1.873

2.899

3.975

6,242

8,634

11,131

13.723

16.406

19.177

22.035

2_.980

28.013

31.133

32.502

-G°(T)K T

JlmokK K

INFINITE o

48.559 40

38.855 50

32.392 60

27.783 70

24.336 80

21.666 90

19.544 100

16.409 120

14.246 140

12.711 160

11.609 180

10.821 200

10.266 220

9.891 240

9.657 260

9,535 280

9.503 298.15

9.503 300

9.712 350

10.199 400

10.855 450

11.613 500

13.289 600

15.044 700

16.797 800

18.515 900

20.182 I000

21.795 1100

23.353 1200

24.856 1300

26.310 1400

27.716 1500

28.307 1543

# 1563 29.480 49.744 59.218 27.392 47,802 28.635 1563

1600 29.480 50.835 59.908 28.136 48.893 29.350 1600

1700 29.480 53.783 61,695 30.058 51.841 31.200 1700

1800 29.480 56,731 63.380 31.863 54.789 32.9_2 1800

1900 29.480 59.679 64.974 33.564 57.737 34.586 1900

2000 29.480 62,627 66.686 35.173 60.685 36.144 2000

2100 29.480 65.575 67,925 36.698 63.633 37.623 Zl00

2200 29.480 68.523 69.296 38.149 66.5CI 39.032 2200

2300 29.480 71,471 70,606 39.532 69.529 40.376 2300

2400 29.480 74.419 71.861 40,853 72.477 41.662 2400

2500 29.480 77.367 73.065 42.118 75.425 42.895 2500

2600 29.480 80.315 74.221 43.330 78.373 44.077 2600

2700 29.480 83.263 75.333 44.495 81.321 45.214 2700

2_00 29.480 86.211 76.405 45.616 84.269 46.309 2800

2900 29.480 89.159 77.440 46.695 87,217 47.365 2900

3000 29.480 92.107 78.439 47.737 90.165 48.384 3000

3100 29.480 95.055 79,406 48.743 93.115 49.370 3100

3200 29.480 98.003 80.342 49.716 96.061 50.323 3200

3300 29.480 100.951 81.249 50.658 99.009 51.246 3300

3400 29.480 103.899 82.129 51.571 101.957 52.142 3400

3500 29.480 106.847 82.984 52.456 104.905 53.011 3500

3600 29.480 109.795 83.814 53.316 107.853 53,855 3600

3700 29.480 112.743 84.622 54.151 110.801 54.676 3700

3800 29.480 115.691 85.408 54.963 113.749 55.474 3800

3900 29.480 118.639 86.174 55.754 116.697 56.252 3900

_000 29.480 121.587 86.920 56.523 119.645 57.009 4000

qlO0 29.480 124.535 87.648 57.274 122.593 57.747 4100

4200 29.480 127.483 88.359 58.005 125.541 58.468 4200

4300 29,480 130.431 89.052 58.719 128.489 59.171 6300

q400 29.480 133.379 89.730 59.417 131.437 59.858 4400

4500 29.480 136.327 90.392 60.098 134.385 60.529 4500

4600 29.480 139.275 91.040 60.763 137,333 61.185 4600

4700 29.480 142.223 91.674 61.414 140.281 61.827 4700

4800 29.480 145.171 92.295 62.051 143.229 62.456 4800

4900 29.480 148,119 92.903 62.675 146.177 63.071 6900

5000 29.480 151.067 93.499 63.285 149.125 63.674 5000

22 NASA/TP-3287/REV l
TABLE Iil.6.- Concluded.

T C° HO(T)'H°(0) sO(T) "{G°(T)-H°(O)}K

K J/m_l-K kJ/mol Jlmot-K J/mobK

5100 29.480 154,015 94.082 63.883

5200 29.480 156.963 94.655 64.470

5300 29.480 159.911 95.216 65.044

5400 29.480 162.859 95.767 65.608

5500 29.480 165,807 96.308 66.162

5600 29._80 168.755 96.839 66.705

5700 29.480 171.703 97.361 67.238

5800 29.480 174.651 97.874 67.762

5900 29._80 177.599 98.378 68.276

6000 29.480 180.547 98.873 68.782

H°_)

kJ/mo!

152,073

155.021

157.969

160.917

163.865

166.813

169.761

172.709

175.657

178.605

.G°mK

J/m_-K

64.264

64.843

65.411

65.968

66.515

67.051

67.579

68,097

68,605

69.106

T

K

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV 1 23
T

K

0

5

IO

15

20

25

30

35

40

45

50

60

70

BO

90

lO0

110

12o

13o

14o

150

160

170

18o

190

2oo

210

220

230

240

250

260

cr 265.90

C °

J/mgt-K

0.000

0.330

2.56O

7 220

12 720

18 030

22 440

26 050

28 990

31 380

33 3qO

36 330

38.610

40.510

42.150

43.600

_4.890

46.070

47. 170

48.200

49.180

50.130

51.050

51.950

52.850

53.770

54.710

55.710

56.780

57.940

59. 230

60.690

61.640

TABLE 1_1.7.- SELECTED THERMODYNAMIC FUNC'RONS FOR _2(cr,

H°(3_-H°(0}

kJ/tool

0.000

0.000

0. 007

0.030

0.080

0 157

0 258

0 380

o 518

0 669

0 831

1 180

I 555

1.950

2.364

2.793

3.235

3.690

cl.156

4.633

5.120

5.616

6. 122

6.637

7.161

7.694

8.237

8.789

9.351

9.924

10.510

11.110

ii ._71

S°(T) -{G°(T).H°(0)}K H=(q

J/mol-K J/moI-K kJ/mol

0.000 0.000 -24.520

0.111 0.029 -2_.520

0.879 0.179 -24.513

2,728 0.728 -24,090

5.543 1.543 -24._40

8.955 2.675 -24,363

12.641 4,041 -24,262

16.379 5.522 -24.140

20.055 7.105 -24.002

23.612 8.745 -23.851

27.023 10.403 -23,689

$3.381 13.714 -23.340

39.161 16.947 -22.965

44.445 20.070 -22.570

49,315 23.048 -22.156

53.833 25.903 -21.727

58.053 28.644 -21.285

62.014 31.264 -20.830

65.747 33.778 -20,364

69.283 36.190 -19.887

72,644 88,511 -19,400

75,850 40.750 -18.904

78.917 42.905 -18.398

81.862 44.990 -17.883

84.696 47.007 -17.359

87.431 48,961 -16,826

90.077 50.853 -16.283

92.645 52.695 -15.731

95.144 54.487 -15.169

97.584 56.234 -14.596

99.976 57.936 -14.010

102.329 59.598 -13.410

103.700 60.560 -13.049

.G°C0/T

J/mot-K

INFINITE

490_.029

2452.179

1635,395

1227.543

983.475

8Z1.374

706,093

620,105

553.634

500.803

422.381

367.232

326.570

295,493

271,I03

251.553

235.597

222.393

211 333

201 977

19_ o00

187 141

181 212

176 059

171 561

167.615

16_.150

161,096

158.401

156.016

153.906

152.775

T

K

0

5

10

15

20

25

3O

35

40

45

50

6O

70

80

90

100

110

120

130

1_0

150

160

170

180

190

200

210

220

230

240

250

260

265.90

| 265.90 77.740 22.043 143.461 60.561 -2.477 152,777 265.90

270 77,350 22.361 144.648 61.829 -2.159 152.644 270

280 76,570 23,131 147._47 64.836 -1.389 152.408 280

290 76.000 23.894 150.125 67.732 -0.626 152.284 290

298.15 75.680 24.520 152.210 69.970 0.000 152.210 298.15

300 75.630 24.661 152.680 70.477 0.141 152.210 300

332.50 75,302 27,110 160.429 78.896 2.590 152.640 332.50

340 75.302 27.675 162.108 80.712 3.155 152.830 340

360 75.302 29,181 166.412 85,355 4.661 153.466 360

380 75.302 30,687 170,484 89,729 6.167 154.256 380

400 75.302 32.193 174.346 93,864 7.673 155.164 400

500 75.302 39,723 191.149 111.703 15.203 160.743 500

600 75.302 47.253 204.878 126.123 22.733 166.990 600

700 75.302 54.783 216.486 138.224 30.263 173.253 700

800 75.302 62.313 226.541 148.650 37.793 179.300 800

900 75.302 69.844 235.411 157.807 45.324 185.051 900

1000 75.302 77.374 243.345 165.971 52.854 190.491 1000

1100 75.302 84.904 250.522 173.336 60.384 195.627 1100

1200 75.302 92.434 257.074 180.045 67.914 200.478 1200

1300 75.302 99.964 263.101 186.205 75.444 205.067 1300

1400 75.302 107.495 268.682 191.900 82.975 209.414 1400

1500 75.302 115.025 273,877 197.194 90.505 213.540 1500

1600 75.302 122.555 278.737 202.140 98.035 217.465 1600

1700 75.302 130.085 283.302 206,781 105.565 221.205 1700

1800 75.302 137.615 287.606 211.153 113.095 224.775 1800

1900 75.302 1_5.146 291.677 215.285 120.626 228,190 1900

2000 75.302 152.676 295.540 219.202 128.156 231,462 2000

2100 75.302 160.206 299.214 222.925 135,686 234.601 2100

2200 75.302 167.736 302.717 226.473 143.216 237.619 2200

2300 75,302 175.266 306.064 229.861 150.746 240.522 2300

2_00 75.502 182.797 309.269 233.104 158.277 243.320 2400

2500 75.302 190.327 312.343 236.212 165.807 246.020 2500

2600 75.302 197.857 315.296 239.198 173.337 248.628 2600

2700 75.302 205.387 318,138 242.069 180.867 251.150 2700

2800 75.302 212.917 320.877 244.835 188.397 253.592 2800

2900 75.302 220.448 323.519 247.503 195.928 255.958 2900

3000 75.302 227.978 326.072 250.080 203.458 258.253 3000

3100 75.302 235.508 328.541 252.571 210.988 260.481 3100

3200 75.302 243.038 330.932 254.983 218.518 262.645 3200

3300 75.502 250.568 333.249 257.319 226.048 264.750 3300

3400 75.302 258.099 335.697 259.586 233.579 266.798 3400

3500 75.302 265.629 337.680 261.786 241.109 268.792 3500

3600 75.302 273.159 339.801 263,924 248.639 270.735 3600

3700 75.302 280.689 341.865 266.003 256.169 272.630 3700

3800 75.302 288.219 343.873 268.026 263,699 274.478 3800

3900 75.302 295,750 345.829 269.996 271.230 276.283 3900

4000 75.302 303.280 347.735 271.915 278.760 278.045 4000

24 NASA/TP-3287/REV 1
TABLE 111.7.- Concluded.

T co Ho_).HO(01 sO(T) .{GO(T).Ho(O)}_ Ho(.r) .G°(T)K T

K J/m_-K kJ/rnol J/m_-K J/mokK _/mol Jlm_-K K

4100 75.302 310.810 349.595 273.787 286.290 279.768 4100

4200 75.302 318.340 351.409 275.614 293.820 281.452 4200

4300 75.302 325.870 353.181 277.397 301.350 283.100 4300

4400 75.302 333.401 354.912 279.139 308.881 284.712 4_00

4500 75,302 340.931 356.605 280.842 316.411 286,291 4500

4600 75.302 348.461 558.26D 282.507 323.94I 287.838 4600

4700 75.302 355.991 359.879 284.136 331.471 289.553 4700

4500 75.502 363.521 361._6_ 285.731 3_9.001 290.839 4800

4900 75.302 371.052 363.017 287.292 546.532 292.296 4900

5000 75.302 378.582 364.538 Z88.822 354.062 293.726 5000

5100 75.302 386.112 366,030 290.321 361.592 295.129 5100

5200 75.302 593.642 367.492 291.791 369.122 296.507 5200

5300 75.302 401.172 368.926 293.233 576.652 297.860 5500

5400 75,302 408.703 370.334 294.648 384.183 299.189 5400

5500 75.302 416.233 371.715 296.037 391.713 300.495 5500

5600 75.302 423.763 373.072 297.400 399.243 301.779 5600

5700 75.302 _31.293 374.405 298.7_0 406.773 303.041 5700

5800 75.302 438.823 375.715 300.056 414.303 304.283 5800

5900 75.302 446.35_ 377.002 301.3_9 421.834 305.505 5900

6000 75.302 453.884 378.268 302.620 429.364 306.707 6000

NASA/TP-3287/REV l 25
T

K

0

20

30

40

5O

6O

7O

8O

9O

100

110

120

130

140

150

160

170

180

190

20O

210

220

23O

240

250

260

27O

273.15

Z80

290

298.15

300

320

340

360

380

qO0

420

440

460

480

500

550

600

650

700

800

900

i000

II00

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

C°

Jlr_l-K

0.000

0.084

0.179

0. 320

0. 502

0.704

0.925

1.163

1.418

1.688

1.972

2.270

2.580

2.901

3.232

3.572

3.920

4. 276

4.637

5.001

5. 365

5.729

6. 092

6. 055

6.816

7.176

7.534

7.646

7 889

8 242

8 528

8 592

9 259

9 922

10 572

II 207

Ii .826

12. 427

13.007

13.566

14. 103

14.616

15.797

16.836

17.744

18. 535

19.829

20.827

21.612

22.2_3

22.763

23.199

23.572

23.897

29.185

24.4_3

24.676

24 891

25 _089

25.275

25.450

25.616

25.773

25. 924

26.070

26.211

26.347

26.480

26.609

26,736

26.860

26.982

27. 102

27.220

27. 337

27.453

27. 568

27.681

27.794

TABLE 1fl.8 - SELECTED THERMODYNAMIC FUNCTIONS FOR C(gr)

H°(T)-H°(O)

kJ/mol

0.000

0.001

0. 002

0. 004

0.008

0.014

0. 023

0.033

0.0co6

0.061

0. 080

0.I01

0.125

0.153

0.183

0.217

0.255

0.296

0,340

0. 388

o 440

0 496

0 555

0 618

0 684

0 754

0 827

0 851

0.904

0.985

1 053

1 069

I 248

1 440

1 645

1 862

2.093

2.335

2,590

2.855

3.132

3.419

4.180

4.997

5.862

6.769

8.690

10.725

12.849

15.043

17. 294

19.592

21.932

24.305

26,709

29.141

31.597

34.076

36.575

39.093

41.630

44.183

46.752

49.338

51.937

54.551

57.179

59.820

62.476

65.142

67. 822

70.514

75.218

75.935

78.662

81.402

84. 153

86.915

89.690

S°(T)

Jtmot-K

0.000

0.041

0,092

0.162

0.252

0.361

0.486

0.625

0.777

0.940

1 .I14

I .298

1.692

1.695

I .906

2. 126

2.353

2.587

2.828

3.075

3. 328

3. 586

3.848

4.115

4. 386

4.660

4.938

5. 026

5.218

5.501

5.734

5.787

6,362

6.943

7 . 529

8.117

8.708

9.299

9,891

10.482

11.070

11.657

13.106

14.526

15.911

17.255

19.819

22.214

24.451

26. 542

28.500

30.340

32.073

33.711

35.263

36.737

38.141

39.481

40.762

41.991

43.171

44.306

45.400

46.455

47.474

48.461

49.417

50.343

51.243

52.118

52.969

53.797

5q .604

55,392

56.160

56.911

57. 644

58. 362

59. 064

-{G°(I")-H°(0) )./T

,NmoI-K

0 000

0 012

0 030

0 054

0 084

0 120

0 164

0.213

0.267

O. 326

0.390

0,457

0.530

0.606

0.685

0.769

0.855

0.945

1. 038

1.133

1. 232

I .333

1. 436

1.542

I .651

1.761

i .874

I .909

1.988

2.104

2.201

2,223

2.463

2.709

2.961

3.216

3.476

3.739

4.005

4.274

4.545

q .818

5.505

6. 198

6.893

7.585

8.956

10.297

II .602

12.867

lq.088

15.269

16 .(407

17. 508

18.570

19.595

20.587

21.546

22.474

23.375

24.248

25.096

25.920

26. 720

27.498

28.257

28.996

29.715

30.418

31.104

31.775

32.429

33.069

33.696

34.309

34.910

35.498

36. 076

36.641

H°Cr)

kJ/room

-I 053

-I 053

-1 052

-1 049

-1 045

-i 039

-I 03I

-I 021

-i 008

-0 992

-0 974

-0.953

-0.928

-0. 901

-0.870

-0.836

-0.799

-0.758

-0.713

-0.665

-0.613

-0.558

-0.499

-0.436

-0.370

-0.300

-0.226

-0.202

-0.149

-0. 068

0.000

0.016

0.194

0. 386

0.591

0.809

1.039

1.282

I .536

1.802

2,079

2.366

3. 127

3.943

4.808

5.716

7.637

9.671

11.795

13.989

16.240

18.538

20.878

23.251

25.655

28. 087

30.543

33.022

35.521

38.039

40.576

43.129

45.698

48. 284

50.883

53.497

56.125

58.766

61.422

64.088

66.768

69.460

72.164

74.881

77.608

80,348

83.099

85.861

88,6_;6

-G°Cr}/T

J/moI-K

INFINITE

52.687

35.146

2_.392

21. 154

17.679

15.214

13. 381

11.973

I0.861

9.967

9.236

8.633

8.131

7.708

7.353

7.052

6.797

6,582

6.401

6. 249

6. 122

6.016

5.932

5.865

5.813

5.775

5.766

5.750

5.737

5.734

5.734

5.755

5.807

5.887

5.988

6.110

6.247

6.400

6. 565

6.739

6.925

7.421

7. 954

8.514

9.090

10.273

II .468

12.656

13.824

14.966

16.080

17,160

18.210

19. 228

20.215

21. 172

22. 101

23. OOl

23.877

24.727

25.554

26. 359

27. 141

27.903

28.647

29.372

30.079

30.769

31.444

32. 104

32. 748

33.379

33.997

34.602

55,195

55.776

36. 346

36,905

T

K

0

20

30

40

50

60

70

80

90

I00

II0

120

130

140

150

160

170

180

190

200

210

220

230

240

250

260

270

275.

280

290

298

300

320

340

360

380

400

420

440

460

480

500

550

600

650

700

8O0

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

15

.15

26 NASA/TP-3287/REV 1
3"ABLEIll.8.* Concluded.

T C° H°_) "H°(O) S°(T) "{G°(T')'H°(O)}K

K J/m_-K kJ/mol JIm_K J/mm-K

qlO0 27,906 92._76 59.752 57,197

4200 28.017 95.270 60._26 37,7_3

_300 28.128 98.078 61.086 38.277

_40D 28.238 100.900 61.736 38,802

q500 28.347 103.730 62.370 39.319

4600 28.456 _06.570 62.994 39.827

6700 28.565 109,420 63.607 _0.326

4800 28.673 112.280 64.210 40.818

4900 28.782 115.150 64.802 41.302

5000 28.890 118.0_0 65.385 _1.777

H°(T)

_/m_

91._20

96.216

97.026

99.8_6

102.676

105.516

108.366

111.226

114.096

116.986

.GocI")K

Nm_-K

37.454

57.993

38.522

39.042

39.553

k0.056

60.550

61.038

41.517

_1.988

T

K

q100

4200

6500

4600

4700

_800

_900

5000

NASA/TP-3287/REV 1 27
TABLE 1119- SELECTED THERMODYNAMIC FUNCTIONS FOR Ca(a,pJ)

T C° H°("T)'H°(0) 8°( T) -{G°('T)-H°(O)}K H°(T) _°('r')_ T

K J/n'_l-K kJ/mol J/mokK J/mokK kJIm_ J/m_-K K

0 0.000 0.000 0.000 0.000 -5.783 INFI_ITE 0

80 18.034 0.643 12.527 4._92 -5.140 76.779 80

90 19.327 0.830 14.729 5.508 -4.953 69.763 90

100 20.319 1.028 16.819 6.536 -4.755 64.365 100

120 21.746 1.450 20.659 8.576 -4.333 56.767 120

140 22.730 1.895 24.089 10.551 -3.888 51.858 140

160 23.448 2.357 27.174 12.440 -3.426 48.583 160

180 23,994 2,832 29.968 14.235 -2.951 46.362 180

200 24.420 3.316 32.519 15.937 -2.467 44,852 200

220 24.761 3,808 34.863 17.553 -1,975 43.839 220

240 25.045 4.306 37.030 19.087 -1.476 43.182 240

260 25.291 4.810 39.045 20.545 -0.973 42.787 260

280 25.518 5.318 40.928 21.935 -0.465 42.568 280

298.15 25.750 5.783 42,536 23.140 0.000 42.536 298.15

300 25.800 5,831 42.696 23.260 0.048 42.557 300

350 26.399 7.135 46,716 26.330 1.352 42.853 350

400 27,112 8,472 50,287 29.106 2.689 43.563 400

450 27.897 9.847 53,525 31.642 4.064 44.493 450

500 28.733 11.263 56.507 33.981 5.480 45.547 500

550 29.607 12.721 59,286 36.157 6.938 _6.671 550

600 30,513 14,224 61.901 38.194 8,441 47.832 600

650 31.444 15.773 64.380 40.114 9.990 _9.011 650

700 32,399 17.369 66.745 41.932 11.586 50.193 700

o 716 32.709 17.890 67.481 42.495 12.107 50.572 716

...... ...... ;;7;;; ...... ;;7;;;...... ;;7;;; ...... ...... ;;7;;;....... ;;;---

800 30.155 21.341 72.109 45.433 15.558 52.661 800

900 31.009 24.394 75.704 48.599 18.611 55.025 900

1000 32.532 27.565 79.044 51.478 21.782 57.261 1000

1100 34.724 30.923 82.242 54.130 25.]40 59.388 1100

1115 35,110 31.446 82.715 54.512 25.663 59.698 1115

............................................................................................

111_ 38 000 39 986 90 574 54 512 34 203 59 698 1115

1200 38.000 43,216 93.166 57.152 37,433 61,971 1200

1300 38.000 47,016

lqO0 38.000 50.816

1500 3_.000 54.616

1600 38.000 58.416

1700 38.000 62.216

1800 38.000 66.016

1900 38.000 69.816

2000 38,000 73.616

2100 38.000 77.416

2200 38.000 81.216

2300 _8.000 85.016

2_DG 38.000 88.816

2500 38.000 92.616

2600 38.000 96.416

27cc 35.000 100.216

2800 38.000 104.016

29_C 53.000 107.816

30OC 35.000 111.616

3_0_ 3_,000 115.416

32CC 38.oo0 119.216

_30C 3_.000 123.016

3_00 3_.000 126.816

5500 38.000 130.616

3600 38.000 134.416

3700 38.000 138.216

3800 38.000 142.016

3900 38.000 145.816

4000 38.000 149.616

4100 38.000 153.416

4200 38,000 157.216

4300 38.000 161.016

4400 38.000 164,816

4500 38,000 168.616

4600 38,000 172.416

4700 38,000 176.216

4800 38.000 180.016

4900 38.000 183.816

5000 38.000 187.616

96.207 60.041 41.233 64.489 1300

99.023 62.726 45.033 66,857 1400

101.645 65,234 48.853 69,090 1500

104,098 67.587 52.633 71.202 1600

106.401 69,803 56.433 73.205 1700

108.573 71.898 60.235 75.110 1800

110.628 73.882 64.033 76.926 1900

112.577 75,769 67.833 78.660 2000

114.431 77.566 71.653 80.320 2100

116.199 79.282 75.433 81.911 2200

117.888 80,924 79.233 83.439 2300

119.505 82.498 83.033 84.908 2400

121.056 84.010 86.833 86.323 2500

122.547 85.464 90.633 87.688 2600

123.981 86.864 94.433 89.006 2700

125.363 88.214 98.233 90.280 2800

126.696 89,518 102.033 91.512 2900

127,985 90.779 105.833 92.707 3000

129.231 92.000 109.633 93.865 3100

130.437 93,182 113.433 94.989 3200

131.606 94.329 117.233 96.081 3300

132.741 95.442 121.033 97.143 3400

133.842 96.523 124.833 98.176 3500

134.913 97.575 128.633 99.181 3600

135.954 98.598 132.433 100.161 3700

136.967 99.595 136.233 101.I17 3800

137.954 100.566 140.033 102.049 3900

138.917 101.513 143.833 102.958 4000

139.855 102,436 147.633 103.847 4100

140.771 103.338 151.433 104.715 4200

141.665 104.219 155.233 105.564 4300

142.538 105.080 159.033 106.394 4400

143.392 105.922 162.833 107.207 4500

144.228 106.746 166.633 108.003 _600

145.045 107.552 170.433 108.782 4700

145.845 108.341 174.233 109.546 4800

146.628 109.115 178.033 ] t.295 4900

1_7.396 109.873 181.633 111,029 5000

28 NASA/TP-3287/REV l
TABt._ _t|g,"Con_udecl,

T C° H°(_'H°(0) S°(T) "{G°_)'HO(o)}_

K Jfm_l-K kJ/mol J/mot-K Jfmo_K

5100 38.000 191._16 1_8.1_9 110.616

5200 38.000 195.216 148.886 111.345

530o 38.000 199.016 149.610 112.060

5qO0 38.000 202.816 150.321 112.762

5500 38.000 206.616 151.018 113.451

5600 38.000 210.416 151.703 11_.128

5700 38.000 21q.216 152.375 11_.793

5800 38.000 218.016 153.036 I15._47

5900 38.000 221.816 153.686 116.090

6000 38.000 225.616 154.324 116.722

H°(T)

_/mol

185.633

189._33

193.233

197.033

200.833

20q.633

208.q33

212.233

216.033

219.833

.G°(l")_

J/mokK

lll .750

112.457

113.151

113.833

11_.503

115.161

115.808

l16._q

117.070

117.685

T

K

5100

5200

5300

5_00

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV l 29
TABLE J110.. SELECTED THERMODYNAMIC FUNCTIONS FOR Cd(cr,t)

T cO H°{T)-H°( O) S°(T) -{Q°(T)-H°(0)}K H°(T) -G°(T)K T

K _r_-K kJ/mol Jlm_-K _m_-K _/mol _mol-K K

0 0,000 0.000 0.000 0,000 -6.247 INFINITE 0

100 25.110 1.360 25.200 11.600 -4.887 74.070 100

200 24,920 3,745 41,635 22.910 -2,502 54.145 200

298.15 26.020 6,247 51.800 30.847 0.000 51,800 298.15

3,)0 26.036 6.295 51.961 30.978 0,048 5].801 300

400 27.080 8,948 59,586 37.216 2.701 52.833 400

500 28.337 11.718 65.761 42.325 5.471 54.819 500

cr 594.26 29.599 14._48 70.760 46.4q8 8,201 56.960 594.26

Q 594.26 29.900 20.508 80,958 46.448 14,261 56,960 594.26

600 29.900 20.680 81.246 46.779 14.433 57,191 600

700 29.900 23.670 85,855 52,041 17,423 60,965 700

800 29.900 26.660 89.847 56.523 20.413 64.331 800

900 29.900 29.650 93.369 60.425 23.403 67.366 900

1000 29,900 32,640 96,519 63.880 26,393 70,127 1000

1100 29.900 35,630 99.369 66.978 29,383 72.657 II00

1200 29.900 38.620 101.971 69.788 32.373 74.993 1200

1300 29.900 41.610 104.364 72.356 35.363 77.162 1300

1400 29.900 44.600 106,580 74,723 38.353 79.185 1400

1500 29.900 47.590 108.643 76.916 41.343 81.081 1500

1600 29.900 50.580 110.572 78,960 44.333 82.864 1600

1700 29.900 53.570 112.385 80.873 47,323 84.548 1700

1800 29.900 56.560 i14.094 82,672 50.313 86.143 1800

1900 29.900 59.550 115.711 84.369 53,303 87.657 1900

2000 29.900 62.540 117.244 85.974 56.293 89.098 2000

2100 29.900 65.530 118.703 87.499 59.283 90.473 2100

2200 29.900 68.520 120.094 88.949 62,273 91.788 2200

2300 29.900 71.510 121.423 90.332 65,263 93.048 2300

2400 29.900 74.500 122.696 91.654 68.253 94.257 2400

2500 29.900 77.490 123.916 92.920 71,243 95.419 2500

2600 29.900 80.480 125.089 94.135 74.233 96,538 2600

2700 29.900 83.470 126.217 95.303 77,223 97.616 2700

2800 29.900 86.460 127,305 96.426 80.213 98.657 2800

2900 29.900 89.450 128.354 97.509 83.203 99.663 2900

3000 29,900 92.440 129.368 98.554 86.193 100.637 3000

3100 29.900 95.430 130.348 99,564 89.183 101.580 3100

3200 29,900 98.420 131,297 100.541 92,173 102.493 3200

3300 29.900 101.410 132.217 101.487 95.163 103.380 3300

3400 29.900 104.400 133.110 102.404 98.153 104.242 3400

3500 29.900 107.390 133,977 103,294 101.143 105.079 3500

3600 29.900 110.380 134.819 104.158 104.133 105.893 3600

3700 29.900 113.370 135.638 104.998 107.123 106.686 3700

3800 29.900 116.360 136.436 105.815 110.113 107.459 3800

3900 29.900 119.350 137.212 106.610 113.103 108.212 3900

4000 29,900 122,340 137.969 107.384 116,093 108,946 4000

4100 29.900 125.330 138.708 108.139 119,083 109.663 4100

4200 29.900 128.320 139.428 108.876 122.073 110.363 4200

4300 29.900 131.310 140.132 109.595 125.063 111.047 4300

4400 29.900 134,300 140.819 110.297 128.053 111,716 4400

4500 29.900 137.290 141.491 110.982 131.043 112.371 4500

4600 29.900 140.280 142.148 111.653 134.033 113.011 4600

4700 29.900 143.270 142.791 112.308 137.023 113.638 4700

4800 29.900 146.260 143.421 112.950 140.013 114.252 4800

4900 29.900 149,250 144.037 113.578 143.003 114.853 4900

5000 29.900 152.240 144.641 114.193 145.993 115.443 5000

5100 29.900 155.230 145.233 114,796 148.983 116.021 5100

5200 29.900 158.220 145,814 115.387 151,973 116,589 5200

5300 29.900 161.210 146.384 115.967 154.963 117.145 5300

5400 29.900 164.200 146.943 116.535 157.953 117.692 5400

5500 29.900 167.190 147.491 117.093 160.943 118.229 5500

5600 29.900 170.180 148.030 117.641 163.933 118.756 5600

5700 29.900 173,170 148,559 118.178 166.923 119.274 5700

5800 29.900 176.160 149,079 118,707 169.913 119.784 5800

5900 29.900 179,150 149.590 119.226 172.903 120.285 5900

6000 29.900 182.140 150.095 119.736 175.893 120.777 6000

30 NASA/TP-3287/REV 1
TABLEIlL11 - SELECTED THERMODYNAMIC FUNCTIONS FOR CI2

T CO H°(T)'H°(O) s°(T) "{G°(T)'H°(O) }_ H°(l') _°(TJ_

K J/m_K k_mol J/moFK J/mokK kJ/mol J/moI-K

0 0.000 0.000 0,000 0.000 -9,181 INFINITE

100 29.299 2,912 189.009 159.889 -6.269 251,700

200 31.720 5.950 209.967 180.216 -3.231 226.122

298.15 33,949 9.181 223.082 192.288 0.000 225.082

300 33.981 9.244 223.292 192.478 6.063 223.082

400 55.296 12.714 235.266 201.480 3.533 224.433

500 36.064 16.285 241.232 208.662 7.104 227,024

600 36.547 19.917 247.853 214.658 I0,736 229.959

700 36.874 23.589 253.512 219.813 14.408 232.929

800 37.111 27.289 258.452 224.340 18.108 235.817

900 37.294 31.009 262,834 228,379 21.828 238,581

1000 37.442 34.746 266.772 232,026 25.565 241,207

1100 57.567 38.497 270.346 235.349 29.316 243.695

1200 37.678 42.260 273.620 238.404 33.075 246.055

1300 37.778 46.033 276.640 241.231 36.851 248.293

1400 37.872 49.816 279.443 243.861 40.634 250.419

1500 37.961 53.607 282.059 246,322 44.426 252.442

1600 38.048 57.408 284.511 248.632 48.227 254.370

1700 38.133 61.217 286.821 250,812 52.036 256.212

1800 38.242 65.038 289.005 252.873 55.857 257.974

1900 38.349 68.867 291.076 254,830 59.686 259.662

2000 38.468 72.708 293.046 256.692 63.527 261.282

2100 38.604 76.561 29_.926 258.468 67.380 262.840

2200 38.760 80.429 296.725 260.166 71.248 264,339

2300 38.940 84.314 298.452 261.793 75.133 265.785

2400 39.145 88.218 300.114 263.356 79.037 267.182

2500 39.379 92.144 301.716 264.858 82.963 268.530

2600 39,639 96.095 303.266 266.306 86.914 269.837

2700 39.927 100.073 304.767 267.703 90.892 271,103

2800 40.239 104.081 306,225 269,053 94.900 272.332

2900 40.571 108.121 307.643 270.359 98.940 273.525

3000 40.920 112.195 309.024 271.625 103.014 274.686

3100 41.281 116.306 310.371 272.853 107.125 275.814

3200 41.648 120.452 311.688 274.046 111.271 276.915

3300 42.01_ 124.635 312.975 275,206 115.454 277,989

3400 42.374 128,855 314.234 276,335 119.673 279.036

3500 42,721 133.110 315.468 277,436 123,928 280.060

3600 43.051 137.399 316,676 278.510 128.218 281.060

3700 43.357 141.719 317.860 279.557 132.538 282.039

3800 43,636 146.069 319.020 280.581 136.888 282.997

3900 43,882 150,445 320.156 281.580 141.264 283.934

4000 44.094 154.844 321.270 282,559 145.663 284.854

4100 44.268 159.262 322.361 283.517 150.081 285.756

4200 44.403 163.696 323.430 284.655 154.515 286.641

4300 44.498 168.142 324.476 285.373 158.961 287.508

4400 44.552 172.594 325.699 286.273 163.413 288.360

4500 46.565 177,050 326,501 287,156 167.869 289,197

4600 44.538 181.506 327.480 288.022 172.325 290.018

4700 44.473 185.957 328.437 288.872 176.776 290.825

4800 44.370 190.399 329.372 289.705 181.218 291.618

4900 44.233 194.829 330.286 290.525 185.648 292.399

5000 44.062 199.244 331.178 291.329 190,063 293.165

5100 43.860 203.640 332.048 292.118 194.459 293.919

5200 43,630 208.016 332.898 292,895 198.834 294.661

5300 43.374 212.366 333.726 293,657 203,184 295.389

5400 43.095 216.690 534.535 294.607 207.508 296.108

5500 42.796 220.985 335.323 295.144 211.806 296.813

5600 42'.477 225.248 336.091 295.868 Z16.067 297.508

5700 42.144 229.479 536,840 296.581 220.298 298.191

5800 41.796 253.676 337.570 297.281 224.495 298.864

5900 41.436 237.838 338.281 297.970 228.657 299.526

6000 41.068 2_1.963 338.974 298.647 232.782 300.177

T

K

0

100

200

298.15

3O0

400

500

600

700

800

900

1000

1100

1200

1500

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

6000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NAS A/TP-3287/REV 1 31
TABLE 1[I.12.- SELECTED THERMODYNAMIC FLINCTtONSFOR Co(=,B,f)

T C° H°(T).H°(O) 8o(-,r,)

K Nm_-K kJ/mol J/moI-K

0 0.000 0.000 0.000

100 13.909 0.522 7.681

150 19,626 1.377 14.221

200 22.226 2.431 20.588

250 23.984 3.587 25.738

298.15 26.802 6.771 30.067

300 24.833 4.817 30.221

350 25.682 6.080 34.113

400 26.527 7.385 37.597

650 27.390 8.733 40.772

500 28.200 10.123 43.700

550 28.943 11.552 46.623

600 29.665 13.017 48.973

700 31.045 16.053 53.650

a 700.10 31.067 16.056 53.654

-{G°(T)-H°(O)}/r

J/moI-K

0 000

2 461

5 041

8 433

11 390

16 065

14 164

16.742

19.135

ZI,365

23.454

25.419

27.278

30.717

30.721

H°("T') -G°(T)_ T

_/mol NrnoI-K K

-4.771 INFINITE 0

-6.249 50.171 i00

-3.394 36,848 150

-2.340 32.288 200

-1.184 30.474 250

0.000 30.067 298.15

0.046 30.068 300

1.309 30.373 350

2.614 31.062 400

3,962 31.968 450

5,352 32.996 500

6,781 34.094 550

8.246 35.230 600

11.282 37.533 700

11.285 37.535 700,10

700.10 30.583 16.508 54.300 30.721 11.737 37.535 700.10

800 32.426 19.654 58._97 33.930 14.883 39.893 800

900 34.518 22.998 62.433 36,880 18,227 42.181 900

1000 36.987 26.570 66.194 39.624 21.799 44.395 1000

1100 39.632 30,406 69.8_9 42.207 25.635 46.564 1100

1200 43.221 34.542 73.445 64.660 29.771 48.636 1200

a_ 1300 68.660 39.125 77.111 47.015 34.354 50.685 1300

1396 54.978 43.986 80.719 69.165 39.215 52.588 1394

1394 54.978 43.986 80.719 49.165 39,215 52.588 139_

1400 64.225 44.282 80.930 69,300 39,511 52,708 1400

1500 39.748 68.630 83.794 51.507 63.659 54.688 1500

1600 38.284 52.323 86.307 53.605" 47.552 56,587 1600

1700 37.782 56.118 88.608 55.597 51.347 58.404 1700

1768 37.990 58.692 90.092 56.895 53.921 59,596 1768

............................................................................................

t 1768 60.501 76.884 99.251 56.895 70.113 59.594 1768

1800 40.501 76.180 99.977 57.655 71,609 60,305 1800

1900 40.501 80.230 102.167 59.941 75.459 62.452 1900

2000 40.501 86.280 104.245 62.106 79,509 64.490 2000

2100 40.501 88.331 106.221 64.158 83,560 66.430 2100

2200 40.501 92.381 108.105 66.113 87,610 68.282 2200

2300 60.501 96.431 109.905 67.979 91,660 70.053 2300

2400 40.501 100.481 111.629 69.762 95.710 71.750 2400

2500 40.501 104.531 i13.282 71.470 99.760 73.378 2500

2600 40.501 108.581 114.871 73.109 103.810 74.944 2600

2700 40.501 112.631 116.399 74.686 107.860 76,451 2700

2800 60.501 116,681 117.872 76.200 111.910 77.904 2800

2900 40.501 120.731 119.293 77.662 115.960 79.307 Z900

3000 _0,501 124.781 120.666 79.072 120.010 80.665 3000

3100 40.501 128.832 121,996 80,436 124.061 81.975 3100

3200 40.501 152.882 123.280 81.755 128.111 85.246 3200

3300 40.501 136.932 124.526 83,032 132.161 84._78 3300

3600 40.501 140.982 125.735 86.270 136.211 85.673 3400

3500 40.501 145.032 126.909 85.472 140.261 86.835 3500

3600 40.501 149.082 128.050 86.639 164.311 87.964 3600

3700 40.501 153.152 129.160 87.773 148.361 89.063 3700

3800 40.501 157.182 130.240 88.876 152.411 90.132 3800

3900 40.501 161.232 131.292 89.951 156.461 91.174 3900

4000 40.501 165.282 132.318 90.997 160.511 92.190 4000

_100 40.501 169.333 133.318 92.017 164.562 93.181 4100

6200 _0.501 173.383 134.294 93.012 168.612 94,148 4200

6300 40.501 177.433 135.247 93.983 172.662 95.095 4300

4400 40.501 181.483 136.178 94.932 176.712 96,016 6400

4500 40.501 185.533 137.088 95.858 180.762 96.919 4500

4600 40.501 189.583 137,978 96.764 184.812 97.802 6600

4700 40.501 193.633 138.849 97.651 188.862 98.666 6700

_800 40.501 197.683 139.702 98.518 192.912 99.512 6800

4900 40.501 201.733 140.537 99.367 196.962 100.341 4900

5000 40.501 205.783 141.355 100.198 201.012 101.153 5000

5100 40.501 209.854 142.157 101.013 205.063 101.949 5100

5200 40,501 213.884 142.944 101.812 209.115 102.750 5200

5300 40.501 217.934 143.715 102.596 213.163 103.496 5300

5400 60.501 221.986 144.472 103.566 217.213 104.248 5400

5500 40.501 226.056 145.215 104.118 221.263 104.986 5500

5600 40.501 230.084 145.945 106.859 225.515 105.711 5600

5700 40.501 236.134 166.662 105.586 229.365 106.423 5700

5800 40.501 238.184 147.366 106.300 253.413 107.123 5800

5900 40.501 242.234 148.059 107.002 237.463 107.811 5900

6000 40.501 246.284 168.759 107.692 241.513 108.487 6000

aLatrd_a maximum t_nsitlon point at 1394 K

32 NASA/TP-3287/REV 1
TABLE tU.13.- SELECTED THERMODYNAMIC FUNCTIONS FOR Cr(cr,I)

T C° HO_.HO(0 ) BO{1_ ._GO(T).HO(0)}K HO(T) .G°(T)_ T

K J/_-K kJ/mol J/mot-K J/moI-K kJ/mol J/m_-K K

0 0,000 0.000 0.000 0,000 -6.057 INFINITE 0

100 9:963 0.311 4.286 1.176 -3.766 41.766 100

150 16.351 0.983 9.645 3.092 -3,074 30.138 150

200 19.860 1.895 14.869 5.394 -2.162 25.679 200

250 22.298 2.955 19,590 7.770 -1.102 23.998 250 298.15 23.434 6.057 23.618 10.011 0000 23.618 298.15

oo 23 472 4 100 23 764 10.097 0.043 23621 300

cr _o£_,_u

......

_J,uuz _., 4'372 • 24'651 • 10" 616 0.315 23:_ ..... _:_

_ _1;50 2368; ,.373 -- -_:;5_ _07;;; ;:;;; _;660 -- 311.50

350 2_.393 5.:,7 27._53 12.319 1.24o 23.910 350

400 25.230 6.538 30.765 14.420 2.681 24.562 400

_50 25.983 7.819 33.781 16.405 3.762 25.421 650

500 26.631 9,135 36.553 18.283 5.078 26.397 500

550 27.20_ 10.481 39.119 20.063 6.424 27.439 550

600 27.719 11,856 41.508 21.751 7.797 28.513 600

700 28.577 14.669 45.846 24.890 10.612 30.686 700

BOO 29.634 17.568 49.715 27.755 13.511 32,826 800

900 30.501 20.562 53.241 30.394 16.505 3_.902 900

I000 31.861 23.678 56.523 32.845 19.621 36.902 1000

1100 33._72 26.94_ 59,634 35.139 22,887 38.828 1100

1200 35.187 30.375 62.618 37.305 26.318 _0.686 1200

1300 37.116 33.990 65.511 39.365 29.933 42._86 1300

1400 39.125 37.801 68.334 41.333 33.744 49,231 1400

1500 41.200 41.817 71.104 43.226 37.760 45.931 1500

1600 63.329 46.043 73.831 65.054 41.986 47.590 1600

1700 65.501 50._84 76.525 66.827 46.427 69.215 1700

1800 67.706 55.1_4 79.186 48.550 51.087 50.804 1800

1900 49.944 60,027 81.825 50.232 55.970 52.367 1900

2DO0 52.204 65.136 84.444 51.877 61.077 53.905 2000

2100 54.488 70.468 87.066 53.490 66.411 55.422 2100

cr Z130 55.17_ 72.113 87.824 53.968 68.056 55.873 2130

............................................................................................

| 21.30 39.330 92.615 97.4_9 53.968 88.558 55.873 2130

2200 39.330 95.368 98,721 55,372 91.311 57.216 2200

2300 39.550

2_00 39,33O

2500 39.330

2600 39.330

2700 39.350

2800 39.330

2900 39.330

3000 39.330

3100 39.330

3200 39.330

3300 39.330

3_00 39.330

3500 39.330

3800 39.330

3700 39.330

3800 39.330

3900 39.330

qOOO 39.330

61oo 39,330

420O 39.33O

4300 39.330

4_00 39.330

_500 39.330

_600 39.330

_700 39.330

_800 39.330

_900 39.330

5000 39.330

5100 39,330

5200 39.330

5300 39.330

5400 39.330

5500 39.330

5600 39.330

5700 39.330

5800 39.330

5900 39.330

6000 39.330

99.301 100.469 57.295 95.244 59.059

103.236 102.1_3 59.129 99.177 60.819

107.167 103.7_9 60.882 103,110 62.505

111.100 105.291 62.560 107.043 66.121

115.033 106.775 66.171 110.976 65.673

118.966 108.206 65.718 116.909 67.167

122.899 109.586 67.207 118,842 68.606

126.832 110.919 68.662 122,775 69.994

130.765 112.209 70.027 126.708 71.335

136.698 113.458 71.364 130.6_1 72.632

138.631 114.668 72.658 134.576 73.888

142.564 115.862 73,911 138.507 75.105

146.497 116.982 75.126 142.440 76.285

150.430 118.090 76.304 146.373 77.431

154.363 119.168 77.448 150.306 78.544

158.296 120.216 78.560 154.239 79,627

162.229 121.23_ 79.641 158.172 80.681

166.162 122,236 80,693 162.105 81.708

170.095 123.205 81.718 166.038 82.708

174.028 126.153 82.717 169.971 83.683

177.961 125.078 83.692 173.904 84.635

181.894 125,982 86.643 177.837 85,565

185.827 126.866 85,571 181.770 86.673

189.760 127.731 86.678 185.703 87.360

193.693 128.577 87.365 189.636 88.228

197.626 129.405 88.232 193.569 89.078

201.559 130,215 89.081 197.502 89.909

205.492 131.010 89.912 201._35 90.723

209.425 131.789 90.725 205.368 91,521

213.358 132.553 91.522 209.301 92.302

217.291 133.302 92.303 213.23_ 93.069

221.224 13_.037 93.070 217.167 93.821

225.157 134.759 93.821 221.100 94.559

229.090 135.467 94.558 225.033 95.283

233.023 136.163 95.282 228.966 95.994

236.956 136.847 95.993 232.899 96.692

2_0.889 137.520 96.691 236.832 97.379

244.822 138.181 97.377 240.765 98.053

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

6100

4200

4300

4_00

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

aMaximum lanYodab.ansition point at 311.5 K.

NASA/TP-3287/REV 1 33
T

K

0

1oo

2OO

298 o15

300

cr 301,59

C °

J/m_-K

0 000

25 820

27 790

32 210

32 379

32 525

TABLE 111.14..SELECTED THERMODYNAMIC FUNCTIONS FOR Cs(crJ)

HO('T).HO_) so_ .{oO_.HO_)}_ HO(T) _0_ T

kJ/mo_ J/moI-K _moI-K kJ/mol _moI-K K

0.000 0.000 0.000 -7.711 INFINITE 0

2.150 54,978 33,478 -5,561 110.588 100

4.829 73,475 49.330 -2,882 87.885 200

7.711 85,230 59,567 0.000 85.230 298.15

7.771 85.430 59.527 0.060 85.230 500

7,822 85.601 59,665 0.111 85.233 301.59

;---1;;7;;---;;7;1; ....... ;7;;; ...... ;;7;;; ...... ;;7;;; ....... ...... ....... ;;;7;;

400 32.024 13.108 101.708 68.938 5.597 88.215 400

500 30.955 16.257 108.740 76.226 8.546 91.648 500

600 30.001 19.503 114.296 82.124 11.592 94,976 600

700 29.361 22.268 118.868 87,057 14,557 98,072 700

800 29.115 25.188 122.768 91.283 27.477 100.922 800

900 29.304 28,106 126,204 94.975 20,395 105.543 900

I000 29.948 31.064 129.520 98.256 23.353 105.967 1000

1100 31.059 34.111 132.225 101.213 26,400 108.223 1100

1200 32.643 37.292 134.990 103.913 29.581 110.339 1200

1300 34.707 _0.655 137.681 106.408 32.944 112.339 1300

1400 37.251 44.249 140.345 108.737 36.538 11_,244 1400

1500 40.278 48.122 143.014 110.935 40.411 116.073 1500

1600 43.791 52.321 145.723 113.022 44.610 117.842 1600

1700 47.788 56.896 148.495 115.027 49.185 119.565 1700

1800 52.273 61.895 151.351 116.965 54.18_ 121.249 1800

1900 57.244 67.367 154.308 118.852 59.656 122.910 1900

2000 62.702 73.360 157.381 120,701 65.649 124.556 2000

34 NASA/TP-3287/REV 1
TABLE 111.15.- SELECTED THERMODYNAMIC FUNCTIONS FOR Cu(c,r.O

T C° HO(T).Ho(O) so(T) .(Go0..).HO(0)}_ HO(T) .G°0"]_ T

K J/n_-K kJ/m_ J/mot-K J/mo4-K kJ/mol J/o'_-K K

0 0.o0o 0.00o 0.000 0.000 -5,004 INFINITE 0

100 16.010 0.669 10.030 3.340 -4.335 53.380 100

200 22.630 2.682 23.730 10.320 -2.322 35.340 200

298,15 24.440 5.004 33.150 16.567 0.000 33.150 298.

3,_0 24.460 5.049 33.301 16.471 0.045 33,151 300

400 25.339 7.5_2 _0.667 21.612 2.538 34.122 400

500 25.966 10.109 46.192 25.974 5.105 35.982 500

600 26.479 12.732 50.973 29.753 7.728 38.093 600

700 26.953 15.403 55.090 33.086 10.399 40.234 700

800 27.448 18.123 58.721 36.067 13.119 _2.322 800

900 28.01_ 20.895 61.986 38.769 15.891 4_.329 900

I000 28.700 23.730 66,971 41.241 18.726 46,245 1000

15

29 553 26 641 67 745 43 526 21 637 48.075 II00

ii00 • • " " 4"644 49 824 1200 30 617 29 6_8 70.361 45.654 2 . '

1200 • " 9 51.501 1300 31 960 32 773 7Z.862 _7.652 27.76 58

" 75 759 29.647 52.444 13

cr la_o 32.844 34.651 _i_ .......... i ........................................

............. ;;-;j ...... ......83 951 48759 42.787 52.444 1358 1358 .... 165 53.404 14oo 1400 32.800 9169 84.950 49.830 44

1500 32.800 52.449 87.213 52.247 47.445 55.583 1500

1600 32.800 55.729 89.330 54.500 50.725 57.627 1600

1700 32.800 59.009 91.318 56.608 54.005 59.551 1700

1800 32.800 62.289 93.193 58.588 57.285 61.368 1800

1900 32.800 65.569 94.967 60.657 60.565 63,091 1900

2000 32.800 68.849 96.649 62.225 63.845 64.727 2000

2100 32.800 72.129 98.249 63.902 67.125 66.285 2100

2200 32.800 75.409 99.775 65.499 70.405 67.773 2200

2300 32.800 78,689 101.233 67.021 73.685 69.196 2300

2400 32.800 81.969 102,629 68.476 76,965 70.561 2400

2500 32.800 85.249 103.968 69.869 80.245 71.870 2500

2600 32.800 88.529 105.255 71.205 83.525 73._30 2600

2700 32.800 91.809 106.493 72.489 86.805 74.343 2700

2800 32.800 95,089 107.685 73.725 90.085 75.512 2800

2900 32.800 98,369 108.836 74.916 93.365 76.642 2900

3000 32.800 101,669 109.948 76.065 96.645 77.733 3000

3100 32.800 104.929 111.024 77.176 99.925 78.790 3100

3200 32.800 108.209 112.065 78.250 103.205 79.814 3200

3300 32.800 111.489 113.075 79.290 106.485 80.806 3300

3400 32.800 11_,769 114.054 80.298 109.765 81.770 3400

3500 32.800 118,049 115.004 81.276 113.045 82.706 3500

3600 32.800 321.329 115.928 82.226 116.325 83.616 3600

3700 32.800 124.609 116.827 83.149 119.605 86.502 3700

3800 32.800 127,889 117.702 84.047 122.885 85.364 3800

3900 32.800 131.169 118.554 84.921 126.165 86.204 3900

4000 32.800 136,449 119.386 85.772 129.445 87.023 4000

4100 32.800 137.729 120.196 86.602 132.725 87.822 4100

_200 32.800 141,009 120.985 87.411 136.005 88.603 4200

4300 32,800 1_4.289 121,756 88.201 139.285 89.365 4300

4400 32.800 147.569 122.510 88.972 1_2.565 90.109 4400

6500 32.800 159.849 123.248 89.726 145.845 90.838 4500

4600 32.800 154.129 123.968 90,462 149.125 91.550 4600

4700 32.800 157.409 124.674 91.183 152._05 92.247 4700

4800 32.800 160.689 125.364 91.888 155.685 92.930 4800

6900 32.800 163.969 126.041 92.578 158.965 93.599 4900

5000 32.800 167.249 126.703 93.254 162.265 94.254 5000

5100 32.800 170.529 127.353 93.916 165.525 94.897 5100

5200 32.800 173.809 127.990 94.565 168.805 95.527 5200

5300 32.800 177.089 128.615 95.202 172.085 96.146 5500

5400 32.800 180.369 129.228 95.826 175.365 96.753 5400

5500 32.800 183.669 129.830 96.439 178.645 97.349 5500

5600 32.800 186.929 130.621 97.040 181.925 97.934 5600

5700 32.800 190.209 131.001 97.631 185.205 98.509 5700

5800 32.800 193.489 131.572 98.211 188.485 99.074 5800

5900 32.800 196.769 132.132 98.782 191.765 99.630 5900

6000 32.800 200.049 132.684 99.342 195.045 100.176 6000

NASA/TP-3287/REV 1 35
TABLE 11116.- SELECTED THERMODYNAMIC FUNCTIONS FOR

D2

Tc° H°03.H°(0) so(D .{oo03.Ho(O)}K Hold

K J/n_-K _/moJ J/moI-K J/m_-K kJ/mol 0 0.000 0.000 0.000 0.000 -8.569

100 30.318 2.750 112.786 85.286 -5.819

200 29.205 5.704 133.305 104.784 -2.865

298.15 29.195 8.569 144.960 116.219 0.000

300 29.196 8.623 145.140 116.396 0.054

400 29.244 11.545 153.545 124.682 2.976

500 29.368 14.474 160.082 131.134 5.905

600 29.622 17.423 165,457 136.418 8.854

700 30.011 20.403 170.050 140.903 11.834

800 30.505 23.428 174.089 144.804 14.859

900 31.061 26.507 177.714 148.262 17.938

I000 31,641 29,641 181,016 151.375 21.072

ii00 32.216 32.834 184.059 154.210 24.265

1200 32.768 36.084 186.886 156.816 27.515

1300 33.289 39.387 189,530 159.252 30.818

1400 33.773 42.7_2 192.015 161._86 34.172

1500 34.221 46.141 194.360 163.600 37.571

1600 34.634 49.583 196.582 165.593 41.013

1700 35.014 53.068 198.694 167.478 44,499

1800 55.364 56.586 200.705 169.269 48.017

1900 35.688 60,140 202.626 170,974 51.571

2000 35.987 63.723 204.464 172,603 55.154

2100 36.265 67.335 206.227 174.163 58.766

2200 36.525 70.975 207.921 175.659 62.406

2300 36.769 74.641 209.550 177.097 66.072

2400 36.999 78,330 211.120 178.482 69.761

2500 37.216 82.038 212.634 179.818 73.469

2600 37.423 85.772 214.098 181.108 77.203

2700 37.620 89.522 215.514 182.357 80.953

2800 37.810 93.297 216.886 183.565 84.728

2900 37.993 97.087 218.216 184.737 88.518

3000 38.171 100.894 219.507 185.875 92.325

3100 38.344 104.719 220.761 186.980 96.150

3200 38.513 108.561 221.981 188.055 99.992

3300 38.679 112.422 223.169 189.101 103.853

3400 38.843 116,298 224.326 190.120 107.729

3500 39.005 120.188 225.454 191.114 111.619

3600 39.165 124.100 226.556 192.083 115.531

3700 39.324 128.026 227.631 193.029 119.456

3800 39.481 131.965 228.681 193.953 123.395

3900 39.639 135.921 229.709 194.857 127.352

4000 39,795 139.894 230.715 195.741 131.325

4100 39.990 ]43.879 231.699 196.606 ]35.310

4200 40.105 147.884 232.664 197.453 139,315

4300 40.258 151.900 233.609 198.283 143.331

4400 40.410 155.934 234.536 199.096 147.365

4500 40.560 159.982 235.446 199.894 151.413

4600 40.709 164.043 236.339 200.677 155.474

4700 40.854 168.121 237.216 201.445 159.552

4800 40.997 172.216 238.078 202.200 163.647

4900 41.135 176.324 238.925 202,940 167.755

5000 41.270 180.442 239.757 203.668 171.873

5100 41.400 184.581 240.576 204.383 176.012

5200 41.525 188.726 241.381 205.087 180,157

5300 41.646 192.885 242,173 205.779 184.316

5400 41,758 197,0_8 242.952 206.461 188.679

5500 41.864 201.236 243.720 207.131 192.667

5600 4i.963 205.427 244.475 207.791 196,858

5700 42.054 209,626 245.218 208.442 201.056

5800 42.137 213,837 245.951 209.083 205.267

5900 42.211 218.055 246.672 209.714 209.486

6000 42.276 222.273 247.381 210.336 213.704

6200 _2.379 230.742 248.769 211.553 222.173

6400 42.443 239.229 250.116 212.736 230.660

6600 62.467 247.721 251.423 213.&90 239.152

6800 42.450 256.Z13 252.690 215.012 247.644

7000 42.395 264.694 253.920 216.107 256.125

7200 42.300 273.164 255.113 217.174 264.595

7400 42.168 281.610 256.270 218.215 273.041

7600 42.001 290.027 257.392 219.231 281.458

7800 41.801 298.409 258.481 220.224 289.839

8000 41.570 306.748 259.536 221.193 298.179

G°_

_moi.K

INFINITE

170.977

147,630

144.960

144.960

146.105

148,272

150,700

153.144

155.515

157.783

159.944

162.000

163.957

165.824

167.606

169,313

]70,949

172.519

174.030

175.484

176.888

178.244

179,554

180,823

182.053

183.246

184.404

185.581

186.626

187.692

188.732

189.744

190.733

191.698

192.641

193.562

194.464

195.345

196.208

197.055

197.886

198.696

199.494

200.276

201.044

201.799

202.540

203.269

203.985

204.689

205.382

206.064

206.735

207.396

208.048

208.690

209,322

209.945

210.560

211.166

211.764

212.935

214.075

215.188

216.272

217.331

218.364

219.373

220.358

221.322

222.264

TK0

lOO

200

298.15

300

400

500

600

7O0

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

370O

3800

3900

4000

4100

4200

4300

4600

4500

4600

4700

4800

4900

5000

5100

5200

5300

5600

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

36 NASA/TP-3287/REVl
T

K

8200

$400

8600

8800

9000

9200

9400

9600

9800

i0000

I0500

ii000

11500

12000

12500

13000

15500

14000

1_500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

Co

J/m_K

41.312

41.029

40.725

q0.401

40.061

39.708

39.3_3

38.969

38.589

38.204

37.234

36.270

35.329

34.424

33.562

32.748

31.985

31.272

30.608

29.991

29.420

28.890

28.401

27.947

27.528

27.140

26.781

26.448

26.140

25.853

H°_-H°(_

kJIm_

315.0_0

323.270

331.448

339.561

347.602

355.584

363.484

371,322

379,079

386.755

405.610

423.989

441.893

459.330

q76.331

492.901

509.078

524.880

540.348

555.502

570.360

584.935

599,254

613.332

627.208

640.862

654.354

667.668

680.812

693.808

TABLE IlL16.- Concluded.

so(F) .{GO(,,r).HO(0)}K HO(T) -G°('T')K T

J/mol_ JIm_K _m_ J/rnol_ K

260.560 222.141 306.471 223.186 8200

261.552 223.068 31_.701 224.088 8_00

262,514 223.974 322.879 224.970 8600

263._46 224.860 330.992 225.833 8800

264.350 225.728 339.033 226,680 9000

265.227 226.577 347.015 227.508 9200

266.077 227.409 354,915 228.320 9400

266.902 228.223 362.753 229,115 9600

267.701 229.020 370.509 229.894 9800

268.477 229.802 378.186 230.659 10000

270.317 231.688 397.041 232.504 10500

272.027 233._83 415._Z0 234.262 11000

273.619 235.194 _33.324 235.939 11500

275.103 236,826 450,760 237.540 IZO00

276.491 238,385 _67.762 239.070 12500

277.791 239.876 484.332 240.535 13000

279.012 241.303 500.509 241.938 13500

280.162 242.671 516.311 243.283 14000

281.248 243.983 531.779 244.57_ 14500

282.275 245.242 546.933 245.813 15000

283.249 246.452 561.791 247,005 15500

284.175 247.617 576.366 248.153 16000

285.056 248,738 590.685 249.257 16500

285.897 249.819 604.763 250.323 17000

286.701 250.861 618.638 251.351 17500

287.471 251.868 632.293 252.344 18000

288.210 252.840 645.785 253.303 18500

288.920 253.780 659.099 254.231 19000

289.603 254.690 672.243 255.129 19500

290,261 255.571 685.239 256.000 20000

NASAfTP-3287/REV 1 37
TABLE IlL17.

- SELECTED THERMODYNAMIC FUNCTION$ FOR Electro_ Gas

TC° H°(T).H°(O) S°(T)

K J/n_-K kJ/mol J/moJ-K 0 0. 000 0. 000 0. 000

200 20,786 4,157 12.679

298.15 20.786 6.197 20.979

300 20.786 6.236 21.108

400 20.786 8.315 27.087

500 20.786 10.393 31.726

600 20.786 12.472 35.516

700 20.786 14.550 38.720

800 20.786 16.629 41.495

900 20.786 18.708 43.964

1000 20.786 20.786 46.134

1100 20.786 22.865 48.115

1200 20.786 24.944 49.923

1300 20.786 27.022 51.587

1400 20.786 29.101 53.128

1500 20.786 31.179 54.562

1600 20.786 33.258 55.903

1700 20.786 35.337 57.163

1800 20.786 37.415 58.352

1900 20.786 39.494 59.475

2000 20.786 41.573 60.542

2100 20.786 43o651 61.556

2200 20.786 45.730 62.523

2300 20.786 47.808 63.447

2400 20.786 49.887 66.331

2500 20.786 51.966 65.180

2600 20.786 54.046 65.995

2700 20.786 56.123 66,780

2800 20.786 58.202 67.536

2900 20.786 60.280 68.265

3000 20.786 62.359 68.970

3100 20.786 64.437 69.651

3200 20.786 66.516 70.311

3300 20.786 68.595 70.951

3400 20.786 70.673 71.571

3500 20.786 72.752 72.176

3600 20.786 74.831 72.760

3700 20.786 76.909 73.329

3800 20.786 78.988 73.883

3900 20,786 81.066 74.423

4000 20.786 83.145 74.950

4100 20.786 85.224 75.463

4200 20.786 87.302 75.966

6300 20.786 89.381 76.453

4400 20.786 91.460 76.93I

4500 20.786 95.538 77.398

4600 20.786 95.617 77.855

4700 20.786 97.695 78.302

4800 20.786 99.774 78.739

4900 20.786 101.853 79.168

5000 20.786 103.931 79.588

5100 20.786 106.010 80.000

5200 20.786 108.089 80.403

5300 20.786 110.167 80.799

5400 20.786 112.246 81.188

5500 20.786 114.325 81.569

5600 20.786 116.403 81.944

5700 20.786 118.482 82.311

5800 20.786 120.560 82.675

5900 20,786 122.639 83.028

6000 20.786 126.718 83.378

6200 20.786 128.875 84.059

6400 20.786 133.032 84.719

6600 20.786 137.189 85.359

6800 20.786 141.347 85.979

7000 20.786 145.504 86.582

7200 20.786 149.661 87.167

7400 20.786 153.818 87.737

7600 20.786 157.976 88.291

7800 20,786 162.133 88.831

8000 20.786 166.290 89.358

-{G°(T)-H°(O)}K

J/mokK

0 000

-8 107 0 193 0 321 6 301

I0 939

14.729

17.933

20.709

23.157

25.347

27.329

29.137

30.801

32.341

33.776

35.117

36.377

37.565

58.689

39.755

40.770

41.737

42.660

43.545

44.396

45.209

45.993

46.749

47.479

48.183

48.865

49.525

50.165

50.785

51.388

51.973

52.543

53.097

55.637

54.165

54.677

55.177

55.667

56.144

56.612

57.068

57.515

57.953

58.382

58.802

59.213

59.617

60.015

60.401

60.783

61.157

61.525

61.887

62.262

62.591

63.273

63.953

66.573

65.193

65.796

66.381

66.951

67.505

68.065

68.571

H°(_

kJ/mol

-6.197

-2.040

0.000

0.038

2.117

4.196

6.276

8.355

10.432

12.510

14.589

16.667

18.746

20.825

22.903

24.982

27.061

29.139

31.218

33.296

35.375

37.654

39.532

41.611

43.690

45.768

67.847

49.926

52,004

54.083

56.161

58.240

60.319

62.397

64.476

66.555

68.633

70.712

72.790

74,869

76.948

79.026

81.105

83.184

85.262

87.361

89.419

91.q98

93,577

95.655

97.734

99.813

101.891

103.970

106.048

108.127

110.Z06

112.284

114.363

116.462

118.520

122.677

126.855

130.992

135.149

139.506

163.666

147.621

151.778

155.936

160.093

_O('r)_

_m_

INFINITE

22.880

-20.979

20.979

21.795

23.33_

25.058

26.787

28.456

30.045

31.545

32.963

34.302

35.568

36.768

37.907

38.990

40.023

41.008

41.951

42.854

43.721

44.554

45.355

46.127

46.875

47.595

48.289

48,963

49.616

50.2_9

50.864

51.662

52.043

52.608

53.158

53.695

5_.218

54.728

55.226

55,713

56.188

56.653

57.108

57.553

57.989

58.4L6

58.834

59.24_

59.646

60.061

60.428

60.809

61.182

61.549

61.910

62.264

62.612

62.955

65.292

63.624

66.273

64.901

65.512

66.106

66.681

67.242

67.788

68.321

68.840

69.346

TKo

20o

298.15

3O0

400

500

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2_00

2900

3000

3100

3200

3500

3400

3500

3600

3700

3800

3900

6000

4100

4200

4300

6400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6600

6600

6800

7000

7200

7400

7600

7860

80DO

38 NASA/TP-3287/REV1
TABLE II1.17.- ConCluded.

T CO H°(_'H°(0) sO(T) "(G°_'H°(O)}_

K J/m_-K kJ/m_ J/mot-K JimoI-K

8200 20.786 170.447 89.871 69.085

8_00 20.786 174.605 90.372 69.585

8600 20.786 178.762 90.861 70.075

8800 20.785 182.919 91.339 70.552

9000 20.786 187.076 91.806 71.020

9200 20.786 191.234 92,263 71.476

9_00 20.786 195.391 92.710 71.923

9600 20.786 199.548 93,147 72.361

9800 20.786 203.705 93.576 72.790

10000 20.786 207,863 93.996 73.210

10500 20.786 218.Z56 95.010 74.224

11000 20,786 228.649 95.977 75.191

11500 20.786 239.042 96.901 76.115

12000 20.786 249.435 97.786 76.999

12500 20.786 259.828 98.634 77.848

13000 20.786 270.222 99.449 78.665

13500 20.786 280.615 100.234 79.448

1_000 20.786 291.008 100.990 80.204

14500 20.786 301.401 101.719 80.933

15000 20.786 311.794 102.H24 81.638

15500 20.786 322.187 103.106 82.319

16000 20.786 332.580 103.765 82.979

16500 20.786 342.974 104.405 83.619

17000 20.786 353.367 105.026 84.239

17500 20.786 363.760 105.628 84.842

18000 20.786 574.153 106.214 85.427

18500 20.786 384.546 106.783 85.997

19000 20.786 394.939 107.358 86.551

19500 20.786 405.332 107.878 87.091

20000 20.786 415.725 108.404 87.618

H°G)

_/m_

164.250

168.407

172,565

176.722

180.879

185.036

189.194

193,351

197.508

201.665

212.058

222.452

232.845

243.238

253.631

264.024

274.417

284.810

295.204

305.597

315.990

326.383

336.776

347.169

357.562

367.956

378.349

388.742

399.135

409.528

_o_

J/moI-K

69.840

70.323

70.795

71.257

71.708

72.150

72.583

73.007

73.422

73.829

74.814

75.754

76.654

77,516

78.344

79.140

79.907

80.646

81.360

82.051

82.719

83.367

83.994

8q.604

85.196

85.772

86.332

86.878

87.4O9

87.927

T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

NASAfrP-3287/REV 1 39
TABLE 11t,18..SELECTED THERMODYNAMIC FUNCTIONS FOR F2

T C° H°('T)oH°(O) S°(T)

K Jtr_.K kJ/mo( J/mol-K

0 0.000 0.000 0.000

100 29.114 2.907 170.372

200 29.686 5.836 190.654

298.15 31.304 8.825 202.792

300 31.337 8.883 202.986

400 31.995 12,102 212.237

500 34.258 15.468 219.742

600 35.171 18.942 226.074

700 35.839 12.494 231.548

800 36.343 26.105 236.368

900 36.740 29.759 240.672

1000 37.065 33.450 244.561

1100 37.342 37.171 248.107

1200 37.588 40.918 251.366

1300 37.811 _4.689 254,384

1400 38.019 48.480 257.194

1500 38.214 52.292 259.824

1600 38,396 56.123 262.296

1700 38.563 59.971 264.629

1800 38.711 63.835 266.837

1900 38.836 67.712 268.934

2000 38.935 71.601 270,928

2100 39.002 75.498 272.830

2200 39.036 79.400 274.645

2300 39.033 83.304 276,380

2400 38.992 87.206 275.041

2500 38.914 91.101 279.631

2600 38.799 94.987 281.155

2700 38.648 98.860 282.617

2800 38.464 102.716 284.019

2900 38.249 106.552 285.365

3000 38.006 110.365 286.658

3100 37.738 114.152 287.900

3200 37.450 117,912 289.093

3300 37.143 121.641 290.241

3_00 36.821 125.341 291.346

3500 36.487 129.006 292.409

3600 36.144 132.638 293.432

3700 35,795 136,235 294.417

3800 35._61 139.797 295.367

5900 35.084 143.323 296.283

_000 34.728 146.813 297.167

_]oo 3_.372 150.268 298.020

4200 3_.019 153.688 298.844

_309 33.670 157.072 299.640

_GO 35.326 160.422 300.410

6500 32.987 163.738 301.156

_60C 3=.65_ 167.020 301.877

_70C 3=.329 170.269 302.576

4800 _.Oll 173.486 303.253

_900 51.700 176.671 303.910

500o 3].398 179.826 304.547

5100 31.103 182.951 305.166

5100 30.817 186.047 305.767

53_0 30.538 L89,114 306.352

5_00 50.268 192.155 306.920

5500 30.007 195.168 307.473

5600 29.753 198.156 308.011

5700 29.507 201,I19 308.536

5800 29.269 204.058 309.047

5900 29.038 206.973 309.5_5

6000 28.815 209.867 310.031

-{G°('r)-H°(_}K

_moI-K

0 000

141 302

161 474

173 193

173 376

181 981

188.805

194.503

199.413

203,736

207.606

211.111

214.315

217.267

220.008

222.566

224,963

227.219

229.352

231.373

233.296

235.128

236.879

238.554

240.161

241.705

2_3.191

244.622

246.003

247.335

248.623

249.870

251.077

252.2_6

253,380

254.481

255.550

256,588

257.596

258.578

259,533

260.463

261.369

262.251

263.111

263.950

264.769

265.568

266.348

267.110

267.854

268.581

269.293

269.988

270,670

271.335

271,988

272.626

273.252

273.864

274,464

275.053

H°(T)

kJ/tool

-8.825

-5.918

-2.989

0.000

0.058

3.277

6.645

i0.117

13.669

17.280

20.934

24.625

28,346

32.093

35.863

39.654

43.467

47.298

51.146

55.0]0

58.887

62.776

66.673

70.575

74.479

78. 381

82.276

86.162

90.035

93.891

97.727

101.540

105.327

109.087

112.816

116.515

120.180

123.812

127.410

130.972

134.498

137.988

141.443

144.863

148.247

151.597

154.913

158.195

161.444

164,661

167.846

171.001

174.126

177.212

180.289

185.330

186.343

189.331

192.294

195.233

198.148

201.041

.O°_K

Jlmol.K

INFINITE

229.553

205.599

202.792

202.793

204.044

206.455

209.212

212.020

214.768

217.412

219.936

222.338

224.622

226.797

228.869

230.846

232.735

234.544

236.276

237.941

239.540

241.081

242.566

243.998

245.383

246.721

248,016

249.271

250.487

251.666

252.812

253.924

255,00_

256.055

257.076

258.071

259.039

259.982

260.900

261.796

262.670

263.521

264.352

265.164

265,956

266.731

267.486

268.226

268.948

269.655

270.346

271.023

271.685

272.335

272.970

273.592

274.202

274.800

275.386

275.960

276.524

T

K

0

100

200

298.15

300

400

500

600

700

800

900

1000

ii00

1200

1300

1400

1500

1600

1700

1800

1900

2000

210D

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

40 NASA/TP-3287/REV l
TABLE IlL19 - SELECTED THERMODYNAMIC FUNCllONS FOR Fe(a,_,L_

T CO HO(T).HO(0) sO(T) .{GO(T)_HO(0)}K HO(1] .G°_K T

K J/m_-K kJ/mol J/mol.K J/moI.K kJ/m_ J/m_-K K

0 0.000 0.000 0.000 0.000 -4.507 INFINITE 0

I00 12.i01 0.423 6.065 1.835 -4.084 46.905 100

150 18.110 1.192 12.221 4.274 -3.315 34.321 150

200 21.588 2.192 17.949 6.989 -2.315 29.524 200

250 23.742 3.330 23.018 9.698 -1.177 27.726 250

298.15 25.094 4.507 27.321 12,204 0,000 27.321 298.15

300 25.140 4.553 27,476 12.299 0.046 27.323 300

350 26.287 5.840 31.439 14.753 1.333 27.630 350

400 27.386 7.181 35.021 17.069 2.674 28.336 400

450 28.518 8.579 38.312 19.248 4.072 29.263 650

500 29.702 10.034 41,377 21.309 5.527 30.323 500

550 30.850 11.548 44.261 23.265 7.041 31.459 550

600 32.049 13.120 46.997 25.130 8.613 32.642 600

700 34.602 16.446 52,119 28.625 11.939 55.063 700

800 37,949 20.060 56.960 31.865 15.555 57.499 800

900 43.095 24.089 61.679 34.913 19.582 59.921 900

950 43.800 26.273 64.054 36.398 21.766 41.142 950

1000 54.434 28,836 66.672 37.836 24.329 42.343 1000

0 72 572 30 531 68 341 38 699 26 024 43.075 1030 1o3 .... 8 26'795 43 022 1o4o 1040 81.660 31.302 6_.p_6 38.98 . '47 1041

1041 82 670 31 384 ov._o5 59.017 26.877 _5.5 ......

_= _o42 831680 31_467 692_ ...... _9:_ ...... z_:9_ ...... ?_:_5_...... _---

;--;_;_ ...... ;_;;; ...... _;_;;5...... ;;_45 39.046 26.960 _3372 1042

O0 46 401 34 479 72 062 40 717 29 972 44.815 1100

_o_ 41"422 58"126 751260 431059 331619 46.866 1184

........ _;;_-- ..... 39.026 .................................76.020 43.059 34.519 46.866 1184

1200 34.016 39.569 76.476 43.502 35.062 47.258 1200

1300 34.853 43.012 79.231 46.145 38.505 49.612 1300

1400 35.690 46.5_0 81.845 48.602 42.033 51.821 1400

1500 36.526 50.150 84.336 50,903 45.643 55.907 1500

00 37.365 53.845 86.720 55.067 49.338 55.884 1600 _65 37.907 56291 88.218 54.410 51:_ ...... _:55_...... _---

00 41 463 58 573 89 580 55 125 54 066 57.776 1700 17 .... 2 770 91 978 57.106 58'263 5961o 18oo

1800 42.468 6 . , 59 772 1809

................ + 18o9 42._ ...... __5_• ...... _L 19° _................................................... 57.280 58.645

809 46.024 76.959 99.823 57.280 72.452 59.772 1809

I _900 46.024 81.148 102,082 59.372 76.641 61.744 1900

2000 46.024

2100 46.024

2200 46.024

2300 46.024

2_00 46.024

2500 46.024

2600 46.024

2700 46.024

2800 46.02_

2900 46,024

3000 46.024

3100 46.024

3200 46.024

3300 46.024

3400 46.024

5500 46.024

3600 46.024

3700 46.024

3800 46.024

5900 46.024

4000 46.024

4100 46.024

4200 46.024

4500 46.024

4400 46.024

4500 46.024

4600 46.024

4700 46.024

4800 _6.024

4900 46.024

5000 46.024

85,750

90.352

94.955

99.557

104.160

108.762

113.364

117.967

iZ2.569

127.172

151.774

156.376

140.979

145.581

150.184

154.786

159.388

163.991

168.593

173.196

177.798

182.400

187.003

191.605

196.208

200.810

205.412

210.015

214.617

219.220

223.822

104.442 61.567 81.243 63.821 2000

I06,688 63.663 85.845 65.809 2100

108.829 65.668 90.448 67.716 2200

110.875 67.589 95,050 69.549 2500

112.833 69.4_4 99.653 71.31Z 2400

114.712 71.207 104.255 73.010 2500

116.517 72.916 108.857 74.669 2600

118.254 74.563 113.460 76.232 2700

119.928 76.153 118.062 77,765 2800

121.545 77.691 122.665 79.245 2900

123.103 79.179 127.267 80.681 3000

124.613 80.620 131.869 82.074 3100

126.074 82.018 136.472 83.426 3200

127.490 83.374 141.074 84,740 3300

128.864 84.692 145.677 86.018 3_00

130.198 85.973 150.279 87.261 5500

131.495 87.220 156.881 88.472 5600

132.756 88,434 159,484 89.652 3700

133.983 89.616 164.086 90.802 3800

135.178 90.769 168.689 91.925 3900

136.344 91.894 173.291 93.021 4000

137,480 92,992 177.893 94.092 6100

158.589 9a.065 182.496 95.138 4200

159.672 95.115 187.098 96.161 4300

140.730 96.158 191.701 97.162 6400

141,765 97.140 196.303 98.142 4500

142.776 98,121 200,905 99,101 4600

143.766 99.082 205.508 100.041 4700

144.735 100.023 210.I10 100.962 4800

145.684 100.945 214,713 101,865 4900

146.614 101.849 219.315 102.751 5000

aMaximum tau'nbd,,_-_nsitio_ point at 1042 K,

41

NASA/TP-3287/REV 1
TABLE IlL19 - Concluded.

T C° H°(T)-H°(0) sO(T) .{GO(T).Ho(O)}K

K Jlm_-K kJlmol J/mol-K J/mol-K

5100 46.024 228.42_ 147,525 102.736

5200 46.024 235.027 148.419 103.606

5300 46.024 237.629 149.295 104.460

5400 46.024 242.232 150.156 105.298

5500 46.024 246.834 151.000 106.121

5600 46.024 251.436 151.829 106.930

5700 46.024 256.039 152.644 107.725

5800 46.024 260.641 153.445 108.506

5900 46.024 265.244 154.251 109.275

6000 46.024 269.846 155.005 110.030

H°ff)

kJ/tool

223.917

228.520

253.122

237.725

242.327

246.929

251.552

256.134

260.737

265.339

.Gomfr

J/moI-K

103.620

104.473

105.310

106.133

106.941

307.735

108.516

109.283

110.039

110,782

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

42 NASA/TP-3287/REV l
TABLE #1.20 - SELECTED THERMODYNAMIC FUNC'RONS FOR Ge(cr.l)

T CO HO(T).HO(0) so(T) .{GO_.HO(0) }_ HO0_ .Go(-D_ T

K J/m_kK kJ/m_ J/m_-K Jtmo_K _/mol J/rr_-K K

0 0.000 0.000 0.000 0.000 -4.636 INFINITE 0

100 13.820 0.620 9.866 3.666 -4.016 50.030 100

200 21.130 2._35 22.175 10.000 -2.201 33.182 200

298.15 23.222 4.636 31.090 15.560 0.000 31.090 298.15

300 23.2_9 4.679 31.234 15.636 0.043 31.090 300

350 23.861 5.838 34.866 18.129 1.222 31,376 350

400 24.310 7.063 38,083 20.426 Z.426 32.017 400

450 24.665 8.287 40.968 22.551 3.651 32.854 450

500 24.962 9.528 43.582 24.526 4.892 33.798 500

600 25.452 12.050 48.178 28.095 7.414 35.822 600

700 25.867 14.616 52.133 31.253 9.980 37.876 700

800 26.240 17,222 55,612 3_.085 12.586 39.880 800

900 26.591 19.864 58.723 36.653 15.227 41.804 900

lOOO 26.926 22,560 61.542 39.003 17.903 43,639 lOOg

1100 27,252 25.249 6_.I24 41.171 20.612 45.386 1100

1200 27,571 27,990 66.509 63.184 23.353 47.048 1200

cr 1211.40 27.608 28.304 66.770 43.405 23.668 47.232 1211.40

...... ...... ...... ...... ...... ......

1300 27.600 67.780 99.286 47.148 63.143 50.714 1300

1400 27.600 70 540 101.331 50.946 65.903 54.258 1400 " 54.369 68.663 57._60 1500

1500 27.600 73.300 103.236

1600 27.600 76.060 105.017 57.480 71.623 60.377 1600

1700 27.600 78.820 106.690 60.326 74.183 63.053 1700

1800 27.600 81.580 108.268 62.946 76.943 65.521 1800

1900 27.600 84,340 109,760 65,371 79.703 67.811 1900

2000 27.600 87.100 111.176 67.626 82.463 69,944 2000

2100 27.600 89.860 112.522 69.732 85.223 71.940 2100

2200 27.600 92.620 113,806 71.706 87.983 73,814 2200

2300 27.600 95.380 115.033 73.564 90.743 75.579 2300

2400 27.600 98.140 116.208 75.316 95.505 77.2_8 2400

2500 27.600 100.900 117.334 76.975 96.263 78.829 2500

2600 27.600 10_.660 118.417 78.548 99.023 80.331 Z600

2700 27.600 106.420 119._58 80.044 101.783 81.761 2700

2800 27,600 109.180 120,462 81.470 104.543 83.125 2800

2900 27.600 111.940 121._31 82.831 107.303 84.430 2900

3000 27.600 114.700 122.366 84.133 110.063 85.679 3000

3100

3200

3300

3400

3500

3100 27.600 117.460 123.271 85.381 112.823 86.877

3200 27.600 120.220 124.148 86.579 115.583 88.028

3300 27.600 122.980 124.997 87.730 118.343 89.135

3400 27.600 125.740 I25.821 88.839 121.103 90.202

3500 27.600 128.500 126.621 89.907 123.863 91.232

3600 27.600 131.260 127.398 90.938 126.623 92,225 3600

3700 27.600 134.020 128.155 91.933 129.383 93.186 3700

3800 27.600 136.780 128.891 92.896 132.143 94.116 3800

3900 27.600 139,540 129.608 93.828 134.903 95.017 3900

4000 27.600 142.300 130.306 94.732 137,663 95.891 4000

4100 27.600 145.060 130.988 95.608 140.423 96.738 4100

4200 27.600 147.820 131.653 96.458 143.183 97.562 4200

4300 27.600 150.580 132.303 97.284 1_5.943 98.362 4300

4400 27.600 153.340 132.937 98.087 148.703 99.141 4400

4500 27.600 156.100 133.557 98.868 151._63 99.899 6500

4600 27.600 158.860 134.164 99.629 154.223 100.637 4600

4700 27.600 161.620 134.757 100.370 156.983 101.357 4700

4800 27.600 164.580 135.339 101.093 159.743 102.059 _800

4900 27.600 167.140 135.908 101.798 162.503 102.744 4900

5000 27.600 169.900 136.465 102.485 165.263 103.413 5000

5100 27,600 172.660 137.012 103.157 168.023 104.066 5100

5200 27.600 175.420 137.5_8 103.813 170.783 104.705 5200

5300 27.600 178.180 138.073 104.455 173.543 105.329 5300

5400 27.600 180.9_0 138.589 105.082 176.303 105.941 5400

5500 27.600 183.700 139.096 105.696 179.063 106.539 5500

5600

57O0

5800

5900

6000

5600 27.600 186.660 139.593 106.297 181.823 107.125

5700 27.600 189.220 140.082 106.885 184.583 107.699

5800 27.600 191.980 140.562 107.46Z 187.343 108.261

5900 27.600 194.740 141.033 108.027 190.103 108,813

6000 27.600 197.500 141._97 108.561 192.863 109.353

43

NASA/TP-3287/REV 1
TABLE tU.21.

- SELECTED THERMODYNAMIC FUNCTIONS FORH2

TC° H°('T).HO(0) sO(r-) .{Go(.T).HO(0)}_ Ho(-r,)

K JIm_K k_mol J/r'noI.K J/m_-K kJtmol 0 0.000 0.000 0.000 0.000 -8.468

50 37.970 1.365 77.632 50,332 -7.103

I00 28,155 2.999 100,727 70.736 -5._69

150 26.556 4.345 111.666 82.699 -4.123

200 27.447 5.693 119.412 90.947 -2.775

250 28.344 7.089 125.642 97.286 -1.379

298.15 28.836 8.468 230.681 102.279 0.000

300 28.849 8.521 130.858 102.454 0,053

350 29.081 9.969 135.325 106.842 1.501

400 29.181 11.426 139.215 110.650 2.958

500 29,260 14.349 145.737 117,039 5.881

600 29.327 17,278 151.077 122.280 8.810

700 29.440 20.216 155,605 126.725 11.748

800 29.623 23.169 159,548 130.587 14.701

900 29.880 26.143 163.051 134.003 17.675

1000 30.204 29.147 166.215 137.068 20.679

ii00 30.580 32.186 169,111 139.851 25.718

1200 30.991 35.264 171.790 142.402 26.796

1300 31,422 38.385 174.288 144.760 29.917

1400 31.860 41.549 176.632 146.953 33.081

1500 32.296 44.758 178.846 149.007 36.289

1600 32.724 48.009 180.944 150.938 39.540

1700 33.138 51.302 182.940 152.762 42.834

1800 33.535 54.636 184.845 154.492 46.168

1900 33.915 58.008 186.669 156.138 49.540

2000 34.277 61.418 188.418 157.709 52.950

2100 34.622 64.863 190.099 159.212 56.395

2200 34.949 68.342 191.717 160.652 59.874

2300 35.259 71.852 193.277 162.037 63.38_

2400 35.555 75.393 194.784 163.370 66.925

2500 35.837 78.963 196.241 164.656 70.495

2600 36.106 82.560 197.652 165.898 74.092

2700 36.363 86.184 199.020 167.100 77.716

2800 36.610 89.832 200.347 168.264 81.364

2900 36.847 93.505 201.636 169.393 85.037

3000 37.076 97.202 202,888 170.487 88.734

3100 37.298 100.920 204.108 171.553 92,452

3200 37.513 104.661 205.295 172.588 96.193

3300 37.723 108.423 206.453 173.597 99.955

3400 37.928 112.205 207.582 174.580 103.737

3500 38.129 116.008 208.685 175.540 107.540

3600 38.326 119.831 209.761 176.474 111.363

3700 58.520 123.673 210.814 177.389 115.205

3800 38.711 127.536 211.84_ 178.282 119.067

3900 38.899 131.416 212.852 179.156 122.947

4000 39.085 135.316 213.839 180.010 126.848

4100 39,269 139.233 214.807 180.848 130.765

4200 39.450 143.169 215.755 181.667 134.701

4300 39.629 147.123 216.685 182.470 138.655

4400 39.806 151.095 217.598 183.258 142.627

4500 39,980 155.084 218,495 184.032 146.616

4600 40 151 159.091 219.376 184.791 150,623

4700 40.318 163.114 220.241 185.536 154.646

4800 40.482 167.154 221.091 186.267 158.686

4900 40.641 171.210 221.928 186.987 162.742

5000 40.796 175.282 222.750 187.694 166.814

5100 40.945 179.370 223.560 188.390 170.902

5200 41.088 183.471 224.356 189,073 175.003

5300 41.226 187,587 Z25,140 189.746 179.119

5400 41.357 191.716 225.912 190.409 183,248

5500 41.480 195.858 226.672 191.062 1871390

5600 41,597 200.012 227,420 191,704 191.544

5700 41.704 204.177 228.158 192.338 195.709

5800 41.80_ 208.353 228.884 192.961 199.884

5900 41.894 212.538 229.599 193.576 204.069

6000 _1.975 216.731 230.304 19_.182 208.263

6200 42.108 225.140 231.683 195.370 216.672

6400 42.201 233.572 233.021 196.526 225.104

6600 42.253 242.018 234.320 197.651 233.550

6800 42.264 250.470 235.582 198.748 242.002

7000 42.234 258.920 236.807 199.819 250.452

7200 42.165 267,360 237.996 200.863 258,892

7400 42.056 275.783 239.150 201.882 267.315

7600 41.911 284.180 240.269 202.877 275.712

7800 41.732 292.546 241.356 203.851 284.077

8000 41.520 300.871 242.410 204.802 292.403

-G°('r)K

J/mo_K

INFINITE

219.694

155.417

139.153

133.287

131.158

130.681

130.681

131.036

131.820

133.975

136.394

138.822

141.172

143.412

145.536

147.549

149.459

151.274

153.002

154.653

136.231

157.743

159.196

160.595

161.943

163.244

164.501

165.719

166.898

168,043

169.155

170.236

171.288

172.313

173.310

174.285

175.235

176.163

177.071

177.959

178.827

179.677

]80.510

181,327

182.127

182.913

183.683

184.440

185.183

185.914

186.632

187,338

188.032

188.715

189.387

190,050

190.702

191.344

191.977

192.601

193.216

193.823

194.421

195.011

195.594

196.736

197.849

198.934

199.994

201.028

202,039

203.027

203,991

204.936

205.860

TK0

50

lO0

150

200

250

298

300

350

400

500

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2_00

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

_700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

.15

44 NASA/TP-3287/REVl
TABLE fll.21.- Concluded.

T C° H°(_'H°(0) $°G) "{G°(T)'H°(0)}_

K J/m_-K kJ/mol J/mot-K J/moI-K

8200 41.280 309.152 243.432 205.731

8400 41.014 317.381 244.424 206.641

8600 40.724 325.556 245.385 207.530

8800 40.415 333.670 246.318 208.401

9000 40.088 341.720 247.223 209.255

9200 39.745 349.704 248.100 210.089

9400 39.391 357.618 248.951 210.907

9600 39.027 365.460 249.776 211.708

9800 38.655 373.228 250.577 212.493

10000 38.277 380.922 251.354 215,262

10500 37.321 399.823 253.199 215.121

ii000 36.367 418.244 254.914 216.891

11500 35.432 436.193 256.510 218.580

12000 34.530 453.681 257.999 220.192

12500 33.669 470.730 259.390 221.731

13000 32.855 487.359 260.695 223.205

13500 32.089 503.593 261.921 22_.617

14000 31.373 519.457 263.074 225.970

14500 30.706 534.975 264.163 227.268

15000 30.085 550.171 265.194 228.516

15500 29.510 565.068 266.171 229.715

16000 28.976 579.688 267.099 230.868

16500 28.483 594.051 267.983 231.980

17000 28.025 608.177 268.827 233.052

17500 27.602 622.083 269.653 234,085

18000 27.211 635.785 270.405 235.083

18500 26,848 649.299 271.145 236.047

19000 26.511 662,638 271.857 236.981

19500 26.200 675.815 272,541 237.884

20000 25.910 688.8fil 273.201 238.759

H°G)

kJ/mol

300.684

308.913

317.088

325.202

533.252

341.236

349.150

356.992

36_.760

372.453

391.355

409.776

427.725

445.213

462.262

478.891

495.125

510.989

526.507

541,703

556.600

571,220

585.583

599.709

613.615

627.317

6_0.831

654.170

667.347

680.373

.G°(T)_

Jlm_-K

206.764

207.649

208.515

209.364

210.195

211.010

211.808

212.590

213.357

214.109

215.928

217.661

219.316

220.897

222,409

223.857

225.245

226.574

227.852

229.080

230.261

231.397

232.493

233.550

234.569

235.554

236.505

237._27

238.318

239.182

T

K

8200

8400

8600

8800

9000

9200

9fi00

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

lqO00

14500

15000

15500

16000

16500

17000

1750O

18000

18500

19000

19500

20000

45

NASA/TP-3287/REV 1
TABLE n122. •SELECTED THERMODYNAMK; FUNC_ONS FOR He

T C° HO(T_HO(o) 80(_ .{GO_%HO(0)}K Ho(_

K Nn_kK k_rr_ JlmoI-K J/m_,-K kNm_

0 0.000 0.000 0.000 0.000 -6.197

100 20.786 2.079 103.446 82.660 -4.119

200 20,786 4.157 117.854 97.068 -2,0_0

298.15 20.786 6.197 126.154 105.367 0,000

300 20.786 6,236 126.282 105.496 0.038

400 20.786 8.315 132.262 111.476 2.117

500 20.786 10.393 136.900 116.114 4.196

600 20.786 12.472 140.690 119.904 6.274

700 20.786 14.550 143.894 123.108 8.353

800 20.786 16.629 146.670 125.884 10.632

900 20.786 18,708 149,118 128.332 12.510

1000 20.786 20.786 151.308 130.522 1_.589

1100 20.786 22.865 153.290 132.503 16.667

1200 20.786 24.944 155.098 134.312 18.746

1300 20.786 27.022 156.762 135.976 20.825

1_00 20,786 29,101 158.302 137.516 22.903

1500 20.786 31.179 159.736 138.950 24.982

1600 20,786 33.258 161.078 140.292 27.061

1700 20.786 35.337 162.338 141.552 29.159

1800 20.786 37.q15 163.526 1_2.740 31.Z18

1900 20.786 39.494 16_.650 143.864 33.296

2000 20.786 41.573 165.716 1_.930 35.375

2100 20.786 43,651 166.730 145.944 37._54

2200 20.786 45.730 167.697 146.911 39.532

2300 20,786 47.808 168.621 147.835 41.611

2400 20.786 49.887 169.506 148.720 43.690

2500 20.786 51.966 170.355 149.568 45.768

2600 20.786 54.044 171.170 150.384 47.847

2700 20.786 56.123 171.954 151,168 49.926

2800 20.786 58.202 172.710 151,924 52.004

2900 20.786 60.280 173.440 152.655 54.085

3000 20.786 62.359 17_.144 153.358 56.161

5]00 20.786 64.437 17_,826 154.040 58.240

5200 20.786 66.516 175.486 154.700 60.319

5300 20.786 68.595 176.126 155.339 62.597

3400 20.786 70.673 176.746 155.960 64._76

5500 20.786 72.752 177.349 156.562 66.555

3600 20.786 74,831 177.934 157,148 68.633

570_ 20.786 76.909 178.504 157.717 70.712

3_00 20.786 78.988 179.058 158.272 72.790

3900 20.786 81.066 179.598 158.812 74.869

600_ :0.786 83.145 180.124 159,338 76.948

_)0o 20.786 85.226 180.638 159.851 79.026

_=00 ;0.786 87.502 181.138 160.352 81.105

_3cn 20786 89.581 181.628 160.841 83.184

_0o Z0.786 91.460 182.105 161,319 85.262

4500 20.786 93.538 182.573 161.786 87.341

_600 20,786 95.617 183.029 162.243 89.419

_70C ;0 786 97.695 183.476 162.690 91.498

_800 20.786 99.774 183.914 163.128 93.577

&gO0 20.786 101.853 184.3_3 163.556 95.655

5000 Z0.786 103.931 184.763 163.976 97.734

5%_0 20.786 106.010 185.174 164.388 99.813

5200 20.786 108,089 185.578 164.792 101.891

53_0 20.786 110.167 185.974 165.188 103.970

5_00 20.786 112.2_6 186.362 165.576 106.048

5500 Z0.786 114.325 186.7_4 165.957 108.127

56CC 20.786 116.405 187.118 166.332 110.206

5700 20.786 I18._62 187.486 166.700 IIZ.284

5803 20.786 120.560 187.848 167.061 114.563

5900 20.786 122,639 188.203 167.417 116.442

6000 20.786 124.718 188.552 167.766 118.520

6200 20.786 128.875 189.234 168.448 122.677

6400 20.786 133.052 189.894 169.108 126.835

6600 20,786 137.189 190.534 169.747 130.992

6800 20.786 141.347 191.154 170.368 135.149

7000 20.786 145.504 191.757 170.970 159.306

7200 20.786 149.661 192.342 171.556 143.464

7400 _0.786 153.818 192.912 172,125 147,621

7600 20.786 157.976 193.466 172.680 151.778

7800 20,786 162.155 194.006 173.220 155.936

8000 20.786 166.290 194.532 175.746 160.093

-oO_

_mokK

INFINITE

144,634

128.055

126.154

126.154

126.969

128,509

130,233

131.962

133.631

135.218

136.720

138,137

139.476

140.743

141.943

143.082

144.165

145.197

146.185

147.126

148.029

148.895

149.728

150.530

151.302

152.047

152,767

153.463

154.137

154.791

155,424

156.039

156.656

157.217

157,783

158.333

158.869

159.592

159.905

160.q01

160.887

161. 363

161.828

162. 283

162,728

163.163

163.590

164.009

164.419

164.821

165.216

165.603

165.983

166.357

166.724

167.084

167.439

167.787

168.150

168.467

168.799

169.447

170.076

170.686

171,279

171,856

172.417

172.963

173.495

174.014

174.521

T

K

0

100

200

298

300

4O0

500

6O0

70O

8O0

9O0

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

720"0

7400

7600

7800

8000

.15

46 NASA/TP-3287/REV l
T

K

8200

8_00

8600

8800

9000

9200

9600

9600

9800

I0000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

C °

J/m_-K

20.786

20.786

20.786

20,786

20.786

20.786

20.786

20,786

20.786

2O.786

20,786

20.786

20.786

20.786

20.787

20.787

20.787

20.788

20.790

20.792

20.795

20.800

20.807

20.817

20.829

20.833

20.862

20.860

20.882

20.910

TABLE W11.22- Concluded.

HO(,T).HO(0) sO0 .) .{ GO(T).HO(0)}K H°(T) .G°('r)_ T

kJ/mol d/moI-K J/m_-K _/m_ _moi-K K

170.667 195.045 176.259 166.250 175.015 8200

174.605 195.566 174.760 168.607 175.698 8600

178.762 196.036 175.249 172.565 175.970 8600

182.919 196,513 175.727 176,722 176.431 8800

187.076 196.980 176.194 180.879 176.883 9000

191.234 197.637 176.651 185.036 177.325 9200

195.391 197.886 177.098 189.196 177.757 9600

199.548 298.322 177.536 193.351 278.181 9600

203.705 198.751 177.966 197.508 178.597 9800

207.863 199.171 178.386 201.665 179.006 10000

218.256 200,185 179.398 212.058 179.989 10500

228.649 201.152 180.365 222.652 180.929 II000

239.042 202.076 181,289 232.845 181.828 11500

249.435 202.960 182.174 243.238 182.691 12000

259.829 203.809 183.023 253.631 183.518 12500

270.222 204.626 183.838 264.025 186.315 13000

280.616 205.609 184.622 276.418 185.081 13500

291.009 206.165 185.378 286.812 185.821 14000

301.406 206.896 186.108 295.206 186.535 16500

311.799 207.599 186.812 305.602 187.226 15000

322.196 208.281 187.496 315.998 187.894 15500

332.595 208.961 188.15_ 326.397 188.541 16000

362.996 209.581 188.794 336.799 189.]69 16500

353.602 210.203 189.414 367.205 189.779 17000

363,812 210.806 190.017 357.615 190.371 17500

376.215 211.392 190.602 368.018 190.967 18000

386.625 211.963 191.172 378.428 191,507 18500

395.050 212.519 191.726 388.853 192.053 19000

605.484 213.061 192.267 399.286 192.584 19500

615.931 213.590 192,793 609.734 193.103 20000

NASA/TP-3287/REV 1 47
TABLE UL23.- SELECTED THERMODYNAMIC FUNCTIONS FOR Hg(cr,_)

T cO H°(l')'H°( 0) S°(T) -{G°(l_-H°(0)}/T H°(T) -G°( D/I" T

K J/m_oK kJ/mol J/mol-K J/moI-K kJ/mol J/mokK K

0 0. 000 0. 000 0. 000 0.000 -9.343 INFINITE 0

100 24. 255 1.706 37.219 20. 159 -7.637 115. 589 100

150 25.878 2.963 47. 393 27.640 -6.380 89.926 150

200 27.275 4,291 55. 022 33. 567 -5.052 80.282 200

cr 234.29 28.485 5.246 59.428 37.037 -4.097 76.915 234.29

l 234.29 28.476 7.541 69.225 37 037 -1.802 76 915 234.29

250 28.351 7.988 71.069 39 117 -1.355 76 489 250

298.15 27.978 9.343 76.028

500 27.963 9.395 76,201

350 27.659 10.784 80.486

400 27.414 12.160 84.161

450 27.267 13.527 87,381

500 27.175 14.888 90.248

550 27.129 16.245 92.836

600 27.139 17.602 95,197

700 27.291 20.322 99.389

800 27.582 23,065 103.052

900 27.896 25.839 106.318

1000 28.210 28,644 109,274

1100 28.523 31.481 111.977

1200 28.837 34.349 114.472

1300 29.151 37.248 116.793

1400 29.465 40.179 118.965

1500 29.778 43.141 121.008

1600 30,092 46,135 122.940

1700 30.406 49.159 124,774

1800 30.719 52.216 126.521

1900 31.033 55.303 128.190

2000 31.347 58.422 129.790

44 691

44 884

49 675

53 761

57 321

60 472

0.000 76 028 298

0,052 76 028 300

1.441 76 369 350

2.817 77 118 400

4.184 78.083 _50

5.545 79.158 500

63.300 6.902 80.287 $50

65.860 8.259 81.432 600

70,358 10.979 83,705 700

74.221 13.722 85.899 800

77.608 16.496 87.989 900

80.630 19.301 89,973 I000

83.358 22.138 91.852 1100

85.848 25.006 93.634 1200

88.141 27.905 95.328 1300

90.266 30.836 96.939 1400

92.247 33.798 98.476 1500

94.106 36.792 99.945 1600

95.857 39.816 101.353 1700

97.512 42.873 102.703 1800

99.083 45.960 104.001 1900

100.579 49.079 105.250 2000

.15

48 NASA/TP-3287/REV 1
TABLE Itl.24. - SELECTED THERMODYNAMIC FUNC_ONS FOR t2(_,_

T co HO(.0.HO(o ) sOcD .{Goco_O(o)}_ Hoco .G°03K T

K J/m_-K kJ/tool J/moI-K J/moI-K kJ/tool J/moI-K K

0 0.000 0.000 0.000 0.000 -13.196 INFINITE 0

5 0.580 0.001 0.192 0.048 -13.195 2639.248 5

I0 4.030 0.011 1.464 0.364 -13.185 1319,964 I0

15 10.250 0.046 4.226 1.159 -13,150 880.893 15

20 16.180 0.112 8.000 2,400 -13.084 662.200 20

25 21.510 0.207 12.201 3.921 -12.989 531.761 25

30 25.760 0.326 16.518 5.651 -12.870 465.518 30

35 28.910 0.462 20.732 7.532 -12,734 384,561 35

60 31.620 0.619 24.773 9.298 -12.577 339.198 40

65 33.930 0.778 28.635 11.346 -12.418 304.591 45

50 35.860 0.953 32.317 13,257 -12.243 277.177 50

60 39,090 1.328 39.146 17.013 -11.868 236.946 60

70 41.650 1.733 45.380 20.623 -11.463 209.137 70

80 63.320 2.158 51.053 24.078 -]1.038 189.028 80

90 44.740 2.598 56.237 27.370 -10.598 173.993 90

i00 45.650 3,051 61.007 30.497 -10.145 162.457 I00

ii0 46.860 3.514 65.421 33.676 -9.682 153.439 Ii0

120 67.730 3.987 69.538 36.313 -9.209 146.280 120

130 68.480 4.468 73.387 59.018 -8,728 140.525 130

I40 69.020 4.956 77.002 61.602 -8.260 135.859 160

150 49.590 5,448 80.400 44.080 -7.768 132.053 150

160 50.070 5.947 83.617 46.448 -7.269 128.923 160

170 50.690 6.449 86.663 48.728 -6.767 126.351 170

180 50.870 6.956 89.563 90.919 -6.240 124.230 180

190 51.230 7.467 92.324 53,024 -5,729 122,477 190

200 51.570 7.981 96.960 55.055 -5.215 121.035 200

210 52.050 8.499 97.487 57.016 -4.697 119.854 210

220 52.460 9.020 99.910 58.910 -4.176 118.892 220

230 52.790 9.546 102.249 60.745 -3.650 118.119 230

240 53.050 10.076 I06,504 62.521 -3.120 117.504 240

250 53.250 10.607 106.671 66.Z43 -2,589 117.027 250

260 53.420 11.140 108.765 65.917 -2.056 116.671 260

270 53,610 11.675 110.784 67.543 -1.521 116.617 270

280 53.860 12.213 112.738 69.120 -0.983 116.269 280

290 54 150 12.752 114.629 70.657 -0.444 116.160 290

298.15 54 440 13.196 116.139 71.879 0.000 116 139 298,15

300 54 517 13.297 116.476 72.153 0.I01 116 139 300

320 55 360 14.396 120,021 75.033 1.200 116 271 320

360 56 952 15.518 123.424 77.783 2.322 116 595 360

360 58 785 16.675 126.730 80.611 3.679 117 066 360

380 60 811 17.871 129.962 82,933 4.675 117 659 380

cr 386.75 61 531 18.286 131.639 83.763 5,658 117 883 386.75

............................................................................................

386.75 79.555 33.949 171.543 83.763 20.753 117.883 386.75

600 79.555 35.003 174.223 86.715 21.807 119.705 400

500 79.555 42.959 191.975 106.058 29.763 132.450 500

600 79.555 50.914 206.480 121.623 37.718 143.616 600

700 79,555 58.870 218,743 134,644 45.674 153.495 700

800 79.555 66.825 229.366 165.835 53.629 162.330 800

900 79.555 74.781 238.737 155.647 61.585 170.309 900

I000 79.555 82.736 247.119 164.383 69.540 177.579 i000

I100 79.555 90.692 254.701 172.254 77.696 184.250 1100

1200 79.555 98.647 261.623 179.417 85._51 190.414 1200

1300 79.555 106.603 267.991 185.989 93.407 196.140 1300

1400 79.555 116.558 273.887 192.059 101.362 201.685 1400

1500 79.555 122.516 279.375 197.700 109.318 206.497 1500

1600 79.555 130.469 284.510 202.967 117.273 211.214 1600

1700 79.555 138.425 289.335 207.906 125.229 215.669 1700

1800 79.555 146.380 293.880 212.558 133.184 219.889 1800

]900 79.555 154.336 298.181 216.952 141.140 225.897 1900

2000 79.555 162.291 302.262 221.116 149.095 227.714 2000

2100 79.555 170.267 306,143 225.074 157,051 231,357 2100

2200 79.555 178.202 309.844 228.843 165.006 236.842 2200

2300 79.555 186.158 313,381 232.643 172.962 238.180 2300

2600 79.555 196.113 316.767 235,886 180.917 261.384 2400

2500 79.555 202.069 320.014 239,187 188.873 264.465 2500

2600 79.555 210.024 323.136 262.356 196.828 267.431 2600

2700 79.555 217,980 326.137 245,606 204.784 250.291 2700

2800 79,555 225.935 329.030 248.339 212.739 253,052 2800

2900 79.555 233.891 331.822 251.170 220.695 255.720 2900

3000 79.555 241.866 334.519 253.903 228.650 258.302 3000

3100 79.555 249.802 337.127 256.546 236.606 260.803 3100

3200 79.555 257.757 339.653 259.104 246.561 263.228 3200

3300 79.555 265.713 342.101 261.582 252.517 265.581 3300

3400 79.555 273.668 344.476 263.985 260.472 267.867 3400

3500 79.555 281.624 346.782 266.318 268.428 270.089 3500

3600 79.555 289.579 349,023 268.585 276,383 272.250 3600

3700 79.555 297,535 351.203 270.788 286.339 276.355 3700

3_00 79.555 305,690 555.525 272,932 292,294 276.405 3800

3900 79.555 313,446 355.391 275,020 300.250 278.604 3900

4000 79.555 321._01 357.605 277.055 308.205 280.354 4000

NASA/TP-3287/REV 1 49
T

K

4100

4200

4300

4400

4500

4600

4700

¢o800

4900

5000

5100

5200

5300

5_,00

5500

5600

5700

5800

5900

60OO

Co

J/m_-K

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

79.555

HO('I_.H°(0)

kNmol

329.357

337.312

345.268

353.223

361.179

369.134

377.090

385.045

393.001

400.956

408,912

416.867

424.823

432.778

440.734

448.689

456.645

464.600

472.556

480.511

TABLE 111.24..Concluded.

S°(T) .{G°(T).H°(0)}/T

J/moI-K J/moI-K

359,370 279,039

361.287 280,974

363.159 282.864

364.988 284.710

366.775 286.514

368.524 288.277

370.235 290.003

371.910 291.692

373.550 293.346

375.157 294.966

376.733 296.554

378,278 298.111

379.793 299.638

381.280 301.136

382.740 302.606

384.173 304.050

385.581 305.468

386.965 306.862

388.325 308.231

389.662 309.577

Ho_")

_/mol

316,161

324.116

332.072

340.027

347.983

355.938

363.894

371.849

379.805

387.760

395.716

403.671

411.627

419.582

427.538

435.493

443.449

451.404

459,360

467.315

.S°_F

_moI-K

282.257

284.116

285.933

207.709

289.446

291.146

292.811

294.441

296.039

297.605

299.142

300.649

302.128

303.580

305.006

306.407

307.783

309.137

310.467

311.776

T

K

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

59OO

6000

50 NASA/TP-3287/REV l
TABLE lU.25.- SELECTED THERMODYNAMIC FUNCTIONS FOR _cr,i)

T G° HO(1,)_HO(0) sO(T) _{GO(T).HO(0)}_ HO(T) _°(l_ T

K _m_kK kJlmol Jlrnol.K Nrnol-K _/m_ Jlm_-K K

0 0.000 0.000 0.000 0.000 -7.088 1NF$NITE 0

100 24.650 1.733 35.590 18.260 -5.355 59,140 100

200 26.820 _.325 53._67 31.842 -2.763 67.282 200

7.088 64.650 40,907 0.0O0 64.660 298.15 296.15 29,600

300 29,671 7,143 64,863 _1,053 0.055 "6_.680 300

cr 336.86 32.130 8.276 68.422 _3.854 1.188 6_.896 336.86

;- -33686--_2129 10.597 -7_3;_ - - -4_;_ 3_;_; 6;_;;; 3_;_;; 400 31.55_ lZ.60_ _0._4 49.266 5._19 6_..6 400 500 30741 15_20 87_3_ 56.2,4 _632 70.470 500

600 30.158 18.763 93.283 62.011 11.675 73.825 600

700 29.851 21.761 97.905 66.818 I_.673 76.9_ 700

800 29.838 24.7_3 101.887 70.958 17.655 79.818 800

900 30.130 27.739 105._15 74.59_ 20.651 B2._69 900

1000 30.750 30,779 108,618 77,839 25.691 84.927 1000

1100 31.643 33.895 111.587 80.773 26.807 87.217 1100

1200 32.870 37.118 114.391 83._59 30.030 89,366 1200

1300 34.411 qO.q80 117.081 85.9q3 33.392 91.395 1300

i_00 36.268 _4.011 119.697 88.261 36.923 93.323 1400

1500 38.4_0 47.7q_ 122.271 90.442 _0.656 95.167 1500

1600 _0.929 51.710 124.830 92.511 44.622 96.941 1600

1700 43,734 55.9_0 127.39_ 94._8 _B.852 9B.65B 1700

I_00 46.856 60.467 129.980 96.387 53.379 100.325 1800

1900 50.295 65,322 132.605 98.225 58.234 101.956 1900

2000 54,050 70,537 135.278 100.009 63.q49 105.553 ZOO0

2100 58.123 76.1_3 138.013 101.754 69.055 105.130 2100

2200 62.512 82.172 i_0.817 103.466 75.08_ 106.6_B 2200

NASA/TP-3287/REV l 51
TABLE 111.26,• SELECTED THERMODYNAMIC FUNCTIONS FOR Yu"

T C° HO('o.HO(o) sO('].) .{G°('i')-H°(0)}_ HO(T)

K J/m_-K kJ/m_ JlmokK _mo/-K kJ/mol

0 0 000 0.000 0.000 0,000 -6.197

100 20:'786 2.079 141.379 120,593 -4.119

200 20.786 4.157 155,787 135.001 -2.040

298.15 20.786 6.197 164.086 143.300 0.000

300 20.786 6.236 164,215 143,429 0.038

400 20.786 8,315 170,195 149.409 2.117

500 20.786 10.393 174,833 154.047 4.196

600 20.786 12._72 178.623 157.837 6.274

700 20.786 14.550 181.827 161.041 8.353

800 20.786 16.629 184.603 163.817 10.432

900 20.786 18.708 187.051 166.265 12,510

1000 20.786 20.786 189.241 168.455 14.589

1100 20.786 22.865 191.222 170.436 16.667

1200 20.786 24.944 193.031 172.245 18.746

1300 20.786 27.022 194.695 173.908 20.825

1400 20.786 29.101 196.235 175.449 22.903

1500 20.786 31.179 197.669 176.883 24.982

1600 20.786 53.258 199.011 178.224 27.061

1700 20,786 35.337 200.271 179.485 29.139

1800 20.786 37.415 201.459 180.673 31.218

1900 20.786 39.494 202.583 181.797 33.296

2000 20.786 41,573 203.649 182.863 35.375

2100 20.786 43,651 204.663 183.877 37.454

2200 20.786 45.750 205.630 184.844 39.532

2300 20.786 47.808 206.554 185.768 41.611

2400 20.786 49.887 207.439 186.653 43.690

2500 20.786 51.966 208.287 187.501 45.768

2600 20.786 54.044 209.I03 188.316 47.847

2700 20.786 56.123 209.887 189.101 49.926

2800 20.786 58.202 210.643 189.857 52.004

2900 20.786 60.280 211.572 190.586 54.083

3000 20.786 62.359 212.077 191,291 56,161

3100 20.786 64.437 212.759 191,972 58.240

3200 20.786 66.516 213.419 192,632 60.319

3300 20.786 68.595 214.058 193.272 62.397

3400 20.786 70.673 214.679 193.893 64,476

3500 20.786 72.752 215.281 194,495 66,555

5600 20.786 74.831 215.867 195.081 68.633

3700 20.786 76.909 216.436 195.650 70.712

3800 20,786 78.988 216.991 196.205 72,790

3900 20.786 81.066 217.531 196.744 74.869

4000 20,786 83.145 218.057 197.271 76,948

4100 20.786 85.224 218,570 197.784 79.026

4200 20.786 87.502 219.071 198.285 81.105

4300 20.786 89.381 219.560 198.774 85.184

4400 20.786 91.460 220.038 199.252 85.262

4500 20.786 93.538 220,505 199.719 87.341

4600 20.786 95.617 220.962 200.176 89.419

4700 20.786 97.695 221.409 200.623 91.498

4800 20.786 99.774 221.847 201.061 93.577

4900 20.786 101.853 222,275 201.489 95,655

5000 20.786 103.931 222.695 201.909 97.734

5100 20.786 106.010 223.107 202.321 99,813

5200 20.786 108.089 223,511 202.724 101,891

5300 20.786 110.167 223.907 203.120 103.970

5400 20.786 112.246 224.295 203.509 106.048

5500 20.786 114.325 224.676 203.890 108.127

5600 20.786 116.403 225.051 204.265 110,206

5700 20.786 118.482 225.419 204.633 112.284

5800 20.786 120.560 225.780 204,994 114.363

5900 20.786 122.639 226.136 205,349 116.442

6000 20.786 124.718 226.485 205.699 118.520

6200 20.787 128.875 227.167 206.380 122.678

6400 20.787 133.032 227.827 207.040 126.835

6600 20,787 137.190 228.466 207.680 130.992

6800 20.788 141.547 229.087 208,301 135.150

7000 20.789 145.505 229.689 208.903 139.307

7200 20.790 149.663 230.275 209.489 143.465

7400 20.792 153.821 230.845 210.058 147.624

7600 20.795 157.980 231.399 210.613 151.782

7800 20.799 162.139 231.940 211.152 155.942

8000 20.805 166.300 232.466 211.679 160.102

-G°(T)_

_mo_-K

INFINITE

182.567

165.988

164.086

164.087

164.902

166.442

168.166

169.894

171.563

173.151

174.652

176.070

177.409

178.676

179.876

181.015

182.098

183.130

184.116

185.058

185,962

186,828

187.661

188.462

189.235

189.980

190.700

191.396

192.070

192.723

193,357

193.972

194.569

195.150

195.715

196.266

196.802

197.325

197.835

198.334

198.820

199.296

199.760

200.215

200.660

201.096

201.523

201.942

202,352

202.754

203.149

203.536

203.916

204,290

204.656

205,017

205.371

205.720

206.063

206.400

206.732

207.380

208.009

208.619

209.212

209.788

210.349

210.896

211.428

211.947

212.453

T

K

0

100

200

298.15

300

400

500

60O

700

800

90O

1000

I10O

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

52 NASA/TP-3287/REV 1
T

K

8200

8400

8600

8800

9000

9200

96,00

9600

9800

i0000

10500

iI0_0

11500

12000

12500

13000

13500

16,000

16,500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

C°

J/rn_l-K

20.812

20.822

20.836

20.853

20.875

20,903

20.938

20.98,2

21,0:35

21.079

21.276

21.580

21.959

22,46,5

23.166

26,.086

25.079

26.045

27. 096,

28.719

30.580

32.672

36,.982

37.491

40.168

42.977

6,5.876

48.262

6,9.484

50.539

TABLE111.26.- Concluded.

H°(D'H°(0) sO(T) .{GO(D.Ho(O)}K HO_) .oO(T)F T

kJ/moi J/moI-K J/mcl-K kJ/mol J/moI-K K

170.6,61 232.980 212.192 164.264 212.948 8200

174.624 233.6,82 212.693 168.427 213.6,31 8400

178.790 233.972 213.182 172.593 213.903 8600

182.959 234.451 213.660 176.762 214,366, 8800

187.132 234.920 214.127 180,934 214.816 9000

191.509 235.379 216,.58_ 185,112 215.258 9200

195.493 235.829 215.032 189.296 215.691 96,00

199.685 236.270 215.470 193.488 216.115 9600

203,887 236,703 215.898 197,689 216.531 9800

208,086 237,127 216.319 201.889 216.938 10000

218.666 238,160 217.334 212.469 217.925 10500

229.376 239.156 218.304 223,178 218.867 11000

240,218 26,0.120 219.231 236,.020 219,770 11500

25_,250 241.058 220,121 245,053 220,637 12000

262.645 241.988 220.977 256.447 221.6,73 12500

274.6,38 26,2.913 221.803 268.26,1 222.279 13000

286.549 243.826 222.600 280.551 223.059 13500

298.886, 246,,720 223.371 292,687 223,81q 14000

311.616 245.610 224.119 305.418 224.547 14500

325,559 246,555 224,851 319,362 225,266, 15000

340.376, 247.527 225,567 336,.177 Z25.967 15500

356.178 26,8,530 226.269 36,9.980 226.656 16000

373,082 249,570 226,959 366,885 227,335 16500

591.193 250,651 227.640 38_.996 228,006, 17000

410.60i 251,776 228.313 40_.404 228,667 17500

431.583 252.96,7 228.981 6,25.185 Z29,326 18000

453.593 256,.164 229.66,5 447,396 229.980 18500

475.662 255,330 230,295 6,69.465 230,621 19000

495.349 256,317 230,914 489.151 231.232 19500

515,256, 257.286 231.523 509.057 231,833 20000

53

NASA/TP-3287/REV 1
TABLE 11127.- SELECTED THERMODYNAMIC FUNCTIONS FOR U(cr,I)

T C° H°("F)'H°(0) son -{Q°(T)'H°(0)}_ H°(T) -G°('T)K T

K J/m_kK _/m_ _moI-K J/moI-K kJ/mol J/moI-K K

0 0.000 0.000 0.000 0.000 -4.632 INFINITE 0

100 12.970 0.494 7,330 2,390 -4.138 48,710 100

200 21.550 2,338 19,852 8.162 -2.294 31.322 200

250 25.392 3.470 24.872 10.992 -1.162 29.520 250

298.15 2_.860 4.632 29.120 13.584 0.000 29.120 298.15

300 24.881 4.678 29.274 13.680 0.046 29.120 300

350 25,921 5.945 33.177 16.192 1.313 29.426 350

400 27.584 7.280 36.742 18.541 2.648 30.121 400

cr 453.69 29.769 8,819 40.3_7 Z0.910 _.187 31.119 453.69

453.69 30.375 11.819 46.960 20.910 7.187 31.119 453.69

500 30.071 13.218 49.897 23.461 8.586 32,725 500

600 29.584 16.199 55.354 28.335 11.567 36.055 600

700 29.248 19.140 59.867 32.525 14.508 39.142 700

800 29.017 22.052 63.757 36.191 17.420 41.981 800

900 28.870 24.946 67.165 39.447 20.314 44.594 900

1000 28.795 27.829 70.202 42.374 23.197 47.006 1000

1100 28.785 30.707 72.9_6 45.030 26.075 49.2_1 1100

1200 28.836 53.588 75.452 47.462 28.956 51.322 1200

1300 28,945 36.476 77.764 _9.706 31.84_ 53.269 1300

1400 29.111 39.379 79.915 51.787 34.7_7 55.096 1400

1500 29,334 42.300 81.931 53.730 37.668 56.818 1500

1600 29.631 45.247 83.832 55,553 40.615 58.448 1600

1700 29.942 48.224 85.637 57.270 43,592 59.995 1700

1800 30.328 51.237 87.359 58.89_ 46,605 61,467 1800

1900 30.767 54.292 89,011 60.436 49.660 62.874 1900

2000 31.260 57.395 90.601 61.905 52.761 64.221 2000

2100 31.806 60.5_6 92.139 63,308 55.914 65.514 2[00

2200 32.406 63.756 93.633 64.653 59.124 66.758 2200

2300 33.058 67.028 95.087 65.944 62.396 67.958 2300

2400 33.764 70.369 96.509 67.188 65.737 69.118 2400

2500 34.522 73.783 97.902 68.389 69.151 70.242 2500

2600 35.334 77.275 99.272 69.551 72.643 71.332 2600

2700 36.198 80.851 100.622 70.677 76.219 72.392 2700

2800 37.115 84.517 101.95_ 71.770 79.885 73.424 2800

2900 38.084 88.276 103.27_ 72.83_ 83.644 74.431 2900

3000 39.107 92.135 104.582 73.870 87.503 75._14 3000

54 NASA/TP-3287/REV l
TABLE 111.28. - SELECTED THERMODYNAMIC FUNCTIONS FOR Mg(cr,#)

T C° HO(T)._olo ) sO(T) .{GO(T).HO[0)}_ Hoco .GO(T)K T

K J/m_-K _/mol J/mobK J/m_-K _/mol J/moI-K K

0 O. 000 0.000 0.000 O. 000 -4.979 INFINITE 0

20 0.396 0.002 0.125 0.036 -4.977 248,994 20

30 1.414 0.009 0.421 0.107 -4.970 166.079 30

40 3.404 0.033 1.088 0,261 -4.946 124.740 40

50 5.710 0.079 2.092 0.522 -4.901 100.105 50

60 8.092 0.148 3.344 0.885 -4.852 85.871 60

70 10.398 0.240 4.766 1.336 -4.739 72.467 70

80 12.502 0.555 6.295 1.860 -4.624 64.099 80

90 14.291 0.489 7.875 2.440 -4.490 57.764 90

100 15.671 0.639 9.455 3.063 -4.340 52.854 100

1Z0 18.047 0,978 12.536 4.387 -4.001 45.880 120

140 19.717 1.356 15.450 5.761 -3.623 41.327 140

160 20.957 1.764 18,168 7.144 -3.215 38.264 160

180 21.907 2,193 20.693 8.511 -2.786 36.173 180

200 22.649 2.639 23,041 9.848 -2.341 34.744 200

220 23.241 3.098 25.229 11.148 -1.881 33.751 220

240 23.721 3.568 27.272 12.408 -I._12 33.154 240

260 24.124 4.046 29.187 13.626 -0.933 32.776 260

280 24,477 4.532 30.988 14.802 -0.447 32.585 280

298.15 24.775 4.979 32.535 15.835 0.000 32,535 298.15

300 24.862 5.025 32.689 15.938 0,046 32.536 300

350 25.642 6,289 56.583 18.615 1.510 32.841 550

400 26.234 7.586 40.047 21.082 2.607 33.530 400

450 26.741 8.911 43.167 23.365 3.932 34.430 450

500 27.218 10.260 46,009 25.489 5.281 35,448 500

600 28.192 13.030 51.057 29.340 8.051 37.639 600

700 29.284 15.902 55.483 32.765 10.923 39.878 700

. . 18 892 59 473 35.858 13.913 42.082 800 800 30 548 • • 44 221 900 22 018 63.154 38.689 17.039 • 3

900 32.010 _'_=_ 9 6 39 308 17.780 44.703 92

__ 923 ____z:_Ct....._L:I ......_:-_ .........:........................................

......... .-. - 31.159 73.067 59.308 26.180 44.703 923

' i_ I_._ 33.800 75,815 4Z.015 28.821 46.994 1000

1100 34,300 37.230 79.084 45.239 32.251 49,765

IZO0 34.300 40.660 82.069 48.185 35.681 52,335

1300 34.300 44.090 84;814 50.899 39.111 54.729

1400 34.300 47.520 87.356 53.413 42.541 56.970

1500 34.300 50.950 89.725 55.756 45.971 59.075

1600 34.300 54.380 91.956 57.949 _9.401 61.061

1700 34.300 57.510 94.016 60.010 52.831 62.939

1800 34.300 61.240 95.976 61,954 56.261 64.720

1900 34,300 64.670 97.831 63.794 59.691 66,414

2000 34.300 68.100 99,590 65.540 63.121 68.030

2100 34.300 71.550 101.264 67.202 66.551 69.573

2200 34,300 74.960 102.859 68.786 69.981 71.050

2300 34.300 78.390 104.384 70.301 75.411 72,466

2400 34.300 81.820 105.844 71.752 76.841 75.827

2500 34.300 85.250 107.244 73.14_ 80.271 75.136

2600 54.300 88.680 108.589 74.481 85.701 76.396

2700 34.300 92.110 109.884 75.769 87.131 77,613

2800 34.300 95.540 111.131 77.010 90.561 78.788

2900 34.300 98.970 112.335 78.207 93.991 79.924

3000 34.300 102.400 113.497 79.364 97.421 81.024

3100 34.300 105.830 114.622 80._83 100.851 82.090

3200 34.300 109.260 115.711 81.567 104.281 83.123

3300 34.300 112.690 116.767 82.618 107.711 84.127

3400 34.300 116.120 117.791 83.638 111.141 85.102

3500 34.300 119.550 118.785 84.628 114.57] 86.050

3600 54.300 122.980 119.751 85.590 118,001 86.973

3700 34.300 126.410 120.691 86.526 121.431 87.872

3800 34.300 129.840 121.606 87.437 124.861 88.747

3900 34.300 133.270 122.497 88.325 128.291 89.601

4000 34.300 136.700 123.365 89.190 131.721 90._35

4100 3_.300 140.130 124.212 90.034 135.151 91.248

4200 54.500 143.560 125.038 90.858 138.581 9Z.043

4300 34.300 146.990 125.846 91.662 142.011 92.820

4400 34.300 150.420 126.634 92.448 145.441 93.579

4500 34.300 153.850 127.405 93.216 148.871 94.323

4600 34.300 157.280 128.159 93.967 152.301 95.050

4700 34.300 160.710 128.896 94.703 155.731 95.762

4800 34.300 164.140 129.619 95.423 159.161 96.460

4900 34.300 167.570 130.326 96.128 162.591 97.144

5000 34.300 171.000 131.019 96.819 166.0ZI 97.815

11o0

1200

1300

1400

15o0

16o0

1700

180o

190o

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

NASA/TP-3287/REV 1

55
T

K

5100

5;)00

5300

5c_00

5500

5600

5700

5800

5900

6000

C o

J/m_K

3_.300

3_.300

3_.300

34.300

34.300

34.300

34.300

34.300

34.300

34.300

H°(T)-H°(0)

_lmol

174.430

177.860

181,290

18_.720

188.150

191.580

195,010

198.qq0

201.870

205.300

TABLE 111.28. - Conclude.

S°(T) -{G°('T').H°(O)}_

_mol-K _mol-K

131.698 97.496

132.36q 98,160

133.017 98.812

133.659 99.451

134.288 100.079

134.906 100.695

135.513 101.301

136.110 101.896

136.696 102._B1

137.272 103.056

H°_)

k_mol

169.451

172.881

176,311

179.741

183.171

186.601

190.031

193.461

196.B91

200.321

.G°_)_

J/moI-K

98.472

99.118

99.751

100.373

100,984

101.584

102.174

102.754

105.325

103.886

T

K

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

56 NASA/TP-3287/REV l
TABLE gl.29 - SELECTED THERMODYNAMIC FUNC'nONS FOR Mn{=.p..1.&#)

T co HO(..r}.HO(0} so(T) .{GOcF).Ho(O)}_ Ho_) _O(T)_ T

K J/m_-K kJ/m_ J/moI-K J/moI-K kJ/mol J/moI-K K

0 0.000 0.000 0.000 0.000 -,.994 INFINITE 0

100 1,.723 0.594 8.875 2.935 -4.400 52.875 100

150 20.020 I.'71 15.915 6.108 -3.523 39.402 150

200 23.054 2.556 22.133 9.353 -2.438 34.323 200

250 24.948 3.758 27.493 12.461 -1.236 32.,37 250

298.15 26.299 4.994 32.010 15.260 0.000 32.010 298.15

300 26.347 5.043 32.173 15.363 0.0,9 32.010 300

350 27.516 6.390 36.325 18.068 1.396 32.336 350

400 28.527 7.792 40.066 20.586 2.798 33.071 400

500 30.292 10.766 46.696 25.164 5.772 35.152 500

550 31.108 12 301 49.622 27.257 7.307 36.337 550 " 8.882 37.559 600

. 99 13 876 52 362 29 235 600 31 8 --" ..... "'_= 32'905 12 149 ,0.039 700

426 1/ xq3 _- J_J 700 33. • " " 15 566 42.498 800 800 36.915 20.560 _?_ _ ,9131 _, 896 900

o 2:088 46.761......

............... T-;; - 29.308 71.572 41.665 2,31, 46.761 980

' 30061 72.332 ,2271 25.067 ,7265 1000

8 116 33 852 75 965 ,5 170 28.858 49.710 1100

1100 3 • --" ..... "pTo _7"876 32 690 52 037 1200

1200 38.535 5_._ _._ _0'41_ 36'565 54 253 1300

13oo _._ _X_X _'_;; _1"8_ 38"948 55 555 1361

1361 _.ZU_ ,o.v_ _ ...... " .........................

;- ;3_;-- - A o_5 46.064 85.731 _8;_ ---J_J_ 55.555 1361 43 _30 47 751 86 953 52 845 _2757 56.412 1400 1400 1,12 4351, ,8273 87_26_....... 53"136 :........................................ 43.279 56.673 1412

................ 22; ...... 50-;5; ...... ;;-;;5 53 136 65.158 56.673 1412

1,12 45. --" ..... "_1_ 55"302 49 173 58.631 1500

1500 65.982 _._o/ vz ......

6 1519 46.108 55.0,2 91.993 55.757 50.048 59.045 1519

............................................................................................

! 1519 _6.024 67.100 99.931 55.757 62.106 59.045 1519

1600 _6.02, 70.828 102.322 58.055 65.834 61.176 1600

1700 46.02, 75.430 105.112 60.742 70.436 63.679 1700

1800

1900

2000

2100

2200

2300

2400

250C

2600

2700

_8C0

29C3

3000

33o_

320C

33_3

3_0_

350o

3600

37o0

3803

3900

4000

4100

4200

_300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5,00

5500

5600

5700

5800

5900

6000

_6.024

_6.024

46.024

_6.024

&6.024

_6.024

_6.024

_602_

we.02_

_,0_

_b 024

_6 OZq

_ 024

_.82&

_ 024

_ 02_

_o 02_

_o.024

_6.024

_o.024

_6.024

_6.026

66.024

66.024

46.026

46.02G

46.024

46.02'

46.024

_6.024

46.024

46.024

46.024

46.024

,6.024

46.02,

46.024

46.024

80.033 107.743 63.280 75.039 66.055

84.635 110.231 65.687 79.641 68.315

89.238 112.592 67.973 84.244 70.470

93.840 114.838 70.152 88.846 72.530

98.4,2 116.979 72.232 93.448 74.502

103.0,5 119.024 74.222 98.051 76.39,

107.647 120.983 76.130 102.653 78.211

112.250 122.862 77.962 107.256 79.960

116.852 124.667 79.724 111.858 81.6,5

121.454 126.404 81.421 116.460 83.271

126.057 128.078 83.058 121.063 84.841

130.659 129.693 84.638 125.665 86.360

135.262 131.253 86.166 130.268 87.831

139.864 132.762 87.645 134.870 89.256

i_4.,66 134.224 89.078 139.472 90.638

149.069 135.640 90.467 14,.075 91.981

153.671 137.016 91.816 148.677 93.285

158.274 138.348 93.127 153.280 94.554

162.876 139.644 94.401 157.882 95.788

167.478 140.905 95.641 162.48, 96.991

172.081 142.133 96.848 167.087 98.163

176.683 1,3.328 98.025 171.689 99.305

181.286 144.493 99.172 176.292 100.421

185.888 145.630 100.291 180.89_ 101.509

190.490 146.739 101.384 185.496 102.573

195.093 147.822 102.452 190.099 103.613

199.695 148.880 I03.095 194.701 104.630

204.298 149.914 104.515 199.304 105.625

208.900 150.926 105.513 203.906 106.599

213.502 151.916 106.490 208.508 107.552

218.105 152.885 107.4,6 213.111 108.487

222.707 153.834 108.383 217.713 109.402

227.310 154.763 109.302 222.316 I10.300

231.912 155.675 110.202 226.918 111.181

236.514 156.569 111.085 231.520 112.0'5

241.117 157.445 111.951 236.123 112.894

245.719 158.306 112.802 240.725 113.727

250.322 159.150 113.657 245.328 114.565

254.924 159.979 116.457 2,9.930 115.3,9

259.526 160.79, 115.263 254.532 116.139

264.129 161.594 116.055 259.135 116.916

268.731 162.381 116.833 263.737 117.680

273.33_ 163.155 117.599 268.340 118.631

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3,00

3500

3600

3700

3800

3900

4000

4100

4200

4300

4,00

4500

4600

4700

,800

_900

5000

5100

5200

5300

5'00

5500

5600

5700

5800

5900

6000

57

NASA/TP-3287/REV l
T C°

K Nm_K

O 0.000

100 15,495

150 18.872

200 21.507

25O 23.074

298.15 23.935

300 23.958

550 24.580

400 25.080

45O 25.500

500 25.850

550 26,170

6O0 26.460

700 26.980

800 27.440

900 27.890

1000 28.570

1100 28.900

1200 29.490

1300 30.140

1400 50.860

1500 31.650

1600 32.500

1700 33.420

1800 34.420

1900 35.490

2000 36.650

2100 37.900

2200 59.240

2500 40.670

2400 42,210

2500 43.890

2600 45.880

2700 48.370

TABLE 111.30- SELECTED THERMODYNAMIC FUNCTIONS FOR Mo(cr,I)

H°('r)-H°_) S°F) -{G°0-)-H°(0)}K H°(T) .G°(I")K

kJ/m_ J/m_-K J/mO_K k_rnol J/n',,o_K

0.000 0,000 0.000 -4.585 INFINITE

0.491 7.026 2.116 -4,094 47.966

1.517 13.6_8 4.868 -3.268 35.435

2.334 19.478 7.808 -2.251 . 50,753

3.452 24.462 10.654 -1.133 28.994

4.585 28.605 13,227 0.000 28.605

4.629 28.753 13.323 0.044 28.606

5.843 32.494 15,800 1.258 28.900

7.085 35.810 18.098 2.500 29.560

8.350 58.789 20.235 5.765 30.42Z

9.634 qi.494 22.226 5.049 31.396

10.934 45.973 24.093 6.349 32.429

12.250 46.265 25.846 7.665 53._88

14.923 50.382 29.063 10.338 35.613

17.644 54.015 31.960 13.059 57.691

20.410 57.272 34.594 15.825 39,689

25.223 60.255 57.012 18.658 41.597

26.086 62.965 39.248 21.501 43.417

29.004 65.502 41.352 24.419 45.153

31.985 67.888 45.284 27.400 _6.811

35.035 70.148 45.125 50.450 48.398

38.160 72.504 46.864 35.575 49.921

41.567 74.573 48.519 36.782 51.384

44.663 76.371 50.099 40.078 52,796

48.054 78.309 51.612 45.469 54.160

51.549 80.198 53.067 46.964 55.480

55.155 82.048 54.470 50.570 56.765

58.882 83.866 55.827 54.297 58.010

62.737 85.659 57.142 58.152 59.226

66.752 87.435 58.421 62.1_7 60.415

70.875 89.198 59.667 66.290 61,577

75.179 90.954 60.882 70.594 62.716

79.664 92.713 62.073 75.079 65.836

84.371 94.490 63.241 79.786 64.940

T

K

0

100

150

200

250

298

30o

350

400

450

5oo

550

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

.15

2800 51.570 89.362 96.504 64.389 84.777 66.026 2800

cr 2896 54.835 94.470 98.098 65.477 89.885 67.060 2896

......i;7;;; ..... .....;;;7;;; ......;;T;;;.....;;;:;;; ...... ......;;;;---

2900 37.656 130.603 110.574 65.559 126.018 67,120 2900

3000 37.656 134,369 111.851 67. 061 129. 784 68. 590 3000

3100 37.656 138.134 115.086 68.526 135.549 70.005 3100

3200 37.656 141.900 114.281 69.938 137.315 71.370 5200

3300 37.656 145.665 115.440 71.299 141.080 72.688 3300

3400 57.656 149.451 116.564 72.614 144.846 73.962 3400

3500 37.656 153.197 117.656 73.885 148.612 75.195 3500

3600 37.656 156.962 118.716 75.116 152.377 76.390 3600

3700 37.656 160.728 119.748 76.308 156.143 77.547 3700

3800 37.656 164.493 120.752 77.465 159.908 78.671 3800

3900 37.656 168,259 121.731 78.587 163.674 79.763 3900

4000 37.656 172.025 122.684 79.678 167.440 80.824 4000

4100 37.656 175.790 123.614 80.738 171.205 81.856 4100

_200 37.656 179.556 124,521 81.770 174.971 82.861 4200

4500 37.656 183.321 125.407 82.774 178,736 83.841 4300

4400 37.656 187.087 126.273 83.753 182.502 84,795 4400

4500 37.656 190.853 127.119 84.708 186.268 85.726 4500

4600 37.656 194.618 127.947 85.639 190.033 86.635 4600

4700 37.656 198.584 128.757 86,547 193.799 87.525 4700

4800 37.656 202.149 129.549 87.455 197.564 88.390 4800

4900 37.656 205.915 130.326 88.302 201.330 89.238 4900

5000 37.656 209.681 131.087 89.151 205.096 90.068 5000

5100 37.656 213.446 131.832 89,980 208.861 90.879 5100

5200 37.656 217.212 132.564 90.792 212.627 91.674 5200

5300 37.656 220.977 133.281 91.587 216.392 92.452 5300

5400 37.656 224.743 133.985 92.366 220.158 93.215 5400

5500 37,656 228.509 134.676 93.129 223.924 93.962 5500

5600 37.656 232.274 135.354 93.877 227.689 94.695 5600

5700 37.656 236.040 136.021 94.610 231.455 95.415 5700

5800 37.656 239.805 136.676 95.330 235.220 96.120 5800

5900 37.656 243.571 137.319 96.036 238.986 96.813 5900

6000 57.656 247.337 137.952 96.729 242.752 97.494 6000

58 NASA/TP-3287/REV 1
TABLE 111.31- SELECTEDTHERMODYNAMIC FUNCTIONS FOR N2

T C° H°(T)'HO{o) s°(r) "{G°(T)'H°(O)}_ H°(T) "GO_O_

K Jlm_.K kJ/mol J/m_-K J/moI-K kJ/mol J/moI-K

0 0.000 0.000 0.000 0.000 -8.670 INFINITE

100 29.104 2.902 159.811 130.791 -5.768 217.492

150 29.105 4.357 171.612 142.564 -4.313 200.565

200 29.107 5.813 179.986 150.920 -2.857 194.271

250 29.111 7.268 186.482 157.409 -1.402 192.090

298.15 29.124 8.670 191.610 162.530 0.000 191.610

300 29.125 8.724 191.790 162.709 0.054 191.610

350 29.165 10.181 196.282 167.195 1.511 191.965

400 29.249 11.641 200.182 171.079 2.971 192.754

500 29.580 14.581 206.740 177.578 5.911 194.918

600 30.109 17.564 212.177 182.905 8.894 197.553

700 30.754 20.607 216.866 187.427 11.937 199.813

800 31.433 23.716 221.017 191.372 15,046 202.209

900 32,090 26.892 224.758 194.878 18.222 204.511

I000 32.696 30.132 228.171 198.039 21.462 206.709

II00 33.241 33.450 231.313 200.922 24.760 208,804

1200 33.723 36.778 234.227 203.579 28.108 210.804

1300 34.147 40.172 236.945 206.041 31,502 212.711

i400 54.517 43.607 239.487 208.340 34,936 214.533

1500 34.842 47.075 241,880 210,497 38.404 216.277

1600 35.127 50.574 244.158 212.530 41.904 217.949

1700 35.377 54.099 246.275 214.453 45,429 219.553

1800 35.598 57,648 248.304 216,278 48.978 221.095

1900 35.795 61.218 250.234 218.015 52.548 222.578

2000 35.969 64.807 252.074 219.671 56.137 224,006

2100 36.126 68.412 253.833 221.256 59.742 225.385

2200 56.267 72.031 255.518 222.776 65.361 226.717

2300 36.394 75.664 257.133 224.235 66.994 228.005

2400 36.509 79.310 258.684 225.638 70.640 229.250

2500 36.616 82.966 260.177 226.990 74.296 250.458

2600 36.710 86.632 261.615 228.295 77.962 231.629

2700 36.799 90.308 263.002 229.554 81.638 232.765

2800 36.881 93.992 264.342 230.773 85.322 233.869

2900 36.956 97.684 265.637 231.952 89.014 234.942

3000 37.027 101.383 266.891 233.096 92.713 235.986

3100 37,093 105.089 268.107 234.207 96.419 237.004

3200 37.155 108.801 269.285 235.284 100.131 237.994

3300 37.213 112.520 270.429 236.352 103.850 258.959

3400 37.268 116.244 271.541 237.351 107.574 239.901

3500 37,320 119.973 272.622 238.344 111.303 240.821

3600 37.369 123.708 273.674 239,310 115.038 241.719

3700 37.417 127.448 274.699 240.255 118.777 242.597

3800 37.462 131.192 275.697 241.173 122.521 243.454

3900 37.505 134.940 276.671 242.071 126.270 244.294

4000 37.547 138.693 277.621 242.948 130.023 245.115

4100 37.588 142.450 278.549 243.805 133.780 245.920

4200 37.628 146,211 279.455 244.643 137.541 246.707

4300 37.667 149.975 280.341 245.463 141.305 247.479

4400 37.705 153.744 281.207 246.265 145.074 248.236

4500 37.743 157.516 282.055 247.051 148.846 248.978

4600 37,780 161.292 282.885 247.821 152.622 249.706

4700 37.817 165.072 283.698 248.576 156,402 250.421

4800 57.855 168.856 284.494 249.316 160.186 251.122

4900 37.893 172.643 285,275 250.042 163.973 251.811

5000 37.931 176.434 286.041 250.754 167.764 252.488

5100 57.971 180.229 286.793 251.454 171.559 253.154

5200 38.011 184.029 287.530 252.140 175.359 253.807

5300 38.053 187.832 288.255 252.815 179.162 254.451

5400 38.096 191.659 288.966 253.477 182.969 255.083

5500 38.141 195,451 289.666 254.129 186.781 255.706

5600 38.188 199,267 290.354 254.770 190.597 256.319

5700 38.258 203.089 291.030 255.400 194.419 256.921

5800 38.291 206.915 291.695 256.020 198.245 257.515

5900 38.346 210.748 292.350 256.630 202.077 258.100

6000 38.405 214.585 292.995 257.231 205.914 258.676

6200 38.534 , 222.279 294.256 258.405 213.609 259.803

6400 38.680 230.000 295.482 259.545 221.530 260.899

6600 38.846 237.752 296.675 260.652 229.082 261.966

6800 39.035 245.540 297.837 261.728 236.870 263.003

7000 39.249 253.368 298.972 262.777 244.698 264.015

7200 39.491 261.242 300.081 265.797 252.572 265.002

7400 39.763 269.167 301.166 264.792 260.497 265.964

7600 40.068 277.149 302.231 265.764 268.479 266+905

7800 40.407 285.196 305.276 266.712 276.526 267.824

8000 40.784 293.316 304.304 267.640 284.645 268.723

K

0

100

150

2OO

250

298.15

300

350

400

5O0

600

7OO

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5500

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

59

NASA/TP-3287/REV l
T

K

8200

8400

8600

8800

9000

9200

9qO0

9600

9800

10000

10500

II000

11500

12000

12500

15000

15500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

C°

d/m_-K

61.198

61.653

62.167

42.682

63.258

_5.875

66.532

65.228

65.960

66.728

68.781

50.985

55.274

55.575

57.811

59.908

61.796

63.621

66.761

65.729

66.575

66.685

66.676

66.369

65.803

65.011

64.055

62.904

61.660

60.552

H°Cr).H°(0)

_/moi

501.515

509.797

318.176

326.658

355.252

365.966

552.804

561.779

570.897

580.166

q06.035

628.971

655.035

682.267

510.598

560.036

570.671

601.786

633.861

666.672

699.512

732.791

766.163

799.616

852.668

865.180

897._68

929.188

960.333

990.856

TABLE 11.31 - Concluded

s°(r)

J/mohK

305.316

306.316

307.300

308.275

309.260

510.198

311.148

512.093

513.035

313.969

316.298

318.618

520,956

323.250

325.565

527.873

350.170

352.468

334.697

336.909

339.077

341.190

563.265

365,229

567.165

368.988

350.756

552.469

354,067

355.611

.(O°0")-H°(0)}_

J/m_.K

268.566

269.636

270.303

271.155

271.990

272.811

273.616

274.608

275.187

275.953

277.819

279.621

281.366

283.065

286.718

286.332

287.913

289.666

290.986

292.678

293,967

295.390

296.810

298.206

299.575

300.922

302.265

305.566

306.819

506.069

H°_)

k_mol

292.863

301.127

309.506

317.988

326.582

355.296

346.154

555.109

562,227

371.695

395.565

620.301

666.363

673.577

501.928

531.366

561.801

593.116

625.171

657.802

690.862

724.121

757.673

790.766

823.798

856.510

888.778

920.518

951.662

982.166

-O°CT')F

d/mol-K

269.606

270.666

271.311

272.160

272.953

275.753

274.538

275.311

276.071

276.820

278.666

280.609

282.120

283.786

285.611

286.999

288.556

290.085

291.582

295.056

296.506

295.932

297.335

298.716

300.070

501.606

302.716

306.000

305.263

306.505

T

K

8200

8600

8600

8800

9000

9200

9400

9600

9800

I0000

10500

ii000

11500

12000

12500

13000

13500

16000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

60 NASA/TP-3287/REV 1
TABLE 11132.• SELECTED "THERMODYNAMICFUNCTIONS FOR Na(cr,l_

T cO H°(T)'H°(0) s°(T) "_'G°(T)'H°(0)}/T H°(T) "G°(T)/T

K J/m_l-K kJ/tool J/moI-K J/moI-K kJ/tool J/moI-K

0 0.000 0.000 0.000 0.000 -6.460 INFINITE

100 22._60 1 .:347 23.656 10.186 -5.113 74.786

200 26.000 3.802 40.539 21.5?-9 -2.658 53.829

T

K

0

100

200

298.15 2g,230 6.460 51.300 29,633 0,000 51.300 298.15 0,052 51.302 300

300 28 261 6 .5 12 51 .475 29 "768 51 946 371.01

._, nl XI dog 8 614 57.752 34.534 2.154 ___ ................

__....._.....:_ ........... :................................... _.........

. 31. 99 11.212 64.75_ 34.534

400 31.532 12.130 67.137 36.812 . "

500 30.659 15.239 74.077 43.599 8.779 56.519 500

600 29.920 18,267 79.599 49.154 11.807 59.921 600

700 29,353 21.229 84.167 53.840 14.769 63.068 700

800 28.973 24.1_4 88.059 57.879 17.684 65,954 800

900 28.787 27.030 91.459 61,426 20.570 68.603 900

1000 28.799 29.908 94.491 6_.583 23.4_8 71.043 1000

1100 29.012 32.796 97.244 67.429 26.336 73,302 1100

1200 29.427 55.717 99.785 70.021 29.257 75._04 1200

1300 30.045 38.689 102.163 72.402 32.229 77.371 1300

1400 30.866 41.733 104.419 74.610 35.273 79.224 1400

1500 31.891 44.869 106.582 76.669 38.409 80.976 1500

1600 33,120 48.118 108.678 78.604 41.658 82.642 1600

1700 34.553 51.499 110.728 80.434 45.039 8_.234 1700

1800 36.190 55.035 112.748 82.173 48.575 85.762 1800

1900 38.032 58.744 114.754 83.836 52.284 87.236 1900

2000 40.078 62.648 116.755 85.431 56.188 88.661 2000

2100 42.328 66.767 118.765 86.971 60.307 90.047 2100

2200 44.784 71.121 120.790 88.462 64.661 91.399 2200

2300 47.4_4 75,730 122.838 89.912 69.270 92.721 2300

61

NASA/TP-3287/REV l
T C°

K _n_-K

0 o.o0o

100 17.439

150 21.351

200 23.091

250 24.154

298.15 24.694

300 24.711

350 25.088

400 25.393

450 25,653

500 25.899

550 26.126

600 26.347

700 26.769

800 27.183

900 27.593

I000 27,999

1100 28.405

1200 28.798

1300 29,179

1400 29.589

1500 30.062

1600 30,606

1700 31.221

1800 31,903

1900 32.639

2000 33,430

2100 34.275

2200 35.187

2300 36.192

2400 37.317

2500 38.635

2600 40.233

TABLE IN,33.. SELECTED THERMODYNAMIc FUNCTIONS FOR Nb(cr,t}

H°(T)'H°(0) s°(r) "{G°F0"H°_)}_ H°(T) -G°(T)K T

Ulrnol J/m_K J/moI-K kJ/mol J/m_-K K

0.000 0.000 0.000 -5.241 INFINITE 0

0.781 12.558 4.748 -4.460 57.158 I00

1.764 20.469 8.709 -3.477 43.649 150

2.880 26.878 IZ,q78 -2.361 38.683 200

4.064 32,159 15,903 -i.177 36,867 250

5.241 36.464 18.886 0.000 36.464 298

5.287 86.616 18.993 0.046 36.463 300

6.532 40.455 21.792 1.291 36.766 350

7.794 43.826 24,341 2.553 37.443 400

9.071 46.832 26.674 3.830 38.321 450

10.359 49.548 28.850 5.118 39.312 500

11.660 51.027 30.827 6.419 40.356 550

12.972 54.309 32.689 7.731 41.424 600

15.628 58.403 36,077 10.387 43.564 700

18.325 62.004 39.098 13.084 45.649 800

21.064 65.230 41.826 15,823 47.649 900

23,844 68.158 44,314 18.603 49.555 1000

26.664 70.846 46.606 21.423 51.371 II00

29.525 73.334 48.730 24,284 53.097 1200

32.423 75.654 50.713 27.182 54.745 1300

35.361 77.831 52.573 30.120 56.317 1400

38.343 79,888 54.326 33.102 57.820 1500

41.376 81.846 55.986 36.135 59.262 1600

44.467 83.719 57.562 39.226 60,645 1700

47.622 85.523 59,066 42,381 61.978 1800

50.849 87.267 60.504 45.608 63.263 1900

54.152 88.961 61.885 48.911 64.505 2000

57.537 90,612 63.213 52.296 65.709 2100

61.009 92,228 64.497 55.768 66.879 2200

64.577 93.815 65.736 59.336 68.015 2300

68.251 95.377 66.939 63.010 69.123 2400

72.046 96.926 68.108 66.805 70.204 2500

75.986 98.471 69.246 70.745 71.261 2600

.15

2700 42.283 80.109 100.027 70.357 74.868 72.298 2700

cr 2750 43.423 82.252 100.813 70.903 77.011 72.809 2750

2800 33.472 110.828 111.199 71.617 105.587 73.489 2800 2900 33.472

3000 33.472

3100 33.472

3200 33.472

3300 33.472

3400 33,472

3500 33.472

3600 33.472

3700 33.472

3800 33.472

3900 33.472

4000 33.472

4100 33,472

4200 33.472

4300 33.472

4_00 33.472

4500 33.472

4600 33.472

4700 33.472

4800 33.472

4900 33.472

5000 33.472

5100 33.472

5200 33,472

5300 33.472

5400 33.472

5500 33.472

5600 33.472

5700 33.472

5800 33.472

5900 33.472

6000 33.472

114.176 112.374 73.003 108.935 74.810 2900

117.523 113.508 74.334 112.282 76.081 3000

120.870 114.606 75.616 115.629 77.306 3100

124.217 115.669 76.851 118.976 78.488 3200

127.564 116.699 78.043 122.323 79.631 3300

130.912 117.698 79.194 125.671 80.736 3400

134,259 118.668 80.308 129.018 81.806 3500

137.606 119.611 81.387 132.365 82.843 3600

140.953 120.528 82.433 135.712 83.849 3700

144.300 121.421 83.447 139.059 84.826 3800

147.648 122.290 84.432 142.407 85.776 3900

250.995 123,138 85.389 145.754 86.699 4000

154.342 123.964 86.320 149.101 87.598 4100

157.689 124.771 B7.226 152.448 88.474 4200

161.036 125.558 88.108 155.795 89.327 4300

164,384 126.328 88.968 159,143 90.159 4400

167.731 127.080 89,807 162.490 90.971 4500

171.078 127.816 90.625 165.837 91.764 4600

174.425 128.536 91.424 169.184 92.539 4700

177.772 129.240 92.204 172.531 93.296 4800

181.120 129.930 92.967 175.879 94.037 4900

184.467 130.607 93.713 179.226 94,762 5000

187.814 131.270 94.443 182.573 95.471 5100

191.161 131.920 95.158 185.920 96.166 5200

194.508 132.557 95.857 189.267 96.846 5300

197.856 133.183 96.5_3 192.615 97.513 5400

201.205 133.797 97.215 195.962 98.167 5500

204.550 13q.q00 97.873 199.309 98.809 5600

207.897 134.992 98.519 202.656 99.439 5700

211.244 135.575 99.153 206.003 100.057 5800

214.592 136.147 99.775 209.351 100.664 5900

217.939 136.709 100,386 212,698 101.260 6000

62 NASA/TP-3287/REV 1
TABLEIK.34.- SELECTED THERMODYNAMIC FUNCTIONS FOR Ne

T cO H°_)'H°(O) SO(7) "{G°(T)'H°(O)}K H°(T)

K JJm_-K kJ/mol J/rno_K J/mo4-K kJ/mo_

0 0.000 0.000 0.000 0.000 -6.197

100 20.786 2.079 123.622 102.836 -4.119

200 20.786 4.157 158.030 117.244 -2.040

298.15 20.786 6.197 146.330 125.543 0.000

500 20.786 6,236 146.458 125.672 0.038

400 20.786 8.315 152.438 131.652 2.I17

500 20.786 10.393 157.076 136.290 4.196

600 20.786 12.472 160.866 140.080 6.274

700 20.786 14.550 164.070 143.284 8.353

800 20.786 16.629 166.846 146,060 10.432

900 20.786 18.708 169.294 148.508 12.510

1000 20.786 20.786 171.484 150.698 14.589

II00 20.786 22.865 173.466 152.679 16.667

1200 20.786 24.944 175.274 154.488 18.746

1300 20.786 27.022 176.938 156.152 20.825

1400 20.786 29.101 178.478 157,692 22.903

1500 20.786 31.179 179.912 159.126 24.982

1600 20.786 53.258 181.254 160.468 27.061

1700 20.786 35.337 182.514 161.728 29,139

1800 20.786 37.415 185.702 162.916 31.218

1900 20.786 39.494 184.826 164.040 35.296

2000 20.786 41.573 185.892 165.106 35.575

2100 20.786 43.651 186.906 166.120 37.454

2200 20.786 45.730 187.875 167.087 39.532

2500 20.786 47.808 188.797 168.011 41,611

2400 20.786 49.887 189.682 168.896 43.690

2500 20.786 51.966 190.531 169.744 45.768

2600 20.786 54.044 191.346 170.560 47.847

2700 20.786 56.123 192.130 171.344 49.926

2800 20.786 58.202 192.886 172.100 52.004

2900 20.786 60.280 193.616 172.829 54.083

3000 20.786 62.359 194.520 175.534 56.161

3100 20.786 64.437 195.002 174.216 58.240

3200 20.786 66.516 195,662 174.876 60.319

3300 20.786 68.595 196.302 175,515 62.397

3400 20.786 70.675 196.922 176.136 64,476

5500 20.786 72,752 197,525 176.738 66.555

3600 20.786 74.831 198,110 177.524 68.633

3700 20.786 76.909 198.680 177.893 70.712

3800 20.786 78.988 199.234 178.448 72.790

3900 20.786 81.066 199.774 178.988 74.869

4000 20.786 83.145 200.500 179.514 76.948

4100 20,786 85.224 200.814 180.027 79.026

4200 20,786 87.502 201.314 180.528 81.105

_300 20.786 89.581 201.804 181.017 83,184

4400 20.786 91.460 202.281 181.495 85.262

4500 20.786 93.558 202.749 181.962 87.341

4600 20.786 95.617 203.205 182,419 89.419

4700 20.786 97.695 203.652 182.866 91.498

4800 20.786 99.774 204.090 185.504 93.577

4900 20.786 101.855 204.519 183.752 95.655

5000 20.786 103.931 204.939 184.152 97.734

5100 20.786 106.010 205.350 184.564 99.813

5200 20.786 108.089 205.754 184.968 101.891

5300 20.786 110.167 206.150 185.564 103.970

5400 20.786 112.246 206.538 185.752 106.048

5500 20.786 114.325 206.920 186.1S3 108.127

5600 20,786 116.403 207.294 186.508 110.206

5700 20.786 118.482 207.662 186.876 112.284

5800 20.786 120.560 208.024 187.237 114.363

5900 20.786 122.639 208.379 187.593 116.442

6000 20.786 124.718 208.728 187.942 118.520

6200 20.786 128.875 209.410 180.624 122.677

6400 20.786 133.032 210.070 189.284 126.835

6600 20.786 137.189 210.710 189.923 130.992

6800 20.786 141.547 211.330 190.544 135.149

7000 20.786 145.504 211.933 191.146 139.306

7200 20.786 149.661 212.518 191.732 143.464

7400 20.786 155.818 215.088 192.301 147.621

7600 20.786 157.976 213.642 192.856 151.778

7800 20.786 162.133 214.182 193.396 155.936

8000 20.786 166.290 214.708 195.922 160.095

.G°CDK

J/mokK

INFINITE

164.810

i_8.231

146.330

-146.330

147.145

148.685

150.409

152.138

153.807

155.394

156.896

158.313

159.652

160.919

162.119

163.258

164.341

165,373

166.359

167.302

168.205

169.071

169.904

170,706

171.478

172.223

172,943

173.639

174.318

17_.967

175.600

176.215

176.812

177.393

177.959

178.509

179.045

179.568

180.079

180.577

181.063

181.539

182.004

182.459

182.904

183.359

183.766

184.185

184.595

184.997

185.592

185.779

186.159

186,535

186.900

187.260

187.615

187.963

188.306

188.645

188.975

189.623

190.252

190.862

191.455

192.032

192.593

193.139

193.671

194.190

194.697

T

K

0

100

200

298.15

300

400

500

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

5200

3500

3400

3500

3600

3700

3800

3900

4000

4100

_200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV 1

63
TABLE III34, - ConckJOed

T C° H°(T).H°(0) sO(T) .{GO(T).Ho(O)}_

K J/m_-K kJ/mol J/mo6K J/moI-K

8200 20.786 170.447 215.221 ]9q.435

8400 20.786 174.605 215.722 19_.936

8600 20,786 178.762 216.211 195,425

8800 20.786 182.919 216.689 195.905

9000 20.786 187.076 217.156 196.370

9200 20.786 191.234 217.613 196.827

9400 20.786 195.391 218.060 197,274

9600 20.786 199.548 218._98 197.712

9800 20.786 203.706 218.927 198.1_0

10000 20.787 207.863 219.347 198.560

10500 20.787 218.256 220.361 199.574

ii000 20,788 228.650 221.328 200.541

11500 20.789 239.04q 222.252 201,q65

12000 20.792 2q9.439 225.137 202.350

12500 20.796 259.836 223.985 203.199

13000 20,804 270.235 226.801 204.014

13500 20.815 280.640 225.587 204.798

1_000 20.834 291.052 226.546 205.554

14500 20.861 301.475 227.075 206.284

15000 20.897 511.912 227.785 206.989

15500 20.950 322.372 228.469 207.671

16000 21.007 332.847 229.136 208.351

16500 21.095 3_5.568 229.782 208.971

17000 21.175 355.901 250.610 209.593

17500 21.510 364.521 231.026 210.196

18000 21.343 375.027 231.617 2]0.782

18500 21.506 385,738 232.206 211.353

19000 21.703 396.539 232.780 211.910

19500 21.937 607.667 253.3_7 212.652

20000 22,216 _18.683 283.906 212.982

H°CD

kJ/mol

166.250

168.607

172.565

176.722

180.879

185.036

189.194

193.351

197.508

201.665

212.059

222.652

252.846

263,242

253.688

266.038

276.468

284.854

295.278

305.716

316.175

326.650

537,171

867.705

358.323

368.830

379.560

390.341

601.250

_12.286

-G°CDK

J/mohK

195.191

195,674

196.146

196.607

197.059

197.501

197.933

198.357

198.773

199.180

200,165

201.105

202,006

202.867

203.694

206.491

205,258

205.997

206.711

207.602

208.071

208.718

209.567

209.957

210.550

211.127

211.688

212.236

212.770

218.291

T

K

8200

8400

8600

8800

9000

9200

9600

9600

9800

i0000

10500

llO00

11500

12000

12500

13000

15500

l_OOD

1_500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

64 NASA/TP-3287/REV 1
TABLE 111.35.- SELECTED THERMODYNAMIC FUNCTIONS FOR Ni(cr,#)

T C o` HO0.)_o(0) so03 .{GOm.Ho(O)}_ Ho_) .Go_)_ T

K J/n_l-K kJ/mo_ J/mot-K J/moI-K kJ/mol J/moI-K K

0 0.000 0.000 0,000 0.000 -4.786 INFINITE 0

100 13.631 0.508 7,454 2,374 -4,278 50.234 100

150 19.305 1.346 14.170 5.197 -3.440 37.103 150

200 22.468 2.397 20.200 8.215 -2.389 32.145 200

250 24.397 3.571 25.432 11.148 -i,215 30,292 250

298.15 25.987 4.786 29.870 13.818 0.000 29.870 298.15

300 26.024 4.834 30.031 13.918 0.048 29.871 300

350 27.294 6.167 34.139 16.519 1.381 30.193 350

400 28.493 7.562 37,863 18,958 2.776 30.923 400

450 29.623 9.014 41.281 21.250 4.228 31.885 450

500 31.045 10,529 44.473 23.415 5.743 32.987 500

550 32.761 12.123 47.510 25.468 7.337 3_.170 550

a 600 34.853 13.808 50.440 27,427 9.022 35.403 600

cr 651 39.832 14,930 52.263 28.602 10.144 36.187 631

cr 6 " 17 130 55,575 31.104 12.344 37.941 700 700 30.794

%00 31.003 20.217 59.697 3_._26 15.931 40.408 800

900 31.589 23.3_6 63.382 37,442 18.560 42.760 900

i000 32,217 26.536 66.7_2 40.206 21,750 44,992 1000

ii00 32.928 29.793 69.845 42.760 25.007 47.111 I100

1200 33.681 33.122 72.742 45,140 28.536 49.129 1200

1300 34.518 36.532 75.471 47.369 31.746 51.051 1300

I_00 35.397 40.027 78.061 49.470 35.241 52.889 1400

1500 36.317 43.613 80.534 51.459 38.827 54.649 1500

1600 57.279 47.292 82.908 53,350 42.506 56.342 1600

170S 38.284 51.07Z 85.199 55.157 46.286 57.972 1700

cr 17!8 38.535 52.147 85.827 55.649 ...... 47.361 ...... 58.419 ...... 1728___

1800 38.911 72.103 97,343 57.285 67.317 59.944 1800

38.911 75.994 99.446 59.449 71.208 61.968

38.911 79.886 101.442 61.500 75.100 63.893

1900

1900 2000

2000

2100 38.911 83,777 103.341 63.447 78.991 65.726 2100

2200 38.911 87.668 105.151 65.302 82.8_2 67._77 2200

2300 35.911 91.559 106.551 67.072 86.773 69.153 2300

2_00 38.911 95.450 108.537 68.766 90.664 70.760 2400

2500 38,911 99.341 110.125 70.389 94.555 72.303 2500

2600 38.911 103.232 111.651 71.947 98.446 73.787 2600

2700 38.911 107.123 113.120 73.444 102.337 75.217 2700

2800 38.911 111.014 114.535 74.887 106.228 76.596 2800

2900 38.911 114.905 115.900 76,278 110.119 77.928 2900

3000 38.911 118.797 117.219 77.621 114.011 79.216 3000

3100 38.911 122.688 I18._95 78.919 117.902 80.463 3100

3200 38.911 +126.579 119.731 80.175 121,793 81,670 3200

3300 38.911 130.470 iZ0.928 81.392 125.684 82.842 3300

3400 38.911 134.361 122.090 82.572 129.575 83,979 3400

3500 38.911 138.252 123,218 83.717 133.466 85.084 3500

3600 38.911 142.143 124.314 84.830 137.357 86.159 3600

3700 38.911 146.034 125,380 85.911 141.248 87.205 3700

3800 38.911 149.925 126.418 86.964 145.139 88,223 3800

3900 38.911 153.816 127,428 87.988 149.030 89.215 3900

_ODO 38.911 157.708 128.413 88.987 152.922 90.183 4000

_100 38.911 161.599 129.374 89.960 156.813 91.127 4100

4200 38.911 165.490 130.312 90.910 160.706 92.049 4200

4500 38.911 169.381 131.227 91.837 164.595 92.950 4300

4_00 38.911 17_.272 132.122 92.742 168.486 93.830 4400

4500 38.911 177.163 132.996 93.627 172.377 94.690 4500

4600 38.911 181.054 133.852 94.492 176.268 95.533 4600

4700 38.911 184.945 154.689 95.358 180.159 96.357 4700

4800 38.911 188.836 135.508 96.167 184.050 97.164 4800

4900 38.911 192.727 136.310 96.978 187.941 97.955 4900

5000 38.911 196,619 137.096 97.772 191.833 98.730 5000

5100 38.911 200.510 137.867 98.551 195.724 99.490 5100

5200 38.911 204.401 1_8.622 99.314 199.615 100.235 5200

5300 38.911 208.292 139.363 100.063 203.506 100.966 5300

5400 38.911 212.183 140.091 100.798 207.397 101.684 5400

5500 38.911 216.074 140.805 101.519 211.288 102.389 5500

5600 38.911 219.965 141.506 I02,226 215.179 103.081 5600

5700 38.911 223.856 I_2.195 102.922 219.070 103.761 5700

5800 38.911 227.747 142.871 103.605 222.961 104.430 5800

5900 38.911 231.638 143.536 104.276 226.852 105.087 5900

6000 38.911 235.530 144.190 104.936 230.744 105.733 6000

aMaximum lambda transition point at 631 K

NASA/TP-3287/REV 1 65
TABLE 111.36.oSELECTED THERMODYNAMIC FUNC13ONS FOR 02

TC° H°m-H°(O) sO('_ .{GO(T).HO(0)}_ Ho(T_ .Go(.r_

K J/n_-K k_rn_ _mol-K J/mo_K kJ/mol J/rnc_.K 0 0.000 0.000 0.000 0.000 -8.680 INFINITE

I_0 29.112 2.901 173.307 144.297 -5.779 231.098

150 29.120 4.357 185.111 156.066 -4.323 215.933

200 29.127 5.812 193.487 164.427 -2.868 207.827

250 29.202 7.270 199.994 170.913 -1.410 205.634

298.15 29.378 8.680 205.149 176.036 0.000 205.149

300 29.387 8.735 205.331 176.214 0.055 205.148

350 29.696 10.211 209.884 180.709 1.531 205.509

400 30.109 11.706 213.875 184.609 3.026 206.309

500 31.094 14.765 220.698 191.167 6.085 208.528

600 32.094 17.925 226.656 196.580 9.245 211.047

700 32.987 21.180 231.472 201.214 12.500 213.614

800 33.741 24.518 235.928 205.280 15.858 216.130

900 34.365 27.924 239.939 208.912 19.244 218.556

1000 34.881 31.387 243.588 212.201 22.707 220.881

I100 35.314 34.898 246.953 215.207 26.218 223.098

1200 35.683 38.448 250,022 217.982 29.768 225.215

1300 36.006 42.034 252.891 Z20.558 33.353 227.235

1400 36.297 45,649 255.570 222.964 56.968 229.164

1500 36.567 49.292 258.084 225.223 40.611 231.010

1600 36.822 52.962 260.452 227.351 44.282 232.776

1700 37.068 56.656 262.692 229.565 47.976 234.471

1800 37.308 60.375 264.817 231.276 51.695 236.098

1900 37.545 64.118 266.841 233.095 55.438 237.663

2000 37.780 67.88_ 268.772 23_.830 59.20_ 239.170

2100 38.013 71.674 270.621 236.491 62.994 240.624

2200 38.244 75.487 272.395 238.083 66.807 242.029

2300 38.47_ 79.323 274.100 239.612 70.643 243.386

2400 38.701 83.181 275.742 241.084 74.501 244.700

2500 38.925 87.063 277.527 242.502 78.385 245.974

2600 39.146 90.966 278.858 243.871 82.286 247.210

2700 39.363 94.892 280.339 245.194 86.212 248.409

2800 39.575 98.839 281.775 246.476 90.159 249.576

2900 39.783 102.807 283,167 247.717 94.127 250.710

3000 39.985 106.795 284.519 248.921 98.115 251.814

3100 40.181 110.803 285.834 250.091 102.123 252.891

3200 40.372 114.831 287.112 251.228 106.151 253.940

5300 40.558 118.878 288.357 252.334 110.198 254.964

3400 40.737 122,943 289.571 253.412 114.263 255.965

3500 40.912 127.026 290.754 254.461 118.345 256.942

3600 41.080 131.126 291.910 255.486 122._45 257.897

3700 41.244 135.242 293.038 256.486 126.562 258.832

3800 41.402 139.374 294.140 257.462 130.694 259.746

3900 41.556 145.522 295.217 258.416 134.842 260.642

4000 41.706 147.685 296.271 259.349 139.005 261.519

4100 41.851 151.863 297.303 260.263 143.183 262.580

4200 41.992 156.055 298.313 261.157 147.375 263.223

4300 42.129 160.261 299.303 262.033 151.581 264.051

4400 42.262 164.480 300.273 262.891 155.800 264.864

4500 42.393 168.713 501.22_ 263.732 160.033 265.661

4600 42.520 172.959 302.157 264.557 164.279 266.444

4700 42.644 177.217 303.073 265.367 168.537 267.214

4800 42.764 181.487 303,972 266.162 172.807 267.970

4900 _2.682 185.770 304.855 266.942 177.090 268.714

5000 42.997 190.063 305.722 267.709 181.383 269.445

5100 43.108 194.369 306.575 268.463 185.689 270.165

5200 43.216 198.685 307.413 269.204 190.005 270.873

5300 43.321 203.011 308.237 269.933 194.331 271.570

5400 43.422 207.349 309.048 270.650 198.669 272.257

5500 43.519 211.697 309.846 271.355 203.016 272.934

5600 43.612 216.053 310.631 272.050 207.372 275.600

5700 _3.701 220.419 311.403 272.733 211.739 Z74.256

5800 43.785 224.793 312.164 273.406 216.113 274.903

5900 43.864 229.175 312.913 274.070 220.495 275,541

6000 43.939 233.565 313.651 274.723 224.885 276.170

6200 44.070 242.367 315.094 276.002 233.687 277.402

6400 44.178 251.192 316.495 277.246 242.512 278.602

6600 44.259 260.035 317.856 278.457 251.355 279.772

6800 44.313 268.893 319.178 279.635 260.213 280,911

7000 44.339 277.759 320.463 280.783 269,079 282.023

7200 44.334 286.626 321.712 281.903 277.946 283.108

7400 44.299 295.491 322.926 282.995 286.810 284,168

7600 44.234 304.344 324.106 284.061 295.66_ 285.203

7800 44.139 313.182 325.254 285.102 304.502 286,215

8000 44.014 321.997 326.370 286.120 313.317 287.205

TK0

100

15o

200

25o

298.15

300

35o

40O

500

6o0

70O

800

9O0

I000

I100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

5600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

66 NASA/TP-3287/REV1
T

K

820O

860O

8600

8800

9000

9200

9600

9600

9800

i0000

10500

11o0o

I1500

12000

12500

13000

13500

16000

16500

15000

15500

16000

165O0

17000

17500

18000

18500

39000

19500

20000

Co

_m_-K

63.862

63.682

63.677

63.268

42.997

62.727

62. 438

62.134

61.816

41.486

40.617

39.711

58.790

37.872

56.970

36,096

55.252

36.668

33.686

32.965

32.287

31.650

31.056

30.495

29.976

29.486

29.031

28.606

28.208

27.837

TABLE 111.36- ConctudecL

HO(.T.).Ho(o) so(_ .(oo(..o.HO(o)}_ HOLT) .oo0")_ T

k_mol J/moI-K J/moI.K kJImol J/moI-K K

330.785 327.655 287.115 322.105 288.176 8200

339.560 328.510 288.089 330.860 289.122 8600

348.256 329.535 289.040 339,576 290.069 8600

356.928 330.532 289.972 368.268 290.958 8800

365.553 331,501 290.886 356.873 291.848 9000

374.126 332.444 291.776 365.646 292.722 9200

382.664 333.359 292.652 373.963 293.576 9400

391,101 334:250 293.510 382._21 29_._15 9600

399.696 335.115 294.350 390.816 295.236 9800

407.825 335.957 295,175 399.165 296.063 I0000

628.353 337.960 297.165 619.673 297.991 10500

648.436 339.828 299.061 639.756 299.850 11000

668.063 361.573 300.872 659,383 301.627 11500

487.227 543.205 302,603 478,547 303.326 12000

505.937 366.733 304.258 697.257 304.953 12500

524,201 366.165 305.842 515.521 306.510 15000

542.038 347.512 307.361 533.357 308,006 15500

559.661 368.779 308,818 550,781 309.638 16000

576.693 369.974 310.216 567.8i3 310.815 16500

593.154 351.106 311.561 586.474 312.139 15000

609.465 352.174 312.854 600.785 313.416 15500

625.649 353.189 314.099 616.768 314.641 16000

641.123 356.156 315.298 632.463 315.824 16500

656.508 355.072 316,454 667.828 316.965 17000

671.626 355.969 317.571 662.944 318.067 17500

686.488 356.786 318.648 677.808 319.130 18000

701.116 357.588 319.690 692.436 320.159 18500

715,525 358.356 320.697 706.845 321.154 19000

729.727 359.096 321.672 721.067 322.118 19500

763.737 359.803 322.616 735.057 323.050 20000

67

NASA/TP-3287/REV 1
TABLE In.37.- SELECTED THERMODYNAMIC FUNCTIONS FOR P(cr.white._)

T C° H°0_'H°(0) S°('0 -{ O°(T)'H°(o)}/'F H°{l_ -G°(l_/T T

K J/n_t-K kJtmol J/moI-K J/moI-K kJ/tool J/mol-K K

0 0,000 0.000 0.000 0.000 -5. 360 INFINITE 0

100 13.728 0.888 17.702 8.822 -4.472 62._22 100

/3 150 17.309 1.663 23.937 12.850 -3,697 48.58_ 150

195.40 21.117 2.533 28.986 16.023 -2.827 43.454 195.40

195.40 20.920 3.054 31.652 16.023 -2,306 43.453 195.40

200 21.092 3.151 32.141 16.386 -2.209 43.186 200

210 21.393 3.364 33.177 17.158 -1.996 42.682 210

220 21.694 3.579 34.180 17,912 -1.781 42.275 220

230 21.987 3.798 35.151 18.638 -1.562 _1.902 230

240 22.280 4.019 36.093 19.347 -1,341 41.680 240

250 22.564 4.243 37.008 20.036 -1.117 41.476 250

260 22.8_0 4.470 37.899 20.707 -0.890 41.322 260

270 23.108 4.700 38.766 21.359 -0.660 41.210 270

280 23.372 4.932 39.611 21.997 -0.428 41.140 280

290 23.627 5.167 40.436 22.619 -0.193 41.102 290

298.15 23.824 5.360 41.090 23.112 0.000 41,090 298.15

300 23.870 5.404 41.237 23.224 0.044 41.090 300

317.30 24.267 5.820 42.585 24.242 0.460 41.135 317.30

317.30 26.120 6.479 4_.662 24.242 1.119 4].135 317.30

400 26.120 8.639 50.711 29.114 3.279 42.514 400

500 26.120 11.251 56.540 3_.038 5.891 44.758 500

600 26.120 13.863 61.302 38.197 8.503 47.130 600

700 26.120 16.475 65.329 41.793 11.115 49.450 700

800 26.120 19.087 68.816 44.958 13.727 51.658 800

900 26.120 21.699 7].893 47.783 16.339 53.738 900

1000 26.120 24.311 74.645 50.334 18.951 55.694 I000

1100 26.120 26.923 77.134 52.659 21.563 57.552 llO0

1200 26.120 29.535 79.407 54.795 24.175 59.261 1200

1300 26.120 52.147 81.498 56.769 26.787 60.892 1300

i_00 26.120 34.759 83.43_ 58.606 29.399 62.43_ 1400

1500 26.120 37.371 85.236 60.322 32.011 63.895 1500

1600 26.120 39.983 86.921 61.932 34,623 65.282 1600

1700 26.120 42.595 88.505 63._49 37.235 66.602 1700

1800 26.120 45.207 89.998 64.883 39.847 67.861 1800

1900 26.120 47.819 91.410 66.242 42.459 69.063 1900

2000 26.120 50.431 92.750 67.534 _5.071 70.214 2000

2100 26.120 53.043 9_.02# 68.766 _7.683 71,318 2100

2200 26.120 55.655 95.259 69.942 50.295 72.378 2200

2300 26.120 58.267 96._01 71.067 52.907 73.397 2300

2400 26.120 60.879 97.512 72.146 55.519 74.379 2400

2500 26.120 63._91 98.578 73.182 58.131 75.326 2500

2600 26.120 66.103 99.603 7_.179 60.743 76.240 2600

2700 26,120 68.715 100.589 75.139 63.355 77.124 2700

2800 26.120 71.327 101.539 76.065 65.967 77.979 2800

2900 26.120 73.939 102.455 76.959 68.579 78.807 2900

3000 26.120 76.551 103.341 77.824 71.191 79.610 3000

3100 26.120 79.163 10_.197 78.661 73.803 80.390 3100

3200 26.120 81.775 105.026 79.472 76.415 81.147 3200

3500 26.120 8_.387 105.830 80.258 79.027 81.883 3300

3400 26.120 86.999 106.610 81.022 81.639 82.598 3400

3500 26.120 89.611 107,367 81,764 84.251 83.295 3500

5600 26.120 92.223 108,103 82.485 86.863 83.974 3600

3700 26.120 94.835 108.819 83.187 89.475 8_.636 3700

3800 26.120 97,447 109.515 83.871 92.087 85.282 3800

3900 26.120 100.059 110.194 84.537 94.699 85.912 3900

4000 26.120 102.671 110.855 85.187 97.311 86.527 4000

4100 26.120 105.283 111.500 85.8Z1 99.923 87.128 4100

_200 26.120 107.895 112.129 86.440 102.535 87.716 4200

4300 26.120 110.507 112.744 87.065 105.147 88,291 4300

4400 26.120 113.119 I13.3_4 87.636 107.759 88.854 4400

_500 26.120 115,731 113.931 88,213 110.371 89.405 4500

4600 26.120 118.343 11_.506 88.779 112.983 89.944 4600

4700 26.120 120.955 115.067 89.332 115.595 90.473 4700

4800 26.120 123.567 115.617 89.874 118.207 90.991 4800

4900 26.120 126.179 116.156 90.fi05 120.819 91.499 4900

5000 26.120 128.791 116.683 90.925 123.431 91.997 5000

5100 26.120 131.403 117.201 91,435 126.043 92.486 5100

5200 26.120 134.015 117.708 91.936 128.655 92,967 5200

5300 26.120 136.627 118.205 92,427 131.267 93.438 5300

5400 26.120 139,239 118.694 92.909 133.879 93.901 5400

5500 26.120 141.851 119.173 93.382 136.491 94.356 5500

5600 26.120 14_.463 119.644 93.847 139.103 94.80_ 5600

5700 26.120 147.075 120.106 94.303 141.715 95.244 5700

5800 26.120 149.687 120.560 94.752 14_.327 95.676 5800

5900 26.120 152.299 121.007 95.193 146.939 96.102 5900

6000 26.120 15_.911 121.4_6 95.627 149,551 96.521 6000

68 NASA/TP-3287/REV l
TABLE MI.38. - SELECTED THERMODYNAMIC FUNCTIONS FOR Pb(cr,t)

T cO Ho(T).Ho(O ) sO(T ) .{GO(.F).HO(0)}K HO(-n .GO(T)_ T

K J/r_l-K kJ/mol JlmoI-K J/moI-K k_mol JlmohK K

0 0.000 0.000 0.000 0.000 -6.870 INFINITE 0

lO0 2_.430 1.766 36.899 19.239 -5.104 87.939 lO0

200 25.770 4.289 54.346 32.901 -2.581 67.251 200

298.15 26.650 6.870 64.800 41.758 0.000 64.800 298.15

300 26.673 6.919 64.965 41.901 0.0_9 64.801 300

350 27.254 8.268 69.121 45.499 1.398 65.127 350

400 27.788 9.644 72.796 48.686 2.774 65.861 400

450 26.295 11.046 76.098 51.551 4.176 66.818 _50

500 28.785 12.473 79.105 54.158 5.603 67.8g8 500

. 13 924 81 871 56.553 7.054 69,044 550

550 29 264 .." ...... "ax7 _8 771 8 529 70.221 600 ._

600 29,736 _._vv _._ _'79o 8"549 70.237 600.6_

cr 600.65 29.742 1b.419 o_.._ ...... _iLil ....... ZLSiL .........................

! 600.65 30.627 20.231 92.481 58.799 13.361 70,237 600.65

700 30.313 23.258 97.146 63.920 16.388 73.734 700

800 29.979 26.273 101.172 68,331 19.403 76.918 800

29,255 104.684 72,179 22.385 79.812

32,206 107,794 75.588 25.336 82.458

900

900 29.660 I000

I000 29.369

II00 29.I16 35,130 110.581 78.6_5 28.260 84.890 1100

1200 28,903 38,030 113.105 81.413 31.160 87.138 1200

1300 28.731 40,912 115.411 83.941 34.042 89.225 1300

1400 28.602 43,778 117.535 86,265 36.908 91,172 1400

1500 28.513 46.633 119.505 88.416 39.763 92.996 1500

1600 28.463 _9.482 121.3_4 90.418 42.612 94.711 1600

1700 28.451 52.327 125.069 92.288 45.457 96.329 1700

1500 28.475 55.173 124.695 94.044 _8.303 97.860 1800

1900 28.532 58.023 126.236 95.698 51,153 99.314 1900

2_00 2_.620 60.881 127.702 97.262 5_.011 100.697 2000

2100 28.737 63.748 129.101 98.745 56.878 102.016 2100

2200 28.881 66.629 130.441 100.155 59.759 103,278 2200

2300 29.048 69.525 131.72g 101.500 62.655 104.487 2300

2400 29.238 72.439 132.969 102.786 65.569 105.648 2400

2500 29.446 75.373 134.167 104.017 68.503 106.765 2500

2600 29.671 78.329 135.326 105.199 71.459 107.841 2600

2700 29.909 51.308 136.450 106.336 74.438 108.880 270U

2800 30.160 84.311 137.542 107.431 77.441 109,885 2800

2900 30 _19 87.340 138,605 108,488 80.470 110,857 2900

3000 30.684 90.395 i39.6_I 109.509 85.525 111.799 3000

3100 30,953 93.477 140.651 110.497 86,607 112,713 3100

3200 31.223 96.586 141.638 111,455 89.716 113.602 3200

3300 31 492 99.722 142,603 112,384 92.852 Ii_.466 3300

3400 31,257 102.884 143.547 113.287 96.014 115.308 3400

350C _2,015 106.073 I_4._71 114.165 99.203 116.128 3500

_6UO _2.26_ 199.287 145.377 115.019 I02._17 116.928 3600

69

NASAfI'P-3287/REV 1
T C°

K J/rn_l.K

0 0,000

100 25.510

200 27.450

250 28.690

298.15 31.060

TABLE gl.39.- SELECTED THERMODYNAMIc FUNCTIONS FOR Rb(_,_

H°(T)-H°_) S°(T) -_G°(T).H°_)}_ H°(T) .Go(-r)_

kJ/mol JAm_-K J/mo_K kJ/mol J/mol-K

0.000 0.000 0.000 -7.489 INFINITE

2.009 46.958 26.868 -5._80 101.758

4.660 65.252 41.952 -2.829 _9.397

6.056 71.513 47.289 -1.433 77.245

7._89 76.780 51.662 0.000 76.780

T

K

0

i00

2O0

250

298.15

300 31.231 7.547 76.973 51.816 0.058 76.780 300

cr 312.47 32.583 7.943 78.268 52.8_8 0.454 76.815 312.67

;---;;;7;;---1;7;;; ......;;7;;; ......;;7;;i ......;;7;;; ....... ...... .......

400 30.822 12.868 92.999 60.829 5.379 79.551 _00

500 30.484 15.930 99,831 67.971 8,441 82.949 500

600 30.439 18.974 105.383 73.760 11.485 86.2_1 600

700 30.524 22.022 110.080 78.620 14.533 89.319 700

800 30.709 25.083 114.167 82,813 17.594 92.174 800

900 31.012 28.167 117.800 86.503 20.678 94,824 900

1000 31.476 31.290 121.090 89.800 23.801 97.289 i000

1100 32.151 34.470 124.120 92.786 26.981 99.592 1100

1200 33.094 57.729 126.955 95.514 30,240 101.755 1200

1300 34.366 41,099 129.652 98.037 33.610 103.798 1300

1400 36.026 44.615 132.257 100.389 37.126 105.738 1_00

1500 38.140 48.320 134.812 102.599 40.831 107.591 1500

1600 40.768 52.261 137.354 104.691 _.772 109.371 1600

1700 43.976 56.493 139.919 206.688 _9.004 111,093 1700

1800 47.828 61.077 14?.539 108.607 53.588 112.768 1800

1900 52.387 66,082 145.2_3 110.463 58.593 114.405 1900

2000 57.719 71.581 148.063 112.272 64.092 116.017 2000

Z100 65.887 77.654 151.024 11_.0_6 70.165 117.612 2100

70 NASA/TP-3287/REV 1
TABLE ILL40.- SELECTED THERMODYNAMIC FUNCTIONS FOR S(=,#J)

T C° H°(T).H°(0) S°('TJ -{G°('r)oH°(0)}_ H°(T) -G°(OK T

K J/r_-K kJ/moi J/moI-K J/mol-K kJ/mo/ _mol.K K

O 0.000 0.000 0,000 0.000 -6,612 INFINITE 0

i00 12.765 0.690 12.541 5.661 -3.722 69,761 100

200 19.360 2.332 23.659 11.999 -2.080 36.059 200

298.15 22.690 6.612 32.070 17.272 0.000 32.070 298.15

300 22.737 6.655 32.210 17.360 0.063 32.067 300

368.30 26.237 6.061 37.050 20.572 1.669 32.551 368.30

368.30 26.773 6.662 38.119 20.572 2.050 32.551 368.30

388.36 25.180 6,966 39.666 21.511 2.552 32.871 388.36

388.36 31.710 8.685 63.875 21.511 6.273 32.871 388.36

600 32.369 9.060 66,826 22.175 6,668 33.205 600

628.15 36.595 10,006 67.103 23.739 5.592 36,064 628.15

432.25 68.833 10.176 67.502 23.961 5.766 36.168 632.25

653.15 62.672 11.121 69.638 25.096 6.709 36.835 653.15

500 38.026 12.996 53.578 27.586 8.586 36.610 500

550 35.61_ 16.830 57.076 30.112 10.618 38.136 550

600 34.371 16.577 60.116 32.689 12.165 39.862 600

650 33.693 18.273 62.832 36.720 13,861 61.508 650

700 32.651 19.923 65.278 36.817 15.511 43.120 700

717 31.992 20,671 66.052 37.501 16.059 63.656 717

800 32.000 23,127 69.557 60.668 18.715 66.163 800

900 32.000 26,327 73.326 66.076 21.915 68.976 900

1000 32,000 29,527 76.697 67.170 25.115 51.582 1000

1100 32.000 32.727 79.767 69.995 28,315 5_.006 1100

1200 32.000 35.927 82.532 52.592 31.515 56.269 1200

1300 32.000 39.127 85.093 56.995 36.715 58.389 1300

1600 32.000 _2.327 87.666 57.231 37.915 60.382 1600

1500 32.000 65.527 89.672 59.321 61.115 62.262 1500

1600 32,000 68.727 91.737 61.283 46.315 66.061 1600

1700 32.000 51.927 93.677 63.132 67.515 65.727 1700

1800 32.000 55,127 95.506 66.880 50.715 67.331 1800

1900 32.000 58.327 97.237 66.538 53.915 68.860 1900

2000 32.000 61.527 98.878 68.116 57.115 70.320 2000

2100 32.000 66.727 100.639 69.617 60.3]5 71.718 2100

2200 32.000 67.927 101.928 71.052 63.515 73.057 2200

Z300 32.000 71,127 103.550 72.626 66.715 76.366 2300

2600 32.000 76.327 106.712 73.763 69.915 75.581 2600

2500 32.000 77.527 106.019 75.008 73.115 76.773 2500

2600 32.000 80.727 107.276 76.225 76.315 77.922 2600

2700 32.000 83.927 108.681 77.397 79.515 79.031 2700

2800 32.000 87.127 109.665 78.528 82.715 80.106 2800

2900 32.000 90,327 110.768 79.621 85.915 81.162 2900

3000 32.000 93.527 111.853 80.677 89.115 82.168 3000

3100 32.000 96.7Z7 112.902 81.700 92.315 83.123 3100

3200 32.000 99.927 113.918 82.691 95.515 86.070 3200

3300 32.000 103.127 116.903 83.652 98.715 84.989 3300

3600 32.000 106.327 115.858 86.585 101.915 85,883 3600

3500 32.000 109.527 116.786 85.492 105.115 86.753 3500

3600 32.000 112.727 117.687 86.376 108.315 87.600 3600

3700 32.000 115.927 118.566 87.232 111.515 88.625 3700

3800 32.000 119.127 119,617 88.068 116.715 89.229 3800

3900 32.000 122.327 120.269 88.883 117.915 90.016 3900

6000 32.000 125,527 121.059 89.677 121.115 90.780 6000

6100 32.000 128.727 121.869 90.652 126.315 91.528 6100

6200 32,000 131,927 122.620 91.209 127.515 92.259 6200

6300 32.000 135.127 123.373 91.968 130.715 92.976 6300

6600 32.000 138.327 126.109 92.671 133.915 93.673 6600

6500 32,000 161,527 126.828 93.377 137.115 96.358 6500

6600 32.000 166.727 125.531 96.069 160.315 95.028 6600

6700 32.000 167.927 126.219 96,765 163,515 95.686 6700

6800 32.000 151.127 126.893 95,608 166.715 96.527 6800

6900 32.000 156.327 127.553 96.057 169.915 96.958 6900

5000 32.000 157.527 128.199 96.694 153.115 97.576 5000

5100 32.000 160.727 128.833 97.318 156.315 98.183 5100

5200 32.000 163.927 129.656 97,930 159.515 98.778 5200

5300 32.000 167.127 130.066 98.531 162.715 99.363 5300

5600 32.000 170.327 130.662 99.120 165.915 99.937 5600

5500 32.000 173.527 131.269 99.699 169.115 100.501 5500

5600 32.000 176.727 131.826 100.267 172.315 101.055 5600

5700 32.000 179.927 132.592 100.826 175.515 101.600 5700

5800 32.000 183.127 132.969 101.375 178.715 102.136 5800

5900 32.000 186.327 133.696 101.915 181.915 102.665 5900

6000 32.000 189,527 136.036 102.6_6 185,115 103.181 6000

NASA/TP-3287/REV 1 71
TABLE 111.41.- SELECTED THERMODYNAMIC FUNCTIONS FOR Si(cr,I)

T Co HO(-T).Ho(O) sO(T) .{GO('T').H°(0))ff H°('T) _°{"r)_ T

K J/n_K kJ/rrlol J/moI.K J/m_-K kJ/mol J/m_-K K

0 0.000 0.000 0,000 0.000 -3.217 INFINITE 0

100 7,280 0.267 3.828 1,158 -2.950 33.333 I00

200 15.650 1.4_3 11.657 4.442 -1.774 20.529 200

250 IB.IZ6 2.305 15.471 6.251 -0.912 19.121 250

298.15 19.789 3.217 18.810 8.019 0.000 18.810 298.15

3UO 19.855 3.254 18.933 8.085 0.037 18.810 300

400 22.301 5,377 25.023 11.580 2.160 19.624 400

500 23.610 7.678 30.152 14.796 4.461 21.231 500

600 24.472 10.085 34.537 17.730 6.867 23.092 600

700 25.124 12.566 38.361 20.410 9.3_8 25.006 700

800 25.662 15.106 41,752 22,870 11.888 26.891 800

900 26.135 17.696 64,802 25.140 ]4.478 28.715 900

1000 Z6.568 20.331 47.578 27.247 17.114 30._64 1000

ii00 26.974 23.009 50,130 29.213 19.791 32.138 Ii00

1200 27,362 25.725 52.493 31,055 22.508 33.737 1200

1300 27.737 28.481 54.698 32.790 25.263 35.265 1300

1400 28.103 31,273 56.767 3_.430 28,055 36.728 1400

1500 28.462 34.101 58.719 35.985 30.883 38.130 1500

1600 28.816 36.965 60.567 37,464 33.747 39.475 ]600

cr 1690 29.131 39.572 62,152 38.737 56.355 40.640 1690

Q 1690 27.200 89.782 91.862 38.737 86.565 40.640 1690

1700 27.200 90.054 92.023 39.050 86.837 40.9_2 1700

1800 27.200 92.774 93.578 42.036 89.557 43.824 1800

1900 27.200 95._94 95.048 44.788 92.277 46.481 1900

2000 27.200 98.214 96.443 47.336 94.997 48.945 2000

2100 27.200 100.93_ 97.770 49.706 97.717 51.239 2100

2200 27.200 103.654 99.036 51.920 100.437 53.583 2200

2300 27.200 106.374 100.245 53.995 103.157 55.394 2300

2400 27.200 109.094 101.402 55.946 105.877 57.287 2400

2500 27.200 111.814 102.513 57.787 108.597 59.074 2500

2600 27.200 114.536 103.580 59.528 111.317 60.765 2600

2700 27.200 117.254 I0_.606 61.179 114.037 62.370 2700

2800 27.200 119.974 105.595 62.747 116.757 63.896 2800

2900 27.200 122.694 106.550 64.241 119.477 65.351 2900

3003 27.200 125.414 1071472 65.667 122.197 66.740 3000

3100 27.200 128.134 108.364 67.030 124.917 68.068 3100

32_0 27.200 130.854 109.227 68.335 127.637 69.341 3200

3300 27.200 133.574 110.064 69.587 130.357 70.562 3300

3400 27,200 136.294 110.876 70,790 133.077 71.736 3400

35C3 27.Z00 139.014 111.665 71,946 135.797 72.866 3560

3600 27.200 141.734 112._31 73,060 138.517 73.954 3600

3700 2! 200 144,454 113.176 74.135 141.237 75.004 3700

_Su_ 27 200 147.174 113.902 75.172 1_3,957 76.018 3800

30o_ 27 200 149.894 114.608 76.174 146,677 76.999 3900

_ooo _7._00 152.614 115.297 77.143 149.397 77.948 4000

4lOC _" 200 155.334 115.969 78.082 152.117 78.867 4100

_20r .': 200 158.054 116.624 78.992 154.837 79.758 4200

_3n0 :_._03 160.77_ 117.264 79.875 157.557 80.623 4300

_oo _'.700 163.49_ 117,889 80.732 160.277 81.463 4400

_buc 2_ _00 166.214 118.501 81.564 162.997 82.279 4500

_600 37.200 168,934 119,098 82.374 165.717 83.073 4600

_700 27.209 171.654 119.683 83.161 168.437 83.866 4700

_oo 21._00 174.374 120.256 83.928 171.157 84.598 4800

_9_0 27.200 177.094 120.817 8_.675 173.877 85.332 _900

5000 27.200 179.814 121.366 85.404 176.597 86.047 5000

5100 27.200 182.534 121.905 86.114 179.317 86.745 5100

5200 27.200 185.254 122.433 86.807 182.037 87.426 5200

5300 27.200 187,974 122.951 87.484 184.757 88.092 5300

5400 27.200 190.694 123.460 88.146 187.477 88.7_2 5400

5500 27.200 193,414 123.959 88.793 190,197 89.378 5500

5600 27.200 196.134 124.449 89.425 192,917 90.000 5600

5700 27.200 198.854 12_.930 90.044 195.637 90.608 5700

5800 27.200 201.574 125.403 90.649 198.357 91.20_ 5800

5900 27.200 204.294 125.868 91.242 201.077 91.788 5900

6000 27.200 207.014 126.326 91.823 203.797 92.359 6000

72 NASA/TP-3287/REV 1
TABLE nl,42.. SELECTED THERMODYNAMIC FUNCTIONS FOR Sn(cr,t)

T cO HO03.HO(0) sO(D .(GO(D.HO(0)}_ HO(-0 .G°0DK T

K J/m_-K _/mol J/moI-K J/moFK kJ/mol Jim.oK K

0 0.000 0.000 0.000 0,000 -6.323 INFINITE 0

100 2Z.210 1.318 24.020 10.840 -5.005 74.070 100

200 25.500 3.740 40.670 21,970 -2.583 53.585 200

298.15 27.112 6.323 51.IB0 29.973 0.000 51.180 298.15

300 27.167 6.376 51.348 30.101 0.051 51.178 300

350 28.025 7.756 55.599 33.645 1.431 51.510 550

400 20.903 9,176 59.398 36.458 2.853 52.265 400

650 29.887 10.646 62.858 39.200 4.323 53.251 450

500 31.033 12.168 66.065 41.729 5.845 54.375 50D

cr 505.12 31.160 12.327 66,381 41.976 6.004 54.494 505.12

....... -..... ...... ...... ;o?;3;...... ;;-;;; ...... ...... .......

, 12 2 663 222 , 85.619 48.496 15.951 59.034 600

700 28.269 25.117 90.003 54.121 18.79_

800 28.043 27.931 93.760 58.847 21.608

900 27.957 30.730 97,057 62.913 24._07

1000 27.945 33.5Z6 100.002 66.477 27.201

II00 27,979 36.320 102.666 69.648 29.997

1200 28.044 39.121 105.]03 72.502 32.798

1300 28.130 41.930 107.351 75.098 35.607

1400 28.229 44.748 109.440 77.477 58.425

1500 28.339 47.576 111.391 79.674 41.253

1600 28.655 50.616 I13.223 81.714 44.093

1700 28.575 53,267 114.952 83.619 _6.944

IBO0 28.698 56.131 116.589 85.405 49.808

1900 28,822 59,007 118.144 87.088 52.684

2000 28.947 61.895 119.625 88.678 55.572

2100 29.071 64.796 121.041 90.186 58.473

2200 29.195 67.709 122.396 9].619 61.386

2300 29.318 70.635 123,696 92.986 64.312

2400 29.439 73.573 124.947 94.291 67.250

2500 29.559 76.523 126.151 95.542 70.200

2600 29.676 79.684 127.315 96.742 73.161

2700 29.792 82.458 128.435 97.895 76.155

2800 29.905 85.463 129.520 99.005 79,120

2900 30.015 88.439 130.572 100.075 82.116

3000 30.123 91,446 131.591 101.109 55.123

3100 30.228 96.463 132,580 I02.I08 88.140

3200 30,351 97.491 133.542 103.076 91.168

3300 30.451 100.529 134.477 104.013 94.206

3400 30.528 103.577 135.386 104.923 97.256

3500 30.622 106.635 136.273 105.806 100.312

3600 30.713 109.701 137.137 106.666 103.378

3700 30.801 112.777 137.979 107.499 106.454

3800 30.886 115.862 138.802 108.312 109.539

3900 30.968 118.954 139.605 I09.104 112.631

4000 31.047 122.055 140.390 109.877 115.732

4100 31.123 I25.166 141.158 110.630 118.841

4200 31.196 128.280 141.909 III.366 121.957

4300 31.266 131.403 142.644 112.085 125.080

6400 31.333 134.533 143.363 112.788 128.210

4500 31.396 137.669 144.068 113.475 131.366

4600 31.657 140.812 144.759 114.148 136.489

4700 31.514 163.960 145.436 114.806 137.637

63.154

66.751

69.938

72.800

75.396

77.772

79.962

81.995

83.889

85.666

87.338

88.918

90.416

91.839

93.196

96.493

95,735

96.926

98.071

99.174

100,237

101.263

102.256

103.217

104.148

105.052

105.929

106.782

107.612

108.420

109.208

109.976

110.725

111.457

I12.172

112.872

113.555

114.225

114.880

115.522

116.151

700

800

900

I000

II00

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

Z800

2900

3000

5100

3200

5300

3400

3500

3600

3700

5800

3900

4000

_100

4200

4300

4600

4500

4600

4700

73

NASA/TP-3287/REV 1
TABLE I/I.43.

- SELECTED THERMODYNAMIC FUNCTIONS FOR 8r(a,_,l)

TC° H°(T)-H°(O]

K J/m_-K kNmol 0 0.000 0.000

100 23.596 1.489

120 24.250 1.968

140 24.773 2.458

160 25.188 2.958

180 25.515 3._65

200 25.777 3.978

220 25.995 4.496

240 26.192 5.018

260 26.388 5.5q3

280 26.606 6.073

298.15 26.830 6.558

300 26.837 6.608

350 27.376 7.964

400 27.846 9.344

450 28.271 10.747

500 28.665 12.171

600 29.386 15.074

700 30.038 18.06,6

800 30.635 21.080

a 820 30.748 21.694

s°cr)

JtmoI-K

0. 000

27. 350

31.712

35.491

38 827

41 81 _,

4el 516

46 983

6,9 254

51 358

53 321

54.999

55.165

59.34_.

63.031

66.335

69.335

7_.626

79.205

83.256

84.014

"{GO_'H°_)}_ HO_) -G°(T)KT

J/m_-K k_mol J/m_KK

0.000 -6.558 INFINITE0

12,461 -5.069 78.044 100

15.315 -4.591 69.968 120

17.934 -4.100 64.778 I_0

20.341 -3.600 61.330 160

22.564 -3.093 58.999 180

24.626 -2.580 57.q17 200

26.548 -2.063 56.358 220

28.347 -1.541 55.673 240

30.037 -1,015 55.261 260

31.631 -0.485 55.053 280

33.003 0.000 54.999 298.15

33.139 0.050 55.000 300

36.591 1.405 55.328 350

39.670 2.786 56.065 400

42.452 4.189 57.026 450

44.993 5.613 58.109 500

49.502 8.516 60.433 600

53.425 11.488 62.79Q 700

56.906 14.522 65.104 800

57.558 15.136 65.556 820

820 29.824 22.544 85.050 57.558 15.986 65.556 820

900 30.146 24.943 87.801 60.127 18.384 67.414 900

1000 30.548 27.977 91.038 63.061 21.419 69.619 1000

10ql 30.713 29.233 92.269 64.187 22.675 70.487 1041

f 1041

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

_000

_100

_200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

37 000

37 000

37 000

37 000

37 000

37 000

37.000

37.000

37,000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37,000

37.000

37.000

37.000

37.000

37.000

37.000

37,000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.000

37.233 99.954 64.187 30.675 70.487 1041

39.416 101.994 66.161 32.858 72.123 1100

43.116 105.213 69.283 36.558 74.748 1200

46.816 108.175 72.162 40.258 77.207 1300

50.516 110.917 74.834 _3.958 79.518 1400

54.216 113.470 77.325 47.658 81.698 1500

57.916 115.857 79.660 51.358 85.759 1600

61,616 I18.I01 81.856 55.058 85.714 1700

65.316 120.215 83.929 56.758 87.572 1800

69.016 122.216 85.892 62.458 89.343 1900

72.716 124.iI_ 87.756 66.158 91.035 2000

76.416 125.919 89.530 69.858 92.653 2100

80.116 127.640 91.224 73.558 94.205 2200

83.816 129.285 92.843 77.258 95.695 2300

87.516 130.860 96,.395 80.958 97.127 2400

91.216 132.370 95.884 84.658 98.507 2500

94.916 133.821 97,_15 88.358 99.837 2600

98.616 135.218 98.693 92.058 101.122 2700

102.316 136.563 100.022 95.758 102.364 2800

106.016 137.862 101.304 99._58 103.566 2900

109.716 139.116 102.544 103.158 10_.730 3000

113.416 I_0.329 103,76,3 106.858 105.859 3100

117.116 141.504 104.905 110.558 106.955 3200

120.816 16,2.642 106.032 114.258 108.019 3300

124.516 143.7_7 107.125 117.958 109.054 3400

128,216 144.820 108.186 121.658 110.060 3500

131.916 16,5.862 109.219 125.358 111.040 3600

135.616 146.876 110.223 129.058 111.995 3700

139.316 147.862 111.200 132.758 112.926 3800

143.016 148.823 112.153 136.458 113.83_ 3900

I_6.716 149,760 113.081 140.158 114.721 4000

150.416 150.674 113,987 143.858 115.587 4100

154.116 151.565 114.871 147.558 116.433 4200

157.816 152.436 115,735 151.258 117.260 4300

161.516 153.287 116.578 154.958 118.069 4400

165.216 154.118 117.403 158.658 118.861 4500

168.916 154.931 118.211 162.358 119.636 _600

172,616 155.727 119.000 166.058 120.396 4700

176.316 156.506 119.774 169.758 121.140 4800

180.016 157.269 120.531 173.458 121.869 4900

183.716 158.017 121.273 177.158 122.585 5000

187.416 158.749 122.001 180.858 123.287 5100

191.116 159.468 122.715 184.558 123.976 5200

194.816 160.172 123.415 188.258 124.652 5300

198.516 160.864 124.102 191.958 125.316 5400

202.216 161.543 12_.776 195.658 125.969 5500

205.916 162.210 125._39 199.358 1Z6.610 5600

209.616 162.865 126.090 203.058 127.240 5700

213.316 163.508 126.729 206.758 127.860 5800

217.016 164.141 127.358 210.458 128.470 5900

220.716 164.762 127,976 214.158 129.069 6000

74 NASMTP-3287/REVl
TABLE 111,44.- SELECTED THERMODYNAMIC FUNCTIONS FOR Ta(cr,t)

T C° HO{T).HO(0) so(3] .{GO(T).HO(0))_ HO09 _°(T)_ T

K J/m_-K _/mo! JhnoFK J/moI-K _/mol Jlm_-K K

0 0,000 0.000 0.000 0.000 -5.681 INFINITE 0

100 191744 0.995 16.143 6.193 -4.686 63.003 100

150 22_814 2.072 24.833 II.020 -3.609 48.893 150

200 24.085 3.247 31.586 15.351 -2.434 43.756 200

250 24.861 4.472 37.049 19.161 -I,209 41.885 250

298.15 25.295 5.681 41.471 22.417 0.000 41.471 298.15

300 25.307 5,728 41,628 22.535 0.047 41.471 300

350 25.598 7.001 45.552 25.549 1.320 41.781 350

400 25.840 8.287 48.986 28.268 2.606 42.471 400

450 26.088 9.585 52.044 30.744 3.904 43.368 450

500 26,349 10.896 54.806 53.014 5.215 44.376 500

550 26.606 12.220 57.330 35.112 6.539 45.441 550

600 26.8_3 13.556 59.655 37.062 7.875 46,530 600

700 27.214 16.260 63,822 40.595 10.579 48.709 700

800 27,459 18.994 67.473 43.730 13.315 50.832 800

900 27,668 21.750 70,718 46.551 16.069 52.864 900

1000 27.933 24.529 73.647 49.118 18.848 5_.799 1000

II00 28.281 27.340 76.325 51.470 21.659 56.635 II00

1200 28.662 30,188 78.802 53.645 24.507 58.379 1200

1300 28.989 33.071 81.110 55.671 27.390 60.041 1300

1400 29.202 35.982 83.267 57,566 30.301 61.623 1400

1500 29.319 38.908 85.286 59,347 33.227 63.135 1500

1600 29.439 41.8_5 87.182 61.029 36,164 64.579 1600

1700 29,688 _4.800 88.975 62.620 39.119 65.962 1700

1800 30.124 47.789 90,682 64.133 42.108 67,289 1800

1900 30,665 50.829 92.325 65.573 45.148 68.565 1900

ZOO0 31.191 53.921 93.911 66.951 48.240 69.791 2000

2100 31.713 57,067 95.445 68.270 51.386 70.975 2100

2Z00 32.252 60.265 96.933 69.540 54,584 72,122 2200

2300 32.828 63.518 98.379 70.762 57.837 73.232 2300

2400 33.459 66.832 99.789 71.942 61.151 74.309 2400

2500 34.167 70.213 101.169 73.084 64.532 75.356 2500

2600 34.970 73.669 102.525 74.191 67.988 76.576 2600

2700 _5,890 77.211 103.861 75.264 71.530 77.368 2700

2800 36.9_6 80.851 105.185 76.310 75.170 78.339 2800

2900 38.158 84.605 106,502 77.328 78.924 79.287 2900

3000 39.546 88.489 107,819 78.323 82.808 80.216 3000

3100 41.130 92.521 109.141 79.296 86.840 81.128 3100

42 930 96 722 110 474 80 248 91 041 82,024 3200 3200 • • " " " 4 82 538 3258

_ _x 4 80 99 245 111 256 80.794 95.56 •

.....................................

- j7840 13;813 122;80 - -;;7;;;--- 130.132 82.558 3258 5300 41.840 137.570 123.016 81.328 151.889 83.049 3500

3400 41.840 141.754 -124.265 82.572 136.073 84.245 3400

3500 41.840 145.938 125.478 83.781 1_0.257 85.404 3500

3600 41.840 150.122 126.656 84.956 144.441 86.534 3600

3700 41.840 154,306 127.805 86.098 148.625 87.634 3700

5800 41.840 158,490 128.919 87.211 152.809 88.706 5800

5900 41.840 162.674 130.005 88.294 156.995 89.751 3900

4000 41.840 166.858 131.065 89.350 161.177 90.770 4000

4100 41.840 171.0_2 132.098 90.380 165.361 91.766 4100

4200 41.840 175.226 133.106 91.386 169.545 92.738 4200

4300 41,840 179.410 134.091 92.367 173.729 93.688 4300

4400 41.840 185.594 135.052 93.327 177.913 94.618 4400

4500 41.840 187.778 155.993 94.264 182.097 95.527 4500

4600 41.840 191.962 136.912 95.181 186.281 96.416 4600

4700 _1.840 196.146 137.812 96,079 190.465 97.288 4700

4800 41.840 200.330 138.693 96.958 194.649 98.141 4800

4900 41.840 204.514 139.556 97.818 198.833 98.978 4900

5000 41.840 208.698 140.401 98.661 203.017 99.798 5000

5100 41.840 212.882 161.250 99.488 207.201 100.60_ 5100

5200 41.840 217.066 142.042 100.299 211.385 101.391 5200

5300 41.840 221.250 142.839 101.094 215.569 102.166 5300

5400 41.840 225.434 143.621 101.874 219,753 102.926 5400

5500 41.840 229.618 144.389 102.640 223.937 103.673 5500

5600 41.840 253.802 145.143 103.392 228.121 104.407 5600

5700 41.840 257.986 145.883 104.131 252,305 105.128 5700

5800 41.840 242.170 146.611 104.857 236._89 105.837 5800

5900 41.840 246.354 147.326 105.571 240.673 106.534 5900

6000 41.840 250.538 148.029 106.273 244.857 107.220 6000

75

NASA/TP-3287/REV l
TABLE 111.45.• SELECTED THERMODYNAMIC FUNCTIONS FOR Th(=,8,/)

T C° H°0")'H°(0) S°(T) "{G°(T')'H°(O)}E H°(T) -G°0")_ T

K JIr_.K kJ/rnol _moi-K J/mot-K kJ/mol J/moI-K K

0 0.000 0.000 0,000 0,000 -6.350 INFINITE D

100 22.690 1.393 24.814 10.884 -4.957 74.384 100

200 25.260 3.820 41.541 22.441 -2.530 54.191 200

298.15 26.230 6.350 51.830 30.532 0.000 51.830 298

300 26.245 6.399 51.992 30.662 0,0_9 51.829 300

400 27.084 9.065 59.656 36.993 2.715 52.868 400

500 27.953 11,816 65.793 42.161 5.466 54.861 500

600 28,834 14.656 70.967 46.540 8.306 57.124 600

700 29,720 17.583 75.478 50.359 11.233 59,431 700

800 30.609 20.600 79.505 53.755 1_.250 61.692 800

900 31.500 23.705 83.162 56.823 17.355 63.879 900

1000 32,391 26.900 86.527 59.627 20.550 65.977 1000

1100 33.284 30.183 89.656 62.217 23.833 67,990 1100

1200 34.177 35.556 92,590 64.627 27.206 69.918 1200

1300 35.070 37.019 95.361 66.885 30.669 71.769 1500

1400 35.964 40.570 97.993 69,01_ 34.220 73.550 1400

1500 36.858 44.212 100.504 71.029 37.862 75.263 1500

.15

1600 37,751 47,942 102.912 72.948 41.592 76.917 1600

1650 38.198 _9.841 104.080 73.873 43._91 77.722 1650

............................................................................................

1650 35.419 53.3_i 106.201 73.873 46.991 77.722 1650

1700 56,D17 55.127 107.268 74.840 48.777 78.576 1700

1800 37.212 58.788 109.360 76.700 52.438 80.228 1800

1900 38.407 62.569 111.404 78.473 56.219 81.815 1900

2000 39.602 66.469 113.404 80.169 60.119 83.344 2000

2023 39.877 67.383 113.858 80,550 61.033 83,689 2023

............................................................................................

t 2023 46.000 81.183 120.680 80.550 74.833 85.689 2023

2100 46,000 84.725 122.399 82.053 78.375 85.077 Zl00

2200 46.000 89.325 124.539 83.936 82.975 86,822 2200

2300 46.000 93.925 126.583 85.746 87.575 88.507 2300

2400 46.000 98.525 128.541 87.489 92.175 90.135 2400

2500 46.000 103.125 130.419 89.169 96.775 91.709 2500

2600 46.000 107.725 132.223 90.790 101.375 93.232 2600

2700 46.000 112.325 133.959 92.357 105.975 94.709 2700

2800 _6.000 116.925 135.632 93.873 110.575 96.141 2800

2900 46.000 ]21.525 137.246 95.341 115.175 97,531 2900

3000 46.000 126.125 138.806 96.764 119.775 98.881 3000

3100 46.000 130,725 140.314 98.145 124.375 100,193 3100

3200 46.000 135.325 141.774 99,485 128.975 101.470 3200

3300 46.000 139.925 143.190 100.788 133.575 102.713 3300

3400 46.000 144.525 144.563 102.056 138.175 103.923 3400

3500 46,000 149.125 145.897 103.289 142.775 105.104 3500

3600 46.000 153.725 147.193 104.491 147.375 106.255 3600

3700 46.000 158.325 148.453 105.662 151.975 107.378 3700

3800 46.000 162.925 I_9.680 106.804 156.575 108.476 3800

3900 46.000 167.525 150.874 107.919 161.175 109.547 3900

4000 46.000 172.125 152.039 109.008 165.775 110.595 4000

4100 46.000 176.725 153.175 110.071 170.375 111.620 4100

4200 _6.000 181.325 154.283 IIi.III 174.975 112.623 4200

4300 46,000 185.925 155.366 112.127 179.575 113.604 4300

4400 46.000 190.525 156.425 113.122 184.175 114.565 4400

4500 46.000 195.125 157._57 114.096 188,775 115.507 4500

4600 46.000 199.725 158.468 115,050 193.375 116.430 4600

4700 46.000 204.325 159,457 115.984 197.975 117.335 4700

4800 46.000 208.925 160,426 116,900 202.575 118.223 4800

4900 46.000 213.525 I61.374 117,798 207,175 119.094 4900

5000 46.000 218.125 162.304 118.679 211.775 119.949 5000

5100 46.000 222.725 163.215 119.543 216.375 120.788 5100

5200 46.000 227.325 164.108 120.391 220.975 121.613 5200

5300 46.000 231.925 164.984 121.225 225.575 122.423 5306

5400 46.000 236.525 165.8_4 122.043 230.175 123,219 5400

5500 46.000 241.125 166,688 122.847 234.775 124.002 5500

5600 46.000 245.725 167.517 123.637 239.375 124.771 5600

5700 46.000 250,325 168.331 124.414 243.975 125.528 5700

5800 46,000 254.925 169.131 125.178 248.575 126.273 5800

5900 46.000 259.525 169.917 125.930 253.175 127.006 5900

6000 46.000 264.125 170.690 126.670 257.775 127.728 6000

76 NASA/TP-3287/REV l
TABLE ttl46 - SELECTED THERMODYNAMIC FUNCTIONS FOR Ti(a,#J)

T C° HO(T).Ho(0) sO(T) _{GO(1-).Ho(O)}ff Ho_) .G°(T)_ T

K J/n_l-K _/mol J/moI-K J/m_-K kJ/rr_ J/m_K K

0 0.000 0,000 0.000 0.000 -4.824 INFINITE 0

I00 14.310 0.559 8.229 2.639 -4.265 50.879 I00

200 22.300 2.477 21,204 8.819 -2.347 32,939 200

298.15 25.060 4.824 30,720 14.540 0.000 30.720 298.15

300 25.095 4.870 30.875 lq.6_2 0.006 30.722 300

400 26.380 7.451 38.291 19.665 2.627 31.723 qO0

500 27.349 10.137 04.281 24.007 5.313 33.655 500

600 28.411 12.925 49.360 27.818 8.101 35.858 600

700 29.511 15.821 53.822 31.221 10.997 38.112 700

800 30.456 18.822 57.828 34.300 13.998 40.330 800

900 31.002 21.899 61.452 37.120 17.075 42.480 900

1000 32.681 25.045 64,764 39.719 20.221 4_.545 1000

1100 39.222 28.597 68.146 02.149 23.773 46,534 Ii00

e 1156 45.189 30.953 70.233 43.457 26.129 47.630 1156

...... ...... - ...... ...... ...... ......

1200 28.565 35.997 74.576 44.578 31.173 48.598 1200 13oo 29.952 38922 76.917 6977 34.098 50.688 1300

1400 31._02 41,989 79.189 49.197 37.165 52.643 1400

1500 32.916 45.204 81.407 51.271 40.380 54.487 1500

1600 34.494 48.574 83.581 53.222 43.750 56.237 1600

1700 36.136 52.105 85.721 55.071 47.281 57.909 1700

1800 37.841 55,804 87.835 56.835 50.980 59.513 i800

1900 39.611 59.676 89.928 58.520 54.852 61.059 I900

1944 40.409 61.436 90.844 59.241 56.612 61.723 1944

............................................................................................

194_ 46.800 76.036 98.354 59.241 71.212 61.723 1944

2000 46.800 78.657 99.683 60.355 73.833 62.767 2000

2100 06.800 83.337 101.967 62.283 78.513 6_.580 2100

2200 46.800 88.017 104.144 6_.136 83.193 66.329 2200

2300 46.800 92.697 106.224 65.921 87.873 68.019 2300

2400 46.800 97.377 108.216 67.6_2 92.553 69.652 2400

2500 46.800 102.057 110.126 69.304 97.233 71.233 2500

2600 _6.800 106.737 III_962 70.909 101.913 72.765 2600

2700 46.800 111.417 113.728 72._63 106.593 74.249 2700

2800 _6.800 116.097 115.430 73.967 111.273 75.690 2800

2900 46.800 120.777 117.072 75.425 115.953 77,089 2900

3000 46.800 125.457 118.659 76.8_0 120.633 78,_8 3000

3100 _6.800 130.137 120.194 78.21_ 125.313 79.770 3100

3200 46.800 134.817 121.679 79.549 129.993 81.057 3200

33B0 46.800 139._97 123.120 80.8_8 134.673 82.310 3300

3400 _6.800 144.177 124.517 82.112 139.353 83.531 3400

3500 46.800 1_8.857 125.873 83.343 I_4.033 84.721 3500

3600 46.800 153.537 127.192 84.543 148.7_3 85.883 3600

3700 _6.B00 158.217 128,474 85.713 153.393 87.017 3700

3800 46.800 162.897 129.722 86.855 158.073 88.124 3800

3900 q6.800 167.577 130,938 87.969 162 v53 89.206 3900

4000 46.800 172.257 132.123 89,058 167._33 90.264 4000

_I00 _6.800 176.957 133.278 90.123 172.113 91.300 4100

4200 46.800 181.617 13_.406 91.164 176.793 92.312 4200

4300 _6.800 186.297 135.507 92.182 181.473 93.304 4300

4400 46.800 190.977 136.583 93.179 186.153 94.276 4400

4500 46.800 195.657 137.635 94.156 190.833 95.228 4500

4600 46.800 200.337 138.663 95.112 195.513 96.161 4600

4700 46.800 205.017 139.670 96.049 200.193 97.076 4700

q800 46.800 209.697 lq0.655 96.968 204.873 97.973 _800

4900 46.800 214.377 I_1.620 97.870 209,553 98.854 4900

5000 46.800 219,057 142.566 98,754 214.233 99.719 5000

5100 46.800 223.737 143._92 99.623 218,913 100.568 5100

5200 46.800 228.417 144.401 100.475 223.593 101.403 5200

5300 _6.800 233.097 145.293 101.312 228.Z73 102.222 5300

5400 _6.800 237.777 146.168 102.I35 232.953 103.028 5400

5500 46.800 242.457 I_7.026 102.943 237.633 103.820 5500

5600 q6.800 247.137 147.870 103.738 2_2.313 104.599 5600

5700 46.800 251.817 148.698 104.519 246.993 I05.366 5700

5800 _6.800 256.497 149.512 105.288 251.673 106.120 5800

5900 q6.800 261.177 150.312 106.045 256.353 106.862 5900

6000 46.800 265.857 151.098 106.789 261,033 107.593 6000

NASAFrP-3287/REV l 77
TABLE I|1.47.- SELECTED THERMODYNAMIC FLI:NC'TION$FOR U(a,,B,'r.g

T C° H°(T)'H°(O) S°CD -_G°(T)-H°[O)}_ H°CD _°FD_ T

K J/r_l-K k_mol J/m_K J/m_-K _/mol J/mokK K

0 0.000 0.000 0.000 0.000 -6.364 INFINITE 0

100 22.240 1.299 22.740 9.750 -5.065 73.390 100

200 25.830 3.738 39,500 20,810 -2.626 52,630 200

298.15 27.665 6.364 50.200 28.855 0.000 50.200 298.15

300 27.703 6.415 50.371 28.988 0.051 50.201 300

400 29,699 9.285 58.613 35,400 2.921 51.310 400

500 31.952 12,364 65.475 40.747 6.000 53.475 500

600 3_.652 15.690 71.531 45.381 9.326 55.988 600

700 37.864 19,312 77.108 49.519 12.948 58.611 700

&O0 _1,614 23.281 82.402 53.301 16.917 61.256 800

900 45.916 27.653 87,547 56.821 21.289 63.893 900

• 942 47.889 29.622 89,685 58.239 23.258 6_.995 942

# 942 42.400 32.402 92.636 58.239 26.038 64.995 942

1000 42.400 34.861 95.170 60.308 28.497 66.672 1000

B 1049 42.400 56.959 97.198 61.984 30.575 68.051 1049

...........................................................................................

7 1049 38.300 41.669 101.707 61.984 35.305 68.051 1049

ii00 38.300 43.622 103.525 63.868 37.258 69.654 II00

1200 38.300 47.452 106.858 67.314 41.088 72.617 1200

1300 38.300 51.282 109,923 70.475 44.918 75.371 1300

1400 38.300 55.112 112.762 73.396 48.748 77.941 1400

7 1408 38.300 55.419 112.980 73.620 49.055 78.140 1408

............................................................................................

t 1408 47.739 64.139 119.173 73.620 57.775 78.140 1408

1500 47.912 68.539 122.200 76.507 62.175 80.750 1500

1600 48.124 73.340 125.299 79.462 66.976 83.439 1600

1700 48.355 78.16_ 128.225 82.244 71.800 85.988 1700

1800 48.600 83.012 130.994 84.876 76.648 88.412 1800

1900 48.858 87.885 133.629 87.374 81.521 90.72_ 1900

2000 49.125 92.784 136.141 89.749 86.420 92.931 2000

2100 49.401 97.710 138.545 92.016 91.346 95.047 2100

2200 49.682 102.664 ]40.849 94.184 96.300 97.076 2200

2300 49.969 107.646 143.064 96.261 101.282 99,028 2_00

2400 50.260 112.658 145.197 98.256 106.294 100.908 2400

2500 50.555 117.699 147.255 100.175 111.335 102.721 2500

2600 50.853 122.769 149.2_3 102.024 116._05 104.472 2600

2700 51.154 127.869 151.168 103.809 121.505 106.166 2700

2800 51.458 133.000 153.034 105.534 126.636 107.807 2800

2900 51.763 138.161 154.845 107.203 131.797 109.398 2900

3000 52,070 143.353 156.605 108.821 136.989 110.942 3000

3100 52.379 148.575 158.318 110.391 142.211 112.443 3100

3200 52,689 ]53.828 159.985 111.914 147.464 113.902 3200

3_00 53.000 159,113 161.611 113,395 152.749 115.323 3300

3400 53.312 164.428 163.198 114.837 158.064 116,709 3400

3500 53.625 169.775 164.748 116.241 163.411 118.059 3500

3600 53.939 175.153 166.263 117.609 168.789 119.377 3600

5700 54.254 180.563 167.745 118.944 174.199 120.66_ 3700

3800 56.569 186.004 169.196 120.248 179,640 121.922 3800

3900 54.885 191.477 170.618 121.521 185,113 123.153 3900

_000 55.201 196.981 172.011 122.766 190.617 124.357 4000

78 NASA/TP-3287/REV 1
TK

0

100

150

200

25O

298.15

30O

350

40O

450

50O

55O

600

7O0

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

C°

J/m_l-K 0 000

13 119

18 838

21 876

23 703

24 896

24 928

25.681

26.234

26.610

26.945

27.217

27.689

28.033

28.660

29.372

30.083

30.878

51.798

32.740

33.807

34.811

35.857

37.028

38.Z00

39.539

40.920

TABLE Iit 48.- SELECTED THERMODYNAMIC FUNCTIONS FOR V(cr,_)

HO(T).HO(_ soco .{oO(l_.HO_)}_ HO(T) .G°m_T

_/mol J/moI-K _moI-K k_mol J/m_-KK

0.000 0.000 0.000 -4.640 INFINITEO

0.489 7.185 2.295 -6,151 48.695 100

1.299 15,676 5,016 -3.341 35.949 150

2.325 19.558 7.935 -2.315 31.133 200

3.469 24.655 10.779 -1.171 29.339 250

4.640 28,.936 13.373 0,000 28.936 298.15

4.686 29.090 13,670 0.066 28.937 300

5.952 32.992 15.986 1.512 29.243 350

7.25I 36.459 18.332 2.611 29.951 400

8.572 39.571 20.522 3.932 30.833 650

9,911 62,392 22.570 5.271 31.850 500

11.265 44.973 24.491 6.625 32.928 550

12.653 47.353 26.298 7.995 34.031 600

15.608 51.630 29.619 10.768 36.247 700

18.242 55.413 32.610 13.602 38.610 800

21.144 58.830 35.337 16.506 40.492 900

24.116 61.961 37.865 19.676 42.485 I000

27.163 66.864 40.170 22.523 44.389 1100

30.296 67.590 62.343 25.656 46.210 1200

33.522 70.172 44.386 28.882 67.955 1300

36.850 72.638 66,317 32.210 49.631 1400

40.280 75.004 48.151 35.660 51.246 1500

43.813 77.285 69.900 39.173 52.800 1600

47.457 79.692 51.576 62.817 54.306 1700

51.Z17 81.641 53.187 66.577 55.765 1800

55.104 85.742 54.760 50.464 57.182 1900

59.125 85.805 56.262 54.485 58.562 2000

2100 42.468 63.292 87.837 57.698 58.652 59.907 2100

cr 2190 64.161 67.187 89.653 58.976 62.547 61.093 2190 @ 2190 46.206 90.032 100.085 58.974 85.392 61.093 2190

2200 46.204 90.494 100.295 59.162 85.856 61.271 2200

2500 46.206

2600 66.204

2500 46.204

2600 46.204

2700 46.204

2800 46.204

2900 46.204

3000 46.204

3100 46.204

3200 66.206

3300 46.206

3600 66.204

3500 46.204

3600 46.204

3700 46.204

3800 46.204

3900 46.204

4000 46.206

_IO0 46.204

4200 46.206

4300 46.204

6400 661204

4500 66.206

4600 46.204

6700 46,204

4800 46.204

4900 46.206

5000 46.204

5100 66.204

5200 46,206

5300 46.204

5600 46.206

5500 46.206

5600 46.206

5700 46.204

5800 46.204

5900 46.206

6000 66.204

95.116 102.369 60.995 90.476 63.012

99.735 106.515 62.759 95.095 64.693

104.355 I06.202 64.459 99.715 66.315

108.975 108.014 66.100 104.335 67.885

113,596 109.757 67.685 108.956 69.403

118.216 111.438 69.218 113.576 70.875

122.837 113.059 70.702 118.197 72.502

127.657 114.626 72.140 122.817 73.686

132.077 116.161 73.535 127.437 75.032

136.698 117.607 76.889 132.058 76.539

161.318 119.029 76.205 156.678 77.612

145.939 120.409 77.485 161.299 78.850

150.559 121.748 78.731 145.919 80.057

155.179 123.049 79.944 150.539 81.233

159.800 124.315 81.126 155.160 82.380

164.620 125,5_8 82.279 159.780 83,500

169.041 126,768 83.404 164.401 84.594

173.661 127,918 84.502 169.021 85.662

178.281 129.058 85.575 173.641 86.707

182.902 130.172 86.624 178.262 87.729

187.522 131.259 87.649 182.882 88.728

192.143 132.321 88.652 187.503 89.707

196.763 133.360 89.634 192.123 90.666

201.383 136.375 90.596 196.743 91.605

206.004 135.369 91.538 201.366 92.525

210.626 136.342 92.461 205.984 93,628

215.245 137.294 93.367 210.605 94.316

219.865 138.228 9_.255 215.225 95,183

224,485 139.143 95.126 219,845 96.036

229.106 160.040 95.981 22_.466 96.873

233.726 160.920 96.821 229.086 97.696

238.3_7 141.784 97.645 233.707 98.505

242.967 142.631 98.456 238.327 99.299

247.587 143.464 99.252 262.947 100,080

252.208 144.282 100.035 247.568 100.849

256.828 145.085 100.805 252.188 101.605

261,449 145.875 101.562 256.809 102.348

266.069 146.652 102.307 261.629 103.080

2300

2600

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

6000

4100

4200

6300

6400

4500

4600

6700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV1 79
TABLE Ut49.. SELECTED THERMODYNAMIC FUNCTIONS FOR W(cr.l)

T C ° H°(T)-H°(0)

K J/m_-K kNm_

0 0. 000 0. 000

I00 16.033 0.652

150 20,531 1.580

200 22.489 2.660

250 23.686 3.817

298.15 24.295 4.973

300 24.313 5.018

350 24.644 6.242

400 24.928 7.482

650 25.144 8.733

500 25.359 9.996

550 25.574 11.269

600 25.790 12.553

/00 26.229 15.154

800 26.669 17.799

900 27.112 20.488

I000 27.564 23.222

Ii00 28.017 26.001

1200 28.672 28,825

]300 28.930 31.695

1600 29.393 34.612

1500 29.862 37.574

1600 30.334 60,584

1700 30.807 43.641

1800 31.284 46.746

1900 31.765 49.898

2000 32.256 53.099

2100 32.744 56.369

2200 33.238 59.668

2300 33.736 62.997

2600 36.233 66.395

2500 34,736 69.863

2600 35.246 73.339

2700 36.192 76.908

2800 37.647 80.586

2900 39.120 84.413

3000 41.003 88.615

3100 43.430 92,635

3200 46.024 97.105

3300 68.953 101.850

3600 52.300 106.906

3500 56.48_ 112.536

3600 61.714 118.243

cr 3680 66.149 123.356

S°(T)

JtmoI-K

0.000

9.612

17.072

23.273

28 431

32 660

32 810

36 583

39 893

42 842

45 502

47.929

50.163

54.172

57.703

60.870

63,750

66.398

68,855

71.152

73.313

75.357

77,299

79.152

80,927

82.631

84.273

85.858

87.393

88.881

90.328

91.735

93.106

94.453

95.791

97.133

98.490

99.873

101.292

102.752

104.261

105.835

107.499

108.903

-{G°('r)-H°(o)}_ H°(T) -G°(T)fl T

NmoI-K _Irnol J/m_-K K

0,000 -4.973 INFINITE 0

3.092 -6.321 52.822 100

6,539 -3,393 39.692 150

9,973 -2.313 34.838 200

13.163 -1.156 33.055 250

15.980 0,000 32.660 298.15

16.083 0,045 32.660 300

18.769 1,269 32.957 350

21.188 2.509 33.620 400

23.635 3.760 34.686 650

25.510 5.023 35.656 500

27.440 6.296 36.482 550

29,241 7.580 37.530 600

32.523 10.181 39.628 700

35.454 12.826 41.670 800

38.106 15.515 43,631 900

60.528 18.269 65.501 1000

42.761 21.028 67.282 ii00

44.836 23.852 48.978 1200

46,771 26.722 50.597 1300

48.590 29.639 52.142 1600

50.308 32.601 53.623 1500

51,934 35.611 55.042 1600

53.481 38.668 56,406 1700

54.957 41.773 57.720 1800

56.369 44.925 58.986 1900

57.723 48.126 60.210 2000

59.025 51.376 61.393 2100

60.280 54.675 62.561 2200

61.491 58.024 63.653 2300

62,663 61.422 64.735 2600

63.798 64.870 65.787 2500

64,899 68.566 66.811 2600

65.969 71.935 67.810 2700

67.010 75.613 68.786 2800

68.025 79.640 69.740 2900

69.018 83.642 70.676 3000

69.991 87.662 71.595 3100

70.947 92.132 72.501 3200

71.888 96.877 73,395 3300

72.818 101.933 74.281 3600

73.739 107.363 75.160 3500

74.654 113.270 76.035 3600

75.383 118.383 76.734 3680

{ 3680 35.564 158.753 118.522 75.383 153,780 76.736 3680

3700 35.564 159.464 118.715 75.617 154.691 76,961 3700

3800 35.564 163,021 119.663 76.763 158.048 78.072 3800

3900 35.564 166.577 120.587 77.875 161.604 79.150 3900

6000 35.564 170.133 121.488 78.956 165.160 80.197 4000

6100 35.566 173.690 122.366 80.002 168.717 81.215 4100

4200 35.564 177.246 123.223 81.021 172.273 82.205 4200

6300 35.566 180.803 12_.060 82.012 175.830 83.169 4300

6600 35.564 184.359 126.877 82.977 179.386 84.108 4600

6500 35.564 187.915 125.676 83.917 182.962 85.023 4500

6600 35.564 191.472 126.458 84.834 186.499 85.915 4600

_700 35.564 195.028 127.225 85.728 190.055 86.786 4700

6800 35.564 198.585 127.972 86.600 193.612 87.636 4800

6900 35.564 202.161 128.705 87.452 197.168 88.667 6900

5000 35.566 205.697 129.423 88.284 200.724 89.279 5000

5100 35.566 209.254 130.128 89.098 204.281 90.073 5100

5200 35,564 212.810 130.818 89.893 207.837 90.850 5200

5300 35.566 216.367 131.496 90.672 211.394 91.610 5300

5600 35.564 219.923 132.161 91.434 216.950 92.355 5600

5500 35.564 223.479 132.813 92.180 218.506 93.085 5500

5600 35.564 227.036 133.654 92.912 222.063 95.800 5600

5700 35.564 230.592 134.083 93.629 225.619 94.501 570_

5800 35,566 234.169 134.702 94.331 229.176 95.189 5800

5900 35.566 237.705 135.310 95.021 232.732 95.864 5900

6000 35.564 241.261 135.908 95.697 236.288 96.526 6000

80 NASA/TP-3287/REV 1
TABLE 111.50- SELECTED THERMODYNAMIC FUNCTIONS FOR Xe

TC° HO_'HO(O) S°CI) "{G°JT)'H°(O)}K H°(T) "G°{T)_

K J/m_-K kJ/mol J/moI-K JlmoI-K kJ/mol J/moI-K 0 0.000 0.000 0.000 0.000 -6.197 INFINITE

i00 20.786 2.079 146.978 126.192 -4.119 188,166

200 20.786 4,157 161.386 140.600 -2.040 171.587

298.15 20.786 6.197 169.686 148.900 0.000 "169,686

300 20.786 6.236 169,815 149.028 0.038 169.686

400 20.786 8.315 175.794 155,008 2.117 170.502

500 20.786 10.393 180.633 159,646 4.196 172.041

600 20.786 12,472 184.222 163.436 6.274 173.765

700 20.786 14.550 187.427 166.640 8.353 175.494

800 20,786 16.629 190.202 169.416 10.432 177.163

900 20.786 18.708 192.651 171.86_ 12.510 178.750

1000 20.786 20.786 194.841 174.054 14.589 180.252

II00 20.786 22.865 196.822 176.036 16.667 181.670

1200 20.786 24.944 198.630 177.844 18.746 183.009

1300 20.786 27.022 200.294 179.508 20.825 184.275

1400 20.786 29.101 201.835 181.048 22.903 185.475

1500 20.786 31.179 203.269 182.482 24.982 186.614

1600 20.786 33.258 20_.610 183.824 27.061 187.697

1700 20.786 35.337 205.870 185.08_ 29.139 188.730

1800 20.786 37.415 207.059 186.272 31.218 189.715

1900 20.786 39.494 208.182 187.396 33.296 190.658

2000 20.786 41.573 209.249 188.462 35.375 191.561

2100 20.786 43.651 210.263 189.476 37.454 192.428

2200 20.786 45,730 211.230 190.443 39.532 193.260

2300 20.786 47.808 212.154 191.367 41.611 19_,062

2400 20.786 49.887 213.038 192,252 43.690 194.83_

2500 20.786 51.966 213.887 193.101 45.768 195.580

2600 20.786 5_.044 214.702 195.916 47.847 196.300

2700 Z0.786 56.123 215.487 194.700 49.926 196,996

2800 20,786 58.202 216.243 195.456 52.004 197.670

2900 20.786 60.280 216.972 196.186 54.083 198.323

3000 20.786 62.359 217.677 196.890 56.161 198.956

3100 20.786 64.437 218.358 197.572 58.240 199.571

3200 20.786 66.516 219.018 198.232 60.319 200.169

3300 20.786 68.595 219.658 198.872 62.397 200.750

3400 20.786 70.673 220,278 199.492 66.476 201.515

3588 20,786 72.752 220.881 200.095 66.555 201.865

3600 20.786 74.831 221.466 200,680 68.633 202.402

3700 20,786 76.909 222,036 201.250 70.712 202.925

3800 20.786 78.988 222.590 201.804 72.790 203.435

3900 20.786 81.066 223.130 202.344 74.869 203.933

4000 20.786 83.145 223.657 202.870 76.948 204.420

4100 20.786 85.224 224.170 203.384 79.026 204.895

_200 20.786 87.302 224.671 203.884 81.105 205.360

4300 20.786 89.381 225.160 204,374 83.184 205.815

6600 20.786 91.460 225.638 204.851 85,262 206.260

4500 20.786 93.538 226,105 205.319 87.341 206.696

4600 20.786 95.617 226.562 205.775 89.419 207.123

4700 20.786 97.695 227.009 206.222 91.498 207.541

4800 20.786 99.774 227.646 206.660 93.577 207.951

4900 20.786 101.853 227.875 207.089 95.655 208.353

5000 20.786 103.931 228.295 207.509 97.734 208,748

5100 20,786 106.010 228.706 207,920 99.813 209.135

5200 20.786 108.089 229,110 208.324 101.891 209.516

5300 20.786 110.167 229.506 208.720 103.970 209.889

5_00 20.786 112.246 229.895 209.108 106.048 210.256

5500 20.786 114.325 230.276 209.490 108.127 210.617

5600 20.786 116.403 230.651 209.864 110.206 210.971

5700 20.787 118.882 231,018 210.232 112.284 211.319

5800 20.787 120.561 231.380 210.594 114.363 211.662

5900 20.787 122.639 231.735 210.949 116.442 211.999

6000 20.787 124.718 232.085 211.298 118.528 212.331

6200 20.788 128.875 232.766 211.980 122.678 212.980

6400 20.789 133.033 233.426 212.640 126.836 213.608

6600 20.790 '137.191 234.066 213.280 130.993 214.219

6800 20.793 141.3_9 234.687 213.900 135.152 214.811

7000 20,797 145.508 235.289 214.503 139.311 215.388

7200 20.803 149.668 235.875 215.088 143.471 215.949

7400 20.812 153.830 236.4_6 215.658 147.632 216.495

7600 20.824 157.993 237.001 216.212 151,796 217.028

7800 20.841 162.159 237.542 216.752 155.962 217.547

8000 20.864 166.330 238.070 217.279 160.132 218.053

TK0

100

200

298.15

300

400

500

600

700

800

900

i000

ii00

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

_300

4_00

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6660

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV1 81
TABLE IILSO,- Co(_luded,

T C° H°(T)-Ho(O) S°(T) .{GO('r).Ho(o)}_

K Nm_-K kJ/mol J/moI-K d/mokK

8200 20.895 170.505 238.585 217.792

8q00 20.936 174.688 239.089 218.293

8600 20.989 178.881 239.582 218.782

8800 21.057 183.085 240.066 219.261

9000 21.1_4 187.305 240.5q0 219.728

9200 21.252 191.544 2_1.006 220.186

9qO0 21.385 195.807 241.464 220.634

9600 21.548 200.100 241,916 221.672

9800 21.745 204.429 2_2.362 221.502

10000 21.982 208.801 242.804 221.924

10500 22.782 219.978 243.895 222.944

11000 23.952 231.644 244.980 223.921

11500 25.588 244.008 246.079 224.861

12000 27.788 257.327 247.212 225.768

12500 30.639 271.905 248.402 226.649

13000 34.207 288.085 249.671 227.510

13500 38.530 306,238 251.040 228.356

14000 43.600 326.740 252.531 229.192

1_500 49.361 349,953 254,159 230.025

15000 55.695 376.197 255.938 230.858

15500 62.430 405,716 257.873 231.698

16000 69.338 438.656 259.965 232.549

16500 76.158 475.039 262.203 233,413

17000 82.611 514.752 264.574 234.294

17500 88.430 557.54_ 267.054 235.195

18000 93.379 603.036 269.617 236.115

18500 97.279 650.747 272.231 237.056

19000 100.020 700.122 274.865 238.016

19500 101.567 750.568 277.485 238.994

20000 101.951 801.494 280.064 239.989

H°_

_/mol

16_.308

168.491

172.683

176.888

181.107

185.346

189.610

193.902

198.231

202.603

213.781

225.447

237,810

251.129

265.707

281.888

300.040

320.542

343.756

369.999

399.5L8

432.458

468.8ql

508.555

551.347

596.839

644.550

693.924

744.371

795.297

.G°CI")_

J/moI-K

218.5_8

219.031

219.503

219.965

220,417

220.859

221,293

221.718

222.135

222.544

223,534

224.485

225.399

226.285

227.145

227.987

228.815

229.635

230.452

231.272

232.098

232.936

233.788

234.659

235.549

236.459

237.391

238.342

239.312

240.299

T

K

8200

8q00

8600

8800

9000

9200

9400

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

82 NASAFFP-3287/REV l
TABLE 111.51.SELECTED THERMODYNAMIC FUNCTIONS FOR Zn(cr,_)

T C° HO(T).HO(o) SOre .{GOcr).Ho(O)}K HO(T) .oO(T)K T

K J/m_-K _/mol J/moJ-K J/moI-K kJ/mol J/mo_K K

0 0.000 0.000 0.000 0,000 -5.657 INFINITE 0

I00 19.460 0.996 16.520 6.560 -4.661 63.130 i00

200 24.050 3.230 31.810 15.660 -2.427 43.945 200

298.15 25.390 5.657 41.630 22.656 0.000 41.630 298,15

300 25,410 5.704 41.787 22.774 0.047 41.630 300

400 26.226 8.288 49.215 28.495 2.631 42.637 400

500 27.220 10.956 55.165 33.253 5.299 44.567 500

600 28.820 13.752 60.258 37.338 8,095 46.766 600

cr 692.73 30.975 16.519 64.543 40.696 10.862 48.863 692.73

;- 692.73- -31.400 23.819 - 757;;; ..... ;;7;9; ...... ;;7;6; ...... ;8_86; ....... 6;;7;3

700 31.400 24.048 75. 0 41.055 18.391 49.137 700

800 31.400 27.188 79.602 45.617 21.531 52.689 800

900 31.400 30.328 83.300 49.603 24.671 55.888 900

I000 31.400 33.468 86.608 53.141 27.811 58.798 i000

i100 31.400 36.608 89.601 56.322 30.951 61.464 II00

1200 31.400 39.748 92.333 59.210 34.091 63.925 1200

1300 31.400 42.888 94.847 61.856 37.231 66.208 1300

1400 31.400 46.028 97.174 64.297 40.371 68.338 1400

1500 31.400 49.168 99.340 66.562 43.511 70.333 1500

1600 31.400 52.308 101,366 68.674 46.651 72.210 1600

1700 31.400 55,448 103.270 70.654 49.791 73.982 1700

1B00 31.400 58.588 105.065 72.516 52.931 75.659 1800

1900 31.400 61.728 106.763 7_.274 56.071 77.252 1900

2000 31.400 64.868 108.373 75.939 59.211 78.768 2000

2100 31.400 68.008 109.905 77,521 62.351 80.214 2100

2200 31.400 71.148 111.366 79.026 65.491 81.598 2200

230O 31.400 74.288 112.762 80.463 68.631 82.922 2300

24D0 31.400 77.428 114.098 81.837 71.771 84.194 2400

2500 31.400 80.568 115.380 83.153 74.911 85.416 2500

2600 31.400 83.708 116.611 84.416 78.051 86.592 2600

2700 31.400 86.848 117.796 85.631 81.191 87.726 2700

2800 31._00 89.988 118.938 86.800 84.331 88.820 2800

2900 31.400 93,128 120.040 87.927 87.471 89.878 2900

3000 31.400 96.268 121.105 89.016 90.611 90.901 3000

3100 31.400 99.408 122.134 90.067 93.751 91.892 3100

3200 31._00 102.548 123.131 91.085 96.891 92.853 3200

3300 3].400 105.688 124.098 92.071 100.031 93.785 3300

3_00 31._00 108.828 125.035 93.027 103.171 94,691 3400

3500 31.400 111.968 125.945 93.954 106.311 95.571 3500

3600 31 _00 115.108 126.830 94.855 109.451 96.427 3600

3700 31._00 118.248 127.690 95.731 112.591 97.260 3700

3800 31,_00 121.388 128.527 96.583 115,731 98.072 3800

390_ 31 _00 124.528 129.343 97.413 118.871 98.863 3900

4000 31._00 127.668 130.138 98.221 122.011 99.635 4000

4100 31.400 130,808 130,913 99.009 125.151 100.389 4100

_200 _l.400 133.948 131.670 99.778 128.291 101.125 4200

4300 31.400 137.088 132.409 100.528 131.431 101.844 4300

4_C0 51 _00 140,228 133.131 101.261 134.571 I02.5_7 4_00

_5_0 _ _00 143.368 133.836 101.977 137.711 103.23_ 4500

_03 _l _oo 146.508 134,527 102.677 140.851 103.907 4600

_7C0 51 _00 I_9.648 135.202 103.362 143.991 10_.566 4700

_8C3 51 _00 152.788 135.863 104.032 147.131 105.211 4800

4903 31_0 155,928 136.510 104.688 150.271 105.843 4900

5000 _._00 159.068 137.145 105.331 153.411 106.463 5000

5100 31._0o 162.208 137.767 105.961 156.551 107.070 5100

5200 31.400 165.348 138.376 106.579 159.691 107.667 5200

5300 31.400 168.4_8 138.974 107.184 162.831 108.252 5300

5_00 31._00 171.628 139.561 107.778 165.971 108.826 5400

5500 _1.400 174.768 140.137 108,362 169.111 109.390 5500

5600 31.400 177.908 140.703 108.934 172.251 109.944 5600

5700 31.400 181.048 141.259 109.496 175.391 110.489 5700

5800 31.400 184.188 141.805 110,049 178.531 111.024 5800

5900 31._00 187.328 142.342 110.591 181.671 111.550 5900

6000 31.400 190.468 142.870 111.125 184.811 112.068 6000

NASA/TP-3287/REV 1 83
TABLE n}52 - SELECTED THERMODYNAMIC FUNCTIONS FOR Zr(,=,_,_

T co H°(l_'H°(0) S°0_ "{G°0_-H°(O)}_ H°0_ -G°('F)_ T

K J/m_K kJ/m_ _mol.K J/m_-K k_rno_ J/moI-K K

0 0.000 0,000 0.000 0.000 -5.497 INFINITE 0

100 18.617 0.886 I_,055 5.195 -4.611 -60.165 100

150 22.260 1.921 22.396 9.589 -3.576 46.236 150

200 25.873 3,079 29.050 13.655 -2.418 41.140 200

250 24.693 4.295 34,474 17.294 -1,202 39.282 250

298.15 25.202 5,497 38.869 20.432 0.000 38.869 298

300 25.218 5.544 39.025 20.545 0.047 38.868 300

350 25.606 6.815 42.943 23.472 1.318 39.177 350

400 25.935 8.103 46.384 26.127 2.606 39.869 400

450 26.246 9.408 49.457 28.550 3,911 40.766 450

500 26.564 10.728 52.238 30.782 5.231 41.776 500

550 26.906 12.065 54.786 32,850 6.568 42.844 550

600 27.281 13.419 57.143 34.778 7.922 43.940 600

700 28.053 16.186 61.406 38.283 10.689 46.136 700

800 28.966 19.035 65.210 41.416 13.538 48.287 800

900 30.003 21.983 68.680 44.254 16.486 50.362 900

I000 31.128 25.039 71.899 46.860 19.542 52.357 I000

i100 32.306 28.210 74.921 49.276 22.713 54.273 ii00

1135 32.724 29.348 75.939 50.082 23.851 54.925 1t35

.15

1135 28.329 33.365 79.478 50.082 27.868 54.925 1135

1200 28.511 35.212 81.060 51.717 29.715 56.297 1200

1300 28.879 38.081 83.356 54.063 32.584 58.291 i300

1400 29.353 40.991 85.513 56.234 35.494 60.160 1400

1500 29.934 43.955 87.558 58.255 38.458 61.919 1500

1600 30.621 46,982 89.511 60.IQ7 41.485 63.583 1600

1700 31.414 50.083 91.390 61.929 44.586 65.163 1700

1800 32.314 53.268 93.211 63.618 47.771 66.672 1800

1900 33.320 56.549 94.985 65.222 51,052 68.116 1900

2000 34.433 59.936 96.722 66.754 54.439 69.502 2000

2100 35,652 63.439 98.431 68.222 57.942 70.840 2100

2125 35.973 64,334 98.854 68.580 58.837 71.166 2125

Q 2125 41.840 85.254 108.699 68.580 79.757 71.166 2125

2200 41.840 88.392 110.150 69.972 82.895 72.471 2200

2300 41.840 92.576 I12.010 71.760 87.079 74.150 2300

2400 41.840 96.760 113.791 73.474 91.263 75.765 2400

2500 41.840 100.944 115.499 75.121 95.447 77.320 2500

2600 41.840 105.128 117.140 76.706 99.631 78.820 2600

2700 41.840 109.312 118.719 78.233 103.815 80.269 2700

2800 41.840 113.496 120.241 79.706 107.999 81.669 2800

2900 41.840 117.680 121.709 81.129 112.183 83.025 2900

3000 41.840 121.864 123.127 82.506 116.367 84.338 3000

3100 41.840 126.048 124.499 83.838 120.551 85.612 3100

3200 41.840 130.232 125.827 85.130 124,735 86.848 3200

3300 41.840 134.416 127.115 86.383 128.919 88.049 3300

3400 41.840 138.600 128.364 87.599 133.103 89.216 3400

3500 41.840 142,784 129.577 88.781 137.287 90.352 3500

3600 41.840 146,968 130,756 89.931 141.471 91.458 3600

3700 41.840 151.152 131.902 91.050 145.655 92.536 3700

3800 41.840 155.336 133.018 92.140 149.839 93.586 5800

3900 41.840 159.520 134.104 93.202 154.023 94.611 5900

4000 41.840 163,704 135.164 94.258 158,207 95.612 4000

4100 41,840 167.888 136.197 95.249 ]62,391 96.589 4100

4200 41.840 172.072 137.205 96.236 166.575 97.544 4200

4300 41.840 176.256 138.190 97.200 170.759 98.478 4300

4400 41.840 180.440 139.152 98.142 174.943 99.392 4400

4500 41.840 184,624 140,092 99.064 179.127 100,286 4500

4600 41.840 188.808 141.011 99.966 183.311 101.161 4600

4700 41.840 192.992 141.911 100.849 187.495 102.019 4700

4800 41.840 197.176 142.792 101.714 191.679 102.859 4800

4900 41.840 201.360 143.655 102.561 195.863 103.683 4900

5000 41.840 205.544 144.500 I03,391 200.047 104.491 5000

5100 41.840 209.728 145.529 104.206 204.231 105.283 5100

5200 41.840 213.912 146.141 105.004 208.415 106.061 5200

5300 41.840 218.096 146.938 105.788 212.599 106.825 5300

5400 41.840 222.280 147.720 106.557 216.783 107.575 5400

5500 41.840 226.464 148.488 107.313 220.967 108.312 5500

5600 41.840 230.648 149.242 108.055 225.151 109.036 5600

5700 41.840 234.832 149.982 108.784 229.335 109.748 5700

5800 41.840 239.016 150.710 109.500 233.519 110.448 5800

5900 41.840 243.200 151.425 110.205 237.703 111.157 5900

6000 41.840 247.384 152.128 110.898 241.887 111,814 6000

84 NASA/TP-3287/REV 1
TABLE IV. - ENTHALPY AND GIBBS ENERGY INPUT FOR PAC91 (EFdata)

-FDA

EFDA

AG1S

100.00

298.15

400.00

600.00

800.00

1000.00

1209.00

1235.08

1400.00

1600.00

1800.00

2000.00

2200 O0

2400 O0

2600 O0

2800 O0

3000 O0

5200 O0

5400 O0

5600 00

3800 O0

4000 O0

6200 O0

4600 O0

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600 O0

5800.00

6000.00

ALIS

100.00

298.15

400.00

600.00

800.00

953.61

1000.00

1200.00

1400.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

CODA89 HO/R

1.253231

2.517494

2.509769

2.750568

2,879504

5.000658

3.108922

4.198271

4.176926

4.156944

4.141403

4,128970

4.118798

4.110321

4.103168

4.097000

_.091671

_.087009

_.082895

4.079258

_.075967

6.075022

4.070358

4.067936

6.065724

6.063697

4 061832

4 060111

4 058517

4 057037

4 055659

6 054573

CODA89 HO/R

0.583318

1,831405

2.151214

2.699245

2.758581

2.922508

6.268909

4.193861

6.140256

4.100052

4.068783

6,043767

4.023300

4.006243

5.991811

3.979461

3.968720

3.959339

5 951062

5 943704

5 937121

3 931196

5 925836

5 920963

3.916515

3.912454

3.908682

5.905218

3.902011

3.899033

5.896261

5.895673

-690.9607MP

0.805820

2.800066

5.510550

4.573892

5.58059_

6.056555

6.593595

6.683176

7.208007

7.764394

8.253078

8.688752

9.081792

9,459800

9.768511

10.072356

I0 354834

i0 618752

i0 866400

11 099666

Ii 320130

ii 529123

II 72778i

Ii 917076

12 097855

12 270867

12 436697

12 595971

12 769171

12 896742

13 039085

13 176556

-566.0336MP

0.256539

1,572285

2.155148

5.095_32

5.851069

4.289542

4.583688

5.554955

5.997202

6.567512

7.028351

7.455699

7.840120

8.189440

8.509526

8.80_887

9.079066

9.334895

9.574675

9.800299

10.015365

10.215139

10.406811

10.589327

10.763521

I0.950119

11.089755

11.262988

11.390511

11.532166

11.668957

11.800982

200

300

50O

700

900

ii00

1235

1300

1500

1700

1900

2100

2500

2500

2700

29OO

3100

3500

3500

5700

3900

6100

6300

6500

4700

4900

5100

5300

5500

5700

5900

1255.0800NT

.00 1.989293

.00 2.522045

.00 2.635152

.00 2.809890

.00 2.9_22fi6

.00 3.055994

.08 5.127095

.00 6.189222

.00 4.166269

.o0 4.148717

.DO 6.134859

.00 4.123662

.00 6.114375

00 6.106591

OD 6.099960

O0 6.094244

O0 6.089265

O0 6.084890

OO 6.081015

00 6.077558

O0 6.074457

O0 6.071657

O0 6.069119

O0 6.066806

00 6.064689

00 6.062746

00 4.060955

00 6.059299

00 4.057763

00 4.056336

O0 6.055005

200.

500.00

500.00

700.00

900.00

953.61

Ii00.00

1500.00

1500.00

1700.00

1900.00

2100.00

2500.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

6100.00

6300.00

4500.00

4700.00

6900.00

5100.00

5300.00

5500.00

5700.00

5900.00

933.6100NT

O0 1.373502

1 838152

2 338322

2 634980

2 880506

6 300929

4 227974

6 164997

6 118814

4 083498

4 055617

4 033046

4 014401

3 998739

5 985397

5 975896

3 965878

3 955075

3 947278

3 940326

3.956083

3 928651

3 923542

3 918688

5 914450

3 910520

5 906916

3.905585

3.900495

5.897623

5.894945

63 0000

1 938779

2 814597

6 084546

5 000793

5 723448

6 525196

6 685176

6 898013

7 495813

8 016155

8 476814

8 890074

9 264781

9.607515

9 923304

10 216076

10 488959

i0 746483

i0 984725

II 211610

Ii 425985

Ii 629680

II 823544

12 008483

12 185282

12 354628

12 517123

12 673301

12 825634

12 968544

13.108408

63.0000

0.928497

1.583577

2.654275

3.490937

6.182928

4.289342

4.988577

5.689470

6.282102

6.795369

7.267980

7.652751

8.018764

8.352829

8.660056

8.9_4633

9.209119

9.456664

9.689151

9.908306

10.115574

10.312177

10.499159

10.677416

I0 847728

Ii 01077I

II 167148

Ii 317360

ii 461896

Ii 601162

II 735530

NASA/TP-3287/REV 1 85
TABLE IV.- Continued.

EFDA ARIG

100 O0

298 15

400 00

600 O0

800 O0

I000 DO

1200 O0

1400 O0

1600 00

1800.00

2000.00

2200 O0

2400 O0

2600 O0

2800 00

3000 O0

3200 OO

3400 O0

3600 00

3800 O0

_000 00

4200 O0

4400 O0

4600.00

4800.00

5000.00

5200.00

5400 O0

5600 O0

5800 O0

6000 00

6400 O0

6800 O0

7200 O0

7600.00

8000.00

8400.00

8800.00

9200.00

9600.00

I0000.00

11000.00

12000.00

13000.00

14000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

L 6/88 HO/R

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2.500003

2.500007

2.500017

2 500038

2 500080

2 500158

2 500294

2 500498

2 501721

2 504698

2 511003

2 523342

2 541827

2 572537

2 616912

2 660719

2.729779

2.777339

-745.3750MP

13.392600

16.123667

16.858336

17.871999

18.591204

19.149063

19.604867

19.990244

20.324072

20.618530

20.881951

21.120207

21.337735

21.537842

21.723112

21.895594

22.056940

22.208502

22.351398

22 486566

22 614799

22 736774

22 853074

22 964204

23 070603

23 172658

23 270710

23 365060

23 455980

23.543708

23.628462

23.789808

23.941370

24.084266

24.219434

24.347668

24.469665

24.585947

24.697082

24.803490

24.905560

25.143928

25.361708

25.562393

25.748881

25.923377

26.088276

26.245363

26.394505

26.539732

26.676535

200

300

500

700 O0

9O0 O0

Ii00 O0

1300 O0

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700 00

2900 O0

3100 O0

3300 O0

3500 O0

3700 O0

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300 O0

550O O0

5700 O0

5900 O0

6200 O0

6600 O0

7000.00

7400.00

7800.00

8200.00

8600.00

9000.00

94O0.00

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

O.O000NT

O0 2.500000

O0 2.500000

O0 2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.5000O0

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2.500004

2.500011

2.500026

2.500055

2.500113

2.500216

2.500396

2.500962

2.502924

2.507255

2.516279

2.531887

2.555305

2.593485

2.643872

2.695113

2.754765

I01.0000

15.125468

16,139131

17.416195

18.257376

18.885662

19.387339

19.804974

20.162726

20.475634

20.755698

21 003906

21 231336

21 439790

21 632193

21 810840

21 977568

22 133869

22 280971

22.419895

22.551504

22.676531

22.795601

22.909257

23.017969

23.122151

23.222164

23.318330

23.410933

23.500229

23.586444

23.710436

23.866737

24.013839

24.152763

24.284373

24.409400

24.528472

24.642131

24.750851

24.855045

25.027569

25.255156

25.463992

25.657253

25.837513

26.006886

26.167748

26.321398

26.46786_

26.608987

86 NASAFI'P-3287/REV 1
TABLE IV.- Continued.

EFDA B 1S

100 O0

130 O0

160 O0

200 O0

250 00

260 00

298.15

310.00

350.00

450.00

550.00

650.00

750.00

850.00

950.00

1050.00

1150.00

1250.00

1350.00

1450.00

1550.00

1700.00

1800.00

1900.00

2000.00

2100.00

2200.00

2300.00

2350 O0

2500 O0

2700 O0

2900 O0

3100 00

3300 O0

3500 O0

3700 O0

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

J6/83

0

0

0

0

0

0

0

HO/R

.028865

.067537

.121775

214685

294404

578856

489719

0 524152

0 639845

0 915401

I 157669

1 565511

i 538194

1 687765

1.816862

1,929959

2.029872

2.119187

2.199724

2.272969

2.340176

2.431539

2.487151

2.539315

2.588367

2.634809

2.678887

2.720911

5.310787

5.221258

5,117559

5 027791

4 949781

4 881226

4 820506

4 766350

4 717749

4,673889

4.634109

4.597866

4.564707

4.534254

4.506190

4.480245

4.456186

4.435815

4.412961

-146.0098MP

0.008178

0.020021

0.039650

0.076252

0.111592

0.152625

0.211946

0.251876

0.302563

0.496829

0.704497

0.915156

1.122816

1.324679

1.519715

1.707176

1 887376

2 060374

2 226514

2 386356

2 540207

2 760589

2 901140

3 037081

3 168557

3.296028

3.419608

3.539590

3.598349

3.924158

4.321942

4.684385

5.017065

5.324362

5.609771

5.876128

6.125756

6.360586

6.582240

6.792087

6.991300

7.180884

7.361714

7.534548

7.700055

7.858818

8.011362

2350.0000NT

ii0.00

150.00

180.00

210.00

250.00

290.00

3O0.O0

330.00

400.00

500.00

600.00

700.00

800.00

900.00

i000.00

1100.00

1200.00

1300.00

1400.00

1500.00

1600.00

1750.D0

1850.00

1950.00

2050.00

2150.00

2250.00

2350.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000 O0

5200 O0

5400 O0

5600 O0

5800 O0

6000 O0

0.040455

0.101830

0.165708

0.240543

0.350231

0.465742

0.495118

0.582406

0,781164

1.041512

1.264857

1.454428

1.615850

1.754496

1.875276

1.981421

2.075689

2 160449

2 257225

2 307292

2 371757

2 459796

2 513613

2 564192

2 611890

2 657109

2 700126

2 741170

5 279701

5.167310

5.070976

4.987486

4.914432

4.849973

4.792676

4.741410

4.69527I

4.653526

4.615576

4.580926

4.549163

4.519942

4.492968

4.467992

4.444801

4.423208

4.403056

94.0000

0.010781

0.032513

0.056554

0.087197

0.138433

0.198880

0.214966

0.266351

0.396776

0.599675

0.809950

1.019560

1.224606

1.423201

1.614286

1.798116

1.974700

2.144314

2 307240

2 464006

2 615067

2 831556

2 969693

3 103370

3 232832

3 358279

3 480054

3 598349

3.709831

4.127875

4.507200

4.854148

5.173650

5.469612

5.745176

6.002904

6.244913

6.472969

6.688562

6.892956

7.087238

7.272344

7.449086

7.618178

7.780244

7.935837

8.085447

NASA/TP-3287/REVI 87
TABLE IV. - Continued.

EFDA BAIS

20.00

40.00

60.00

80 O0

I00 O0

160 O0

180 O0

220 O0

260 O0

298 15

550 O0

650 O0

600 O0

800 O0

I000 O0

II00.o0

1500.00

1500.00

1700.00

lgO0.O0

2100.00

2300.00

2500 O0

2700 O0

2900 00

3100 O0

3300 O0

3500 00

3700 O0

3900 O0

4100 O0

4300 O0

4500 O0

4700 O0

6900 O0

5100.00

5300.00

5500.00

5700.00

5900.00

SRD 92 HO/R

0.352680

1. 056892

1.525311

I .826668

2.055957

2.307864

2.481562

2.606863

2,705750

2.786235

2.882166

5.039079

3 240071

3 479955

3 705387

6 666188

6 686754

6 703302

6 715957

6 725947

4 754055

4 760716

4 746328

4.75Ii09

4.755230

6.758819

4.761976

6.766768

6.767260

6.769496

6.771516

6.773566

4.775012

4.776538

6.777939

6.779230

6.780626

4.781531

4.782560

4.783520

-830.7156MP

0.136931

0.609528

1.133597

1.616629

2.068O37

2.780217

3.382697

5.895205

6,336992

6.712966

5.167369

5.911167

6.815626

7.779087

8.580015

9.023870

9.806979

10.476870

11.066358

11.591660

12,064860

12.695832

i2.891358

13.256827

13.596685

13.913759

14.211362

16.691661

16.756489

15.007516

15.246090

15.673392

15.690437

15.898113

16.097193

16.288362

16.Q72225

16.669318

16.820126

16.985073

i

30.00

50.00

70 O0

90 O0

120 O0

160 O0

200 00

260 O0

280 O0

300 00

400 O0

500 O0

700,00

900 O0

I000 O0

1200 O0

1600.00

1600.00

1800.00

2000.00

2200.00

2600.00

2600.00

2800.00

5000.00

3200.00

3400.00

3600.00

3800.00

4000.00

6200.00

4600.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

O00.O000NT

0.752361

1 317702

1 691292

1 960138

2 189668

2 602851

2 568536

2.658750

2.769155

2.789912

2.966055

3.109288

3.362596

5.593876

6.6_9520

6.676411

6.695619

6.710025

6.721230

4.750193

6.737527

6.745639

6.768810

6.755243

6.757086

4.760646

4.763612

6.766048

6.768407

6.770530

6.772451

6.776197

6.775791

6.777255

6.778597

6.779839

6.780988

6.782055

4.783068

4.783976

80.0000

0.352590

0.874281

1.381651

1.838528

2.453660

5.094803

5.647509

6.122296

6.539118

6.730192

5.557645

6.255015

7.522368

8.195572

8.580013

9.630267

10.152637

10 780655

II 336067

11 833979

i2 285169

12 697658

13 077561

13 629652

13 757726

14 06_851

16 3535_2

16 625887

14 883639

I5 I28281

i5 361083

15 583138

I5.795396

i5.998683

16 I93727

16 381172

16 561586

16 755479

16 903305

17 065676

88 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA BEIS

40 O0

60 O0

80 00

i00 00

140 O0

180 O0

220 O0

260 00

298 15

350 O0

450 00

600 O0

800 O0

I000 O0

1200.00

Iq00.00

1543.00

1563.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800 O0

3000 DO

3200 O0

3400 O0

3600 O0

3800 O0

_000 O0

4200 O0

4400 O0

4600 O0

4800 O0

5000.00

5200.00

5400.00

5600.00

5800.00

6000,00

SRD 92 HO/R

0.002115

0,009198

0,022746

0.048798

0.146577

0.291662

0.457027

0.626487

0.783417

0.979565

1.293960

1.640556

1.965326

2.206761

2.403164

2 573356

2 684823

3 212197

3 821266

3 790637

3 76613_

3 746087

3 729380

3 71524_

3 703127

3 692626

3 683437

3.675330

3.668123

3.661675

3.655872

3.650621

3.645848

3.641490

3.637495

3.635819

3.630426

3.627285

3.624368

3.621652

3.619Ii7

-233.5758MP

0.000882

0,002935

0.007207

0.014801

0.044973

0.098615

0.173004

0.263132

0.359491

0.500696

0.786435

1.209051

1.728209

2.193793

2.614002

2.997490

3.253153

_.29_488

3.383969

3.832210

4.230280

4.588260

4.913475

5,211411

5.486286

5.741409

5.979426

6.202485

6.412353

6.610502

6.798171

6.976413

7.146128

7.308095

7. 462989

7.611404

7.753858

7.890811

8.022674

8.149810

8.272546

1563.0000NT

50.00

70,00

90.00

120 O0

160 O0

200 00

240 O0

280 00

300 O0

400 O0

500 00

700 O0

900 O0

1100 O0

1300 O0

1500 O0

1543 O0

1563 O0

1700 O0

1900 O0

2100 00

2300 O0

2500 OD

2700 O0

2900 00

3100 00

3300 O0

3500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

0.005147

0,014765

0.033900

0.089739

0.215170

0.373037

0.541938

0.709699

0.790769

1.146974

1.423344

1.817087

2.093405

2.309134

2.490766

2.652004

3.207065

3.827791

3.805051

3.777741

3.755633

3.737370

3.722029

3.708961

3.697695

3.687883

3.679261

3.671623

3.664812

3.658699

3.653182

3.648179

3.643620

3.639450

3.635619

3.632089

3.628826

3.625800

3.622986

3.620363

81,0000

0.001655

0.004746

0.010496

0.027050

0.068916

0,133524

0.216409

0,312616

0.364360

0.642667

0.929605

1.475631

1.967254

2.408997

2.809854

3.177735

3.253153

3.294488

3.615135

4,036807

q.413772

4.754585

5.065565

5.351507

5.616138

5.862411

6.092707

6.308969

6.512810

6.705577

6.888411

7.062285

7.228035

7.386387

7.537973

7.683346

7.822995

7.957355

8.086811

8.211709

NASA/TP-3287/REV 1 89
TABLE IV. - Continued.

EFDA BR2S

5.00

15.00

25.00

35.00

65.00

60.00

80.00

i00,00

120.00

140.00

160.00

180.00

200.00

220.00

240.00

260.00

265.90

280.00

298 15

332 50

360 O0

400 00

600 00

800 O0

1000 00

1200 00

1400 O0

1600 O0

1800 00

2000 O0

2200 O0

2400 O0

2600 O0

2800 O0

3000 O0

3200 00

3600 O0

3600 00

3800 O0

qOOO 0o

q2oo 00

_400 00

46O0 00

_800 00

5000 O0

5200 o0

5_00 O0

5600 O0

5800 00

6000 O0

TPISS9 HO/R

0.009862

0.240545

0.755306

1.305807

1.788039

2.365343

2.931622

3.559188

3.698356

3.980133

6.221536

4.434684

6.626851

6.806853

6.973236

5.139301

9.970672

9.935729

9.891200

9.806122

9.768880

9.679662

9.672007

9.368180

9.505883

9.266352

9.234687

9.212638

9.195134

9 181290

9 169966

9 160525

9 152538

9 165692

9 139759

9.134568

9.129987

9.125916

9.122273

9.118996

9.116027

9.113330

9.110868

9.108611

9.106536

9.104618

9.102843

9.101195

9.099660

9.098228

-2949.0613MP

0.003688

0.087558

0.521727

0.666123

1.051816

1.649646

2.613852

3 115397

3 760173

6 352669

6 901071

5 610996

5 888621

6 337716

6 763557

7 167979

7 283822

7 797968

8 415351

9.688962

I0 265784

11 289221

15 169051

17 878528

19 961568

21 654330

23.080091

24.311693

25.395723

26.565785

27.238307

28.035782

28.768691

29.466710

30.077691

30.667188

31.220827

31.762565

32.235879

32.703706

33.148550

33.572566

33.977613

36.365319

3_.737108

35.09_235

35.637813

35.768852

36.088178

56.396666

i0,

20.

30

40

5O

70

90

II0

130

150

170

190

210

250.

250.

265.

270.

290.

300.

360.

380.

500.

700.

900.

II00.

1300.

1500.

1700.

1900.

2100.

2300.

2500.

2700.

2900.

3100

3300

3500

3700

3900

6100

6300

6500

4700

4900

5100

5300

5500

5700

5900

265.9000NT

O0

O0

O0

O0

O0

O0

O0

O0

O0

00

O0

O0

O0

oo

O0

90

O0

O0

OO

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

O0

0.086190

0.681087

1.034536

1.557518

1.998915

2.671749

3.159136

3 537080

3 864993

6 105273

6 331195

4 532976

6 717513

4.889828

5.056221

5.188553

9.960721

9.909556

9.886732

9.789597

9.712450

9.555069

9.612677

9.333571

9.283230

9.268379

9.22282I

9.203277

9.187868

9.175357

9.165039

9.156372

9,148988

9.142623

9.137080

9 132208

9 127893

9 i26065

9 12059i

9 117676

9 114667

9 112072

9 109716

9 107552

9 105557

9 103713

9 102006

9 100616

9 098932

99.0000

0.021529

0.185579

0.486018

0.854530

1 251186

2.038210

2 772062

3.465051

Q 062509

4.631742

5 160284

5.653553

6 116198

6.553300

6 968059

7.283619

7.636335

8.146228

8.676346

9.707401

10.791886

13._36758

16.624477

18.979662

20.867416

22.395226

23.716806

26.869913

25.892680

26.811596

27.645818

28.609647

29.114063

29.767590

30.377138

30.968237

31.485453

31.992580

32.472813

32.928859

33.363038

35.777353

34.i7354i

36.553122

34.917432

35.267653

35.604835

35.929912

36.243725

90 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA C 13

10.00

30.00

50.00

70.00

90.00

110.00

130.00

150.00

170.00

190.00

210.00

230.00

250.00

270.00

280.00

298.15

320.00

360.00

400.00

440,00

480.00

550.00

650 O0

800 O0

i000 O0

1200 O0

1400 O0

1600 O0

1800 O0

2000 O0

2200 O0

2_00 O0

2600 O0

2800 00

3000 O0

3200 O0

3400 O0

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

X 4/83 HO/R

0.002381

0.007481

0.020230

0.038767

0.061514

0.087126

0.115757

0.146868

0.180153

0.21533I

0.252107

0.290100

0.329001

0.568557

0.388520

0.424975

0.468984

0.549441

0.629261

0.707881

0.784823

0.914152

1.084628

1.306511

1.545371

1.733315

1.884142

2.007710

2.111236

2.199468

2.275868

2.342892

2.402519

2.456076

2.504698

2.549083

2.590015

2.628003

2.663479

2.696792

2.728162

2.758048

2.786381

2.813355

2.839374

-126.7062MP

-0 001179

0 003584

0 010079

0 019685

0 032137

0 046857

0 063688

0 082370

0 102846

0 124798

0 148158

0 172705

0 198511

0 225345

0.239057

0.264663

0 296184

0 356084

0 418064

0 481726

0 546585

0 662128

0 829014

I 077153

1 395392

1 694427

1 973332

2.233430

2.476046

2.703046

2.916380

3.117442

3 307258

3 487389

3 658384

3 821587

3 977299

4 12645_

4 269461

4 406934

539374

4 666803

4 790015

4 909289

5.024590

20.00

40.00

60.00

80.00

I00.00

120.00

140.00

160.00

180.00

200.00

220.00

240.00

260.00

273.15

290.00

300.00

340.00

380.00

420.00

460.00

500.00

600.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

4100.00

6300.00

4500.00

4700.00

4900.00

O.O00ONT

0 003488

0 012971

0 028925

0 049599

0 073843

0 101108

0.131019

0.163254

0.197519

0.233544

0.270978

0.309454

0.348709

0.374835

0.408575

0.428688

0.509244

0.589458

0.668739

0.746599

0.822514

1.001622

1.163061

1.433237

1.644770

1.812587

1.948802

2.061669

2.157041

2.238943

2.310419

2.573585

2.429978

2.480914

2.527335

2.569950

2.609380

2.646042

2.680562

2.712684

2.7_3257

2.772396

2.800027

2.826384

89.0000

0.001443

0.006515

0.014493

0.025571

0.039212

0.055004

0 072842

0 092444

0 113623

0 156292

0 160317

0 185464

0,211757

0.229651

0.253039

0.267324

0,325802

0.386787

0.449667

0.514088

0.579493

0.745444

0.912226

1.238477

1.547481

1.836456

2.105676

2.356752

2.591_05

2.811385

5.018358

5.213635

3.598508

3.573922

3.740984

5.900305

4.052709

4.198739

4.338933

6.473789

4.603658

4.728948

4.850093

4.967460

NASA/TP-3287/REV 1 91
TABLE IV.- Continued.

EFDA CAIS

80.00

100,00

140.00

180.00

220.00

260.00

298.15

350.00

450.00

550.00

650.00

716.00

800.00

I000.00

1115.00

1200.00

1400 O0

1600 O0

1800 O0

2000 O0

2200 O0

2400 O0

2600 00

2800 O0

3000.00

3200.00

3400,00

3600.00

3800.00

4000.00

4200.00

4400.00

_600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

SRD 92 HO/R

0.966374

1.236807

1 628207

1 892326

2 081960

2 224962

2 332800

2 451828

2.631909

2.781836

2.918528

3.005087

3.208423

3.315326

3.392012

4.331409

4.365540

4.391138

4.411047

4.426975

4._40006

4.450866

4.460055

4.467931

4.474758

4 480730

4 486001

4 490685

4 694877

4 498649

4 502062

4 505165

4 507998

4.510595

4.512984

4.515189

4.517231

4.519127

4.520893

4.522541

-695.5244MP

0.540270

0.786069

1.269039

1.712010

2.111099

2.471028

2.783130

3.166800

3.805607

4.348610

4.824549

5.110927

5.464253

6.191387

6.556219

6.873774

7.544162

8.128846

8,647243

9.112847

9.535414

9.922224

10.278856

10.609677

10.918171

11.207160

11.478964

11.735512

11.978425

12.209079

12.428653

12.638162

12.838488

13 030402

13 214583

13 391629

1Z 562072

13 726388

13 885001

14.038295

IIIS.00OONT

90.00

120.00

160.00

200.00

240.00

280.00

300.00

400.00

500 O0

600 00

700 O0

716 O0

900 O0

1100 O0

1115 O0

1500.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

5700.00

5900.00

4100.00

4300.00

4500.00

4700.00

4900 O0

5100 O0

5300 O0

5500 O0

5700 O0

5900 O0

1.109051

1.453252

1.772066

1.994331

2.158099

2.284291

2.337543

2,547475

2.709222

2.851273

2.984281

3.161305

3.259873

3.381003

4.313196

4.349787

4.379192

4.401678

4.419430

4.433801

4.445672

4.455644

4.464139

4.471462

4.477840

4.4834_5

W.488410

4.492858

4.496811

4.500397

6.503650

4.506613

4.509324

4.511814

4.514108

4.516230

4.518197

4.520026

4.521731

79.0000

0.662481

1.031422

1.496146

1.916808

2.295592

2 638128

2 797574

3 500597

4 086958

4 593657

5 043249

5 110927

5 845122

6 510352

6 556219

7 221217

7 845830

8 395380

8 885965

9 329008

9.732907

10.104015

10.447257

10.766525

11.064948

11.345081

11.609057

11.858581

12.095207

12.320184

12.53_608

12.739422

12.935452

13.123420

13.303963

13.477645

13.644968

13.806383

13.962290

92 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA CDIS

100.00

298.15

400.00

594.26

600 O0

800 O0

1000 DO

1200 00

1400 O0

1600 O0

1800,00

2000.00

2200 00

2600 O0

2600 O0

2800 O0

3000 00

3200 O0

3600 O0

3600 O0

3800 O0

4000 00

4200 oo

4400.00

6600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

CODA89

1

2

2

2

6

4

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

3

HO/R

.635695

.519997

.690477

.924126

.145301

.008006

.925630

.870712

,831485

.802065

.779182

.760876

.745899

.733417

.722856

.713804

.705958

.699096

.693037

.687653

,682835

,678500

.674577

.671011

667755

664770

662024

659690

657143

654963

.652934

.651041

-751.3371MP

1 395151

3 710075

4 676030

5 586346

5 626233

6 798067

7 682896

8.393664

8.987036

9.496651

9.945096

10.340291

10.698016

11.023401

11.321805

11.597359

11.853311

12.092265

12.316335

12.527268

12.726518

12.915310

13.094689

13.265546

13.628656

13.584691

13.736237

13.877815

14.015880

14.148842

14.277064

14.600872

200.00

300.00

500.00

594.26

700.00

900.00

Ii00.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500,00

3700.00

3900.00

4100 O0

4300 O0

6500 O0

4700 00

6900 O0

5100 O0

5300 O0

5500 O0

5700 O0

5900 00

O.O000NT

2.252087

2.523701

2.818687

4.150607

4.066847

3.962241

3.895674

3.869590

3.815794

3.789950

3.769547

3.753031

3.739387

3.727926

3.718162

3.709746

3.702415

3.695973

3.690268

3.685179

3.680612

3.676490

3.672752

3.669347

3.666231

3.663369

3.660732

3.658294

3.656033

3.653931

3.651971

63.0000

2,755424

3.725736

5.090498

5.586346

6.259032

7.267394

8.055598

8.702430

9.250833

9.726779

10.147163

10.523592

10.864382

11.175694

11.462218

ii.727610

11.976771

12.206044

12.423347

12.628272

12.822152

13.006117

13.181132

13.348026

13.507519

13.660241

13.806742

13.947510

14.082976

14.213524

14.339500

NASA/TP-3287/REV l 93
TABLE IV. - Continued.

EFDA

EFDA

CLZG

100.00

298.15

400.00

600.00

800.00

1000 O0

1200 O0

1400 O0

1600 O0

1800 O0

2000 O0

2200 O0

2400 O0

2600 O0

2800.00

3000.00

3200.00

3400.00

5600.00

5800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

COIS

100.00

200.00

298.15

350.00

450.00

550.00

700.OO

700.10

900.00

II00.o0

1300.00

1594 O0

1500 O0

1700 00

1768 O0

1900 O0

2100 O0

2500.00

2500.00

2700.00

2900.00

5100.00

5500.00

5500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5180.00

5500.00

5500.00

5700.00

5900.00

TPIS89 HO/R

3 502555

3 705597

3 822881

5 992466

4 102666

4 179O10

4 235518

4.279575

4.515324

4.545668

4.572549

4.596966

4.420889

4.445202

4.470724

4.497974

_.527195

4.558105

4.590524

4.623140

4.655852

4.687616

4.717768

4.745665

4.770758

4.792691

4.811225

4.826226

4.857664

4.845617

4.850214

J 9/67 HO/R

0.627818

1 461902

1 924589

2 089291

2 534072

2 526142

2 758173

2 855944

5 075342

5 324528

5 619715

5 795028

5 883171

5 970239

5 094149

5,078655

5.058890

5.042562

5.028847

5.017164

5.007092

4.998320

4.990611

4.985783

4.977695

4.972228

4.967296

4.962825

4.958747

4.955019

4.951594

4.948459

4.945521

4.942816

4.940300

4.957955

-1104.2275MP

19.250108

23.126809

24.252587

25.817226

26,981800

27.906129

28.6.73251

29.529544

29.905340

50.415505

30.872726

31.290593

51.674276

32.029064

52.559430

52.668824

32.960015

55.255518

55 496805

55 745908

35 983850

34 211857

54 450550

54 640896

34.845557

35.038638

35.226975

55.408860

55.584567

55.754498

55.918764

-575.8161MP

0.295989

1.014251

1.691620

2.015557

2.569644

3.057229

5.694402

5.694822

4.455579

5.076528

5.654554

5.915180

6.194875

6.686794

6.842910

7.209149

7.716455

8.175895

8.595773

8 982343

9 340500

9 674134

9 986587

10 279834

10 556612

10.818511

11.067050

11.505525

11.529053

11.744603

11.951021

12.149047

12.559359

12.522477

12.698979

12.869511

200 O0

500 O0

500 O0

700 O0

900 O0

1100 O0

1300 O0

1500 O0

1700 00

1900 00

2100 O0

2500.00

2500.00

2700.00

2900.00

5100.00

3300.00

5500 O0

5700 O0

5900 O0

4100 00

4500 O0

4500 O0

4700 O0

4900.00

5100.00

5500.00

5500.00

5700.00

5900.00

150.00

250.00

300.00

QO0 O0

500 O0

600 O0

700 i0

800 O0

1000 O0

1200 O0

1594.00

1400.00

1600.00

1768.00

1800.00

2000 O0

2200 O0

2400 O0

2600 O0

2800 O0

5000 O0

5200 O0

5400.00

5600.00

5800.00

4000.00

4200.00

4400.00

4600 O0

4800 O0

5000 00

5200 O0

5400 O0

5600 O0

5800.00

6000.00

O.O000NT

3.578125

5.706016

5.917295

4.053052

4.143943

4.209231

4 258779

4 298240

4 330964

4 359531

4 584814

4 408951

4 432950

4 657767

4 48411fi

4 512576

4 542460

4 574090

4.606688

4.659551

4.671877

4.702959

4.752O25

4.758595

4.782135

4.802588

4.819162

4.852599

4.842069

4.848552

O.O000NT

1.104094

1.725658

1.951162

2.220516

2.435020

2.609294

2.758294

2.954774

5.195618

3.462020

3.795028

3.804193

3 933109

5 992638

5 090184

5 068278

5 050355

5 055419

5 022781

5011948

5 002560

4.994345

4.987097

4.980654

4.974889

4.969701

4.965006

4.960759

4.q56843

6.953271

4.949985

4.946952

4.944145

4.941536

4.939107

4.956841

61.0000

21.674899

25.1496_8

25.096068

26.437285

27.467560

28.305764

29.015216

29.625514

50.165530

30.648806

31.086374

51.486320

51.854912

52.197029

52.516588

52.816431

33.099537

55 567749

35 622844

33 866128

34 09900_

54 322500

34 556786

54 745067

34 941913

55 135579

35.518623

35.497462

35.670246

35.857297

72.0000

0.606289

1.569894

1.705568

2.301558

2.820852

3.280771

5.694822

4.080758

4.765645

5.371535

5.915180

5.929395

6 _47178

6 842910

6 954252

7 469582

7 951575

8 390352

8 792888

9 164710

9 510171

9 832761

I0 155519

I0 420188

10.689520

10.944565

11.186722

11.417594

11.658020

11.848905

12.051040

12.245122

12.451768

12.611527

12.784890

12.952294

94 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA

EFDA

CRIS

i00 O0

200 O0

298 15

311 50

350 O0

450 O0

550 O0

700 O0

900 O0

1100 00

1300 O0

1500 O0

1700 O0

1900 O0

2100 O0

2130 O0

2300 oo

2500 O0

2700 O0

2900.00

3100 00

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500 O0

4700.00

4900.00

5100.00

5300,00

5500.00

5700.00

5900.00

CSIS

lOO O0

298 15

301 59

400 O0

60O O0

800 O0

1000 oo

1200 oo

l_OO OO

1600 oO

1800 00

2000 oo

J 6/73 HO/R

0.374045

1.139574

1.636566

1.688051

1.820226

2.089787

2.291941

2.520379

2.747807

2.946000

3.144642

3.352934

3.571644

3.799762

4.035859

5.229559

5.192656

5.155666

5.124157

5.096993

5.073334

5.052544

5.034129

5.017705

5.002965

4.989664

4.977600

4,966608

4.956552

4.947316

4.938805

4.930936

4.923640

4.916856

4.910531

CODA89 HO/R

2.585841

3.110565

3.119351

3.941303

3.869340

3.78675_

3.736119

3.737643

3.801358

3.932959

4.135675

4.411565

-487.9422MP

0 141439

0 648745

1 204010

1 276766

1 481592

1 973110

2 412967

2 993596

3 655577

4 226281

4 73_476

5 198863

5 631905

6 041468

6 433309

6 490813

6 890941

7.322350

7.717907

8.083092

8._22220

8.738750

9.035497

9.314782

9.578541

9.828406

10.065765

10.291806

10.507560

10.713919

10.911666

11.101492

11.284004

11.459745

11.629199

-927.4148MP

4.026455

7.140190

7.17602q

8.291288

9.877231

10.978759

11.817413

12.497830

13.077929

13.593390

14.067562

14.516911

2130.O000NT

O0 0.788180

00 1.421611

O0 1.643713

50 1.688437

O0 1,965840

O0 2.197363

O0 2.376167

O0 2.641166

O0 2.847793

O0 3.O44377

00 3.247421

3.461043

3.684589

150

250

300

311

400

500

600

8O0

I000

1200

1400

1600 O0

1800 00

2000 O0

2130 O0

2200 O0

2400 O0

2600 O0

2800 O0

3000 O0

3200 O0

3400 O0

3600 O0

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.

6000.00 4.907527

301.5900NT

200.00 2.903959

300.00 3.115437

301.59 3.955219

500.00 3,910513

700.00 3,826014

900.00 5.755951

1100.00 3.729624

1300.00 3.761265

1500.00 3.858476

1700.00 4.025281

1900.00 4.264390

3.916887

4.071902

5.213673

5.173391

5.139306

5.110090

5.084769

5.062614

5.043065

5.025689

5.010141

4.996148

4.983488

4,971979

4.961470

4.951838

4.942976

4.934795

4.927221

4.920187

O0 4.913639

70 0000

0 371840

0 934511

1 214423

1 276766

1 734317

2.198927

2,616069

3.338140

3.950323

4.486795

4 971223

5 418735

5 839243

6 239333

6 490813

6 659655

7 111526

7 524236

7 904003

8 255679

8 583120

8 889441

9 177193

9 448494

9 705119

9 948570

10 180132

10 400910

I0 611862

10 813824

11 007530

ii 193627

11 372689

11 545230

11 711705

23.0000

5.933001

7.159372

7.176024

9.167828

10.470439

11.422815

12.173057

12.797859

13.342057

13.834461

14.294491

NASA/TP-3287/REV l 95
TABLE IV.- Continued.

EFDA CUIS

I00.00

298.15

400.00

600.00

800 O0

I000 O0

1200 00

1358 O0

1400 00

1600 O0

1800 O0

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

5400.00

3600 O0

5800 O0

4000 O0

4200 O0

4400 O0

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600.00

5800.00

6000.00

CODA89 HO/R

0.804617

2.018579

2.267722

2.552165

2.724604

2.854047

2.971512

3.068876

4.223993

4.1891O7

4.161974

4.140268

4.122508

4.107708

4.095186

4.084452

4.075149

4.067009

4.059827

4.053443

4.047730

4 042589

4 037938

4 033710

4 029849

4 026510

4 023054

4 020048

4 017265

4 014681

4.012275

4.010050

-601.8394MP

0.401707

1.968426

2.599311

5.578443

4.337868

4.960124

5.490925

5 864312

5 993102

6 554757

7 046553

7 483877

7 877627

8.255679

8.563964

8.867047

9.148520

9.411259

9.657600

9.889469

10.108471

10.315960

10.515084

10.700830

10.880049

11.051482

11.215777

11.373505

11.525170

11.671221

11.812059

11.948043

200 O0

300 O0

500 O0

700 O0

900 O0

1100 O0

1300 O0

1358 O0

1500.00

1700.00

1900 O0

2100 O0

2300 O0

2500 O0

2700 O0

2900 O0

3100.00

3300.00

3500.00

5700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900 O0

5100 O0

5300 O0

5500 O0

5700 O0

5900 O0

1358.0000NT

1.412843

2.024172

2.451653

2.646492

2 792307

2 912871

5 032049

4 232624

4 205387

4 174743

4.150550

4.130965

4.114787

4.101197

4.089620

4.079640

4.070948

4.063309

4.056543

4.050509

4.045094

4.040207

4.035775

4.031736

4.028042

4.024648

4.021521

4.018630

4.015950

4.013457

4.011134

63.0000

1.241204

1.980995

5.123936

3.979274

4.662852

5.254954

5.751186

5.864312

6.283878

6.808280

7.271248

7.685653

8.060707

8.403230

8.718412

9.010291

9.282074

9.536350

9.775236

10.000489

i0 213579

10 415752

10 608073

10 791457

10 966696

11 134484

11 295429

11 450066

Ii 598871

11 742268

ii 880637

96 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA D 2G

I00.00

298.15

400.00

600.00

800 O0

I000 O0

1200 00

1400 O0

1600 O0

1800 O0

2000.00

2200.00

2600.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

6400.00

6600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

6600.00

6800.00

7200.00

7600.00

8000.00

8400.00

8800.00

9200.00

9600.00

I0000.00

II000.00

12000.00

13000.00

14000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

TPIS89

3

3

3

3

3

3

3

3

5

5

3

3

3

3

4

4

6

6

6

6

6

4

6

HO/R

.307511

.656718

.671383

.692531

.522198

.565015

.616613

.671852

.727116

.780919

.832022

.880120

.925364

.967671

.007500

.066905

.080265

.113942

.146048

.176737

.206312

.234816

.262370

4.289070

6.315149

6.360616

4,365081

6.388766

6.611983

4.434221

6.655518

4.695696

6.531643

6.563045

4.589749

6.611632

4.628596

6.660861

6.648556

6.652039

4.651563

6.635807

6.603694

6,560155

4.509159

6.456076

6.396945

6.339206

6.282086

6.226397

6.172274

-I030.6203MP

10.257693

15.977833

16.995712

16.407258

17.615788

18.206102

18.860508

19.622150

19.916176

20.358256

20 759260

21 126826

21 466536

21 782201

22 077696

22 555525

22 617720

22 866084

23 102187

23 327078

23 562139

23 768047

23 945645

26 135797

26.318373

24.495544

24.666203

26.831667

26.991426

25.146711

25 297405

25 586174

25 859810

26 119830

26 567228

26 605211

26 828717

27 044249

27 250761

27.448736

27.638662

28.081367

28.683440

28.850273

29.186437

29.695659

29.781307

30.046156

30.292588

30.522551

30.737960

200.00

300.00

500.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2500.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

6100.00

4300.00

4500.00

6700.00

4900.00

5100.00

5500.00

5500.00

5700.00

5900.00

6200.00

6600.00

7000.00

7400.00

7800.00

8200.00

8600.00

9000.00

9400.00

9800.00

10500.00

11500.00

12500.00

13500.00

16500.00

15500.00

16500.00

17500.00

18500.00

19500.00

O.O000NT

3.430189

3.457050

3.681666

5.505618

5.562311

3.590043

3 663998

3 699601

3 756431

3 806897

3 856414

3 903124

3 946738

3 987767

6 026695

4.062826

6.097361

4.130076

4.161580

4.191641

6.220618

4.248662

4.275863

4.302169

6.327918

4.352920

4.377102

6.600553

6.42316O

4.445050

4.476080

4.514215

6.547887

4.576993

6.601295

4.620776

6.635526

4.645188

6.650731

4.652287

4.666036

4.621500

4.583127

4.535385

6.481974

6.425686

6.368079

6.310588

4.256067

4.199098

101.0000

12.602578

13.999169

15.771654

16.946585

17.831665

18.547066

19.151125

19.676441

20.142875

20.563323

20.946909

21.299747

21.627055

21.932413

22.218662

22.488627

22.743530

22.985619

23.215969

23.635815

23.646182

23.847860

24.041620

26.228177

26.407976

24.581546

26.749439

24.912050

25.069612

25.222600

25.645782

25.724852

25.991502

26.245037

26 486660

26 717227

26 937690

27 148649

27 350818

27 544586

27 865471

28 287169

28 670946

29 021898

29 364239

29 661193

29 916134

30 171473

30 609487

30 631996

NASAFFP-3287/REV l 97
TABLE IV.- Continued.

EFDA E IG

200.00

300.00

500.00

700.00

900.00

ii00.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300,00

2500.00

2700.00

2900.00

3100.00

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500.00

4700.00

4900.00

5100 O0

5300 O0

5500 O0

5700 O0

5900 O0

6200 O0

6600 O0

7000 O0

7400 O0

7800 O0

8200.00

8600.00

9000.00

9qO0.O0

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

L 6/88 HO/R

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

-745.3750MP

-0 975019

0 038643

1 315708

2 156888

2 785174

3 286851

3 704486

4.062238

4.375146

4.653210

4.903419

5.130848

5.339302

5.531705

5.710352

5.877081

6.033382

6.180_83

6.319408

6.451017

6.576043

6.695113

6.808769

6.917482

7 021663

7 121677

7 217843

7 310446

7 399741

7 485956

7 609949

7.766250

7.913351

8.052275

8.183885

8.308911

8.427981

8.541637

8.650350

8.754531

8.927014

9.154443

9.362897

9.555300

9.733947

9.900676

10.056976

10.20_078

10.343002

I0.474612

298

400

600

800 O0

1000 O0

1200 O0

1400 O0

1600.00

1800.00

2000.00

2200.00

2400,00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600 O0

5800 O0

6000 O0

6400 O0

6800.00

7200.00

7600.00

8000.00

8400.00

8800.00

9200.00

9600.00

10000.00

II000.00

12000 O0

13000 O0

14000 O0

15000 O0

16000 O0

17000 O0

18000 O0

19000 O0

20000 O0

15

O0

O0

O.O000NT

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,5000O0

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

100

0

0

1

2

0000

023179

757849

771511

490717

3 048575

3 504379

3 889756

4 223585

4 518042

4.781443

5.019719

5.237247

5.437354

5.622624

5.795106

5.956453

6.108014

6,250910

6.386078

6.514311

6.636287

6.752587

6.863716

6,970115

7.072170

7.170222

7.264573

7.355492

7.443220

7.527974

7.689320

7.840882

7.983778

8.118946

8.2_7179

8,369155

8.485455

8.596584

8,702983

8.805038

9.043314

9.260842

9.460949

9.646219

9.8187O1

9.980047

10.131609

10.274505

10.409673

10.537906

98 NASA/TP-3287/REV l
TABLE IV.- Continued.

EFDA F 2G

I00.00

298.15

400.00

600.00

800.00

I000.00

1200.00

1400.00

1600.00

1800 O0

2000 O0

2200 O0

2400 00

2600 O0

2800 00

30OO O0

3200 O0

3400 O0

36O0 O0

3800 O0

4000 O0

4200 O0

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600. O0

5800. O0

6000.00

TPIS89 HO/R

3.496339

3.559987

3.638863

3.797022

3.924662

4.023136

4.101113

4.164800

4.218730

4.265286

4.305778

4.340711

4.370174

4.393947

4.412090

4.424607

4.431726

4.433798

4.431263

4.624626

_.414354

4.401022

4.385048

4.366908

4.346971

_.325599

4.303118

4.279785

q.255821

4.231457

4.206833

-I061.qI03MP

16.994591

20.830198

21.887181

23.393241

24.503693

25.390617

26.131098

26.768363

27.328067

27.827671

28.279216

28.691338

29.070323

29.421080

29.747399

30 052283

30 338029

30 606813

30 860237

31 099602

31 326366

31 541396

31.745717

31.940299

32.125731

32.302737

32.471951

32.633959

32.789140

32.938108

33.081081

200

300

500

700

900

1100

1300

1500

1700

1900

2100

2300

2500

2700

2900

3100

3300

3500

3700

3900

4100

4300

4500

4700

4900

5100

5300

5500

5700

5900

O.O000NT 61.0000

.00 3.509570 19.420741

.00 3.561287 20.852231

.00 3.720769 22.707925

.00 3.864891 23.983748

.00 3.976897 24.969113

.00 4.064247 25.775994

.00 4.134435 26._60761

• 00 4.192801 27.056680

• 00 _.242811 27.58_583

•00 4.286217 28.058952

•00 4.323933 28.489820

• 00 4.356135 28.884588

.00 4.382752 29.248979

.00 q.403733 29.587133

.00 4.419042 29.902335

• 00 4.428805 30.197464

.00 4.433340 30.474489

• 00 4.433061 30.735400

.00 4.428424 30.981545

.00 _.419914 31.214485

O0 4.408039 31.435274

00 4.393325 31.644830

O0 4.376231 31.8_4259

O0 _.357137 32.034141

O0 4.336435 32.215287

O0 _.314480 32.388305

O0 4.291526 32.553902

O0 4.267859 32.712396

O0 4.243679 32.864426

O0 4.219161 33.010300

NASAfrP-3287/R.EV l 99
TABLE IV. - Continued.

EFDA FEIS

I00.00

200.00

298.15

350.00

450.00

550.00

700.00

900.00

i000.00

1040.00

I042.00

1100.00

1184.00

1300.00

1500.00

1665.00

1700.00

1809.00

1900.00

2100.00

2300.00

2500.00

2700.OO

2900.00

3100.00

5300.00

3500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

J 3/78 HO/R

0.508749

1.318177

1.818093

2.006819

2.292913

2.525268

2.825697

3.219138

3.468154

3.619946

3.632043

3.769861

3.964292

3.979327

4.021083

4.066194

4.143925

4.198693

5.136709

5.174678

5.206044

5.232391

5.254835

5.274183

5.291035

5.305844

5.318960

5.330659

5.341157

5.350632

5.359225

5.367054

5.374217

5.380795

5.386858

5.392462

5.397659

5.402492

5.406997

-542.0644MP

0.220699

0.840579

1.467849

1.774402

2 314936

2 798077

3 442742

4 199098

4 550599

4 689143

4.696169

4.897156

5.178776

5.549918

6.122149

6.543932

6,630011

6.889188

7.140808

7.656839

8.129037

8.564239

8.967804

9.344009

9.696319

10.027585

10.340173

10.636075

10.916979

11.184332

11.439378

ii.683200

ii.916744

12.140840

12.356223

12.563544

12.76338_

12.956265

13.142655

150.00

250 O0

300 O0

400 O0

500 O0

600 O0

800 O0

950.00

1030.00

1041.00

1042.00

1184.00

1200.00

1400.00

1600.00

1665.00

1800.00

1809.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

O.O000NT

0.955759

1.602019

1.825325

2.159177

2.413612

2.629941

3.015812

3.326208

3.565062

3.625942

3.632043

3.872870

3.965858

3.998174

4.047518

4.126655

4.194140

5.116654

5.156643

5,191074

5.219766

5.244044

5.264854

5.282890

5.298670

5.312595

5.324972

5.356046

5.346013

5.355031

5.363228

5.370713

5.377575

5.383887

5.389714

5.395109

5.400119

5.404783

5.409136

78.0000

0.514081

1.166595

1.479261

2.052857

2.562869

3.022467

3.832457

4.377674

4.654424

4.692648

_.696169

5.178776

5.232038

5 84546i

6 3824_2

6 543932

6 868207

6 889188

7 404802

7 897950

8 350899

8.769687

9.159093

9.522960

9.864425

10.186081

10.490098

10.778306

11.052267

11.313322

11.562630

11.801203

12,029925

12.249578

12.460853

12.664365

12.860664

13.050244

13.233549

100 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA GEIS

100.00

298.15

350.00

450.00

600.00

800.00

1000.00

1200.00

1211.40

1400.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200 O0

3_00 O0

3600 O0

3800 00

40O0 O0

4200 O0

4400 O0

_600 O0

4800 00

5000 00

5200 O0

5400 O0

5600 OO

5800.00

6000.00

TPIS91

0

1

2

2

2

2

2

HO/R

.745684

.870276

,012994

.214985

,615634

.589133

.710867

2.805309

6,486587

6.059936

5.717580

5.450949

5.237806

5.063612

6.918086

4.795118

4.689716

4.598368

6.518639

4.447915

4.385223

4.329133

4.278651

6.232977

4.191455

4.1535_4

6.118792

4.086820

4.057308

6.029982

4.004607

3.980983

3,958953

-557.6228MP

0.440916

1.868973

2.180429

2.712260

3.379056

4.099662

6.690936

5.193841

5.220389

6.127357

6.915169

7.570581

8.133470

8.624243

9.058604

9.447074

9.798476

10.118846

10.413011

10.684780

10.937207

11.172774

11.393523

11.601156

11.797101

11.982570

12.158598

12.326079

12.485784

12.638389

12.784486

12.924596

13.059182

I211,4000NT

200.00

300 O0

400 O0

500 O0

700 00

900 O0

1100 O0

1211.40

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.0D

3300.00

3500 O0

5700 00

3900 O0

4100 00

4300 O0

4500 00

6700 O0

4900 O0

5100 00

5300 00

5500 00

5700.00

5900.00

1.464308

1,875975

2,123619

2.291970

2.511322

2,656476

2.760618

2.810136

6.270737

5.877239

5.576328

5.338767

5.146456

4.987590

4.854142

4.740465

4.642467

6.557115

6.482107

4.615673

4.356420

4.303244

6.255257

4.211733

4.172078

4.135798

4.102480

4.071775

4.043387

4.017064

3.992588

3.969771

65.0000

1,202717

1.880560

2,456697

2.969726

3.758858

4.408273

4.951688

5.220389

5.670553

6.539075

7.255666

7.862239

8.386777

8.867623

9.257856

9.627005

9.962211

10.268945

10.551489

10.813246

11.056961

11.286887

11.498885

11.700509

11.891077

12.071705

12.263356

12.406859

12.562935

12.712217

12.855259

12.992553

NASA/TP-3287/REV 1 101
TABLE IV.- Continued.

EFDA H 2G

50.00

150.00

250.00

300.00

400.00

600.00

800.00

1000.00

1200.00

1400.00

1600.00

1800.00

2000.00

2200.00

2600.00

2600.00

2800.00

5000.00

3200.00

3400.00

5600.00

3800 O0

6000 O0

42O0 O0

4600 O0

6600 O0

6800 O0

5000 O0

5200 00

5400 O0

5600 O0

5800 O0

6000.00

6600.00

6800.00

7200 O0

7600 OO

8000 O0

8600 O0

8800 O0

9200 O0

9600 O0

10000 OO

110oo O0

12000 O0

13000 O0

16000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

TPIS78 HO/R

3.283656

5.685911

5.610666

3.416157

3.435602

5.665465

5.485260

5.505601

5.534626

5.569668

3.608795

3.650625

3.693407

5.736175

5.778179

3.819088

3.858662

3.896889

3 955685

3 969156

4 003424

6 036556

4 068659

6 099796

4 130097

4 159595

4 188511

6.216294

6.263536

6.270007

4.295683

6.520501

6.346625

6.389586

4.650066

6.666092

6.497218

4.523276

6.564276

6.560547

6.571686

6.578597

6.581607

6.572992

6.567086

6.508882

6.662571

4.611529

6.357503

_.302735

6.268160

4.194557

6.142405

-I018.6727MP

6.053519

9.966319

11.700703

12.322555

15.308033

16.706869

15.705888

16.685608

17.126985

17.676525

18.155596

18.580955

18.967905

19.521918

19.648792

19.952827

20.237388

20.504775

20.757679

20.997072

21.226877

21.442275

21.650116

21,869425

22.040785

22.225136

22.602685

22.576235

22.740151

22.900825

23.056521

23.207784

23.5566_7

23.656468

23.903808

24.158121

26.600576

26.631822

26.853052

25.066779

25.267767

25.462633

25.669416

26.085882

26.682830

26.845290

27.177751

27.483952

27.766899

28.029498

28.275864

28.502106

28.715903

100.00

200.00

298.15

350.00

500.00

700 O0

900 O0

ii00 O0

1300 O0

1500 O0

1700 O0

1900 O0

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

5500.00

3700.00

3900.00

6100.00

4300 O0

6500 O0

6700 O0

6900 O0

5100 O0

5300 O0

5500 O0

5700 O0

5900.00

6200.00

6600.00

7000.00

7400.00

7800.00

8200.00

8600.00

9000.00

9400 O0

9800 O0

10500 O0

11500 O0

12500 O0

13500 O0

14500 O0

15500 O0

16500 O0

17500 O0

18500 O0

1950O O0

O.OO00NT

3.606991

3.623574

3.615976

3.625722

3.651598

3.673688

3.493667

3.519191

5.551295

5.588709

5.629489

3.671938

3.716836

3.757280

3.798802

5.839073

3.877937

3.915433

3.951591

5.986635

6.020113

4.052711

6.086328

4.115067

4.166932

6.174060

4.202392

6.250029

6.256876

4.282968

6.508204

6.352586

6.367608

6.610288

6.468679

6.682286

6.510889

6.534416

6.552925

4.566583

6.575676

4.580691

6.579768

6.561886

4 529255

6 486517

4 437606

6 386622

6 330153

6 275373

4.221203

4.168278

105.0000

8.507572

10.958292

12.301269

12.850050

16.076658

15.261425

16.116798

16.820128

17.610558

17.921369

18.372967

18.779017

19.148656

19.688660

19.803607

20.097375

20.573145

20.632965

20.878867

21.112652

21.534856

21 547355

21 750871

21 946026

22 133835

22 316726

22 689275

22 65792I

22 821108

22 979295

23.132762

23.281695

23.697521

23.771801

26.052529

26.280722

26.517641

26.765606

26.959986

25.167390

25.566129

25.556878

25.872977

26.288965

26.667980

27.015110

27.333873

27.628165

27.900570

28.155801

28.389823

28.610650

102 NASAJTP-3287/REV 1
TABLE IV.- Continued.

EFDA HE1G

100.00

298.15

400.00

600.00

800.00

1000.00

1200.00

1400.00

1600.00

1800 O0

2000 00

2200 O0

2400 O0

2600 O0

2800 O0

30O0 oo

3200 OO

3400.00

3600.00

3800.00

4000.00

4200.00

6400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

6400.00

6800.00

7200.00

7600.00

8000.00

8400.00

8800.00

9200.00

9600.00

10000.00

Ii000.00

12000.00

13000.D0

14000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

EFDA HG1S

I00.00

200,00

254.29

298.15

550.00

450.00

550.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

LIO/90

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

2

J12/61

2

2

3

3.

3

3

3

3

3

3

3

3

3

3

HO/R

.500000

.500000

.50000o

.500000

.500000

.500000

.500000

.500000

.500000

.500000

.500000

.500000

.500000

.500000

.500000

500000

500000

500000

500000

500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2 500000

2 500001

2 500004

2 500013

2 500041

500107

500251

500415

500705

501238

HO/R

.051835

.580429

.871291

768902

705762

615366

552388

491658

653000

662066

446061

459095

_77903

500728

-745.5750MP

9.941649

12.672716

13.407385

14.421048

15.140253

15.698112

16.153916

16.539293

16.873121

17.167579

17.430980

17.669256

17.886784

18,086891

18.272161

18.444643

18.605989

18.757551

18.900447

19,055615

19,163848

19.285823

19.402124

19.513253

19.619652

19,721707

19.819759

19.914110

20.005029

20.092757

20.177511

20.538857

20,490419

20.633315

20.768483

20.896716

21,018691

21.134991

21.246121

21.352520

21,654575

21.692850

21,910379

22.110486

22.295756

22,468240

22.629591

22.781163

22,924072

23.059265

23,187566

-1123.6982MP

2.424557

6.037159

4.454495

5.375112

5,974666

6.894092

7.613153

8.662023

9.334044

10.025595

10.600828

11.094741

11.528874

11.916897

200.00

300.00

500.00

700 O0

900 O0

1100 O0

1300 O0

1500 O0

1700 O0

1900 O0

2100 00

2500 O0

2500 O0

2700,00

2900.00

3100.00

3300.00

5500,00

5700.00

3900,00

4100.00

6300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600.00

7000,00

7600.00

7800,O0

8200,00

8600,00

9000.00

9400,00

9800.00

10500.00

11500.00

12500,00

15500.00

16500.00

15500.00

16500.00

17500.00

18500,00

19500.00

150.00

254.29

250.00

300.00

400,00

500,00

600.00

800.00

1000.00

1200.00

1600.00

1600.00

1800.00

2000.00

O.O000NT

2 500000

2 500000

2 500000

Z 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.5D0000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500002

2.500007

2.500024

2.500067

2.500166

2.500559

2.500513

2.500952

O.O000NT

2.375766

2.693009

3.842920

3.766508

3.656259

3.581209

3.523570

3.467585

3.445062

3.442676

3.451711

5.467958

3.488948

3,513256

i01.0000

11.674517

12.688180

13.965244

14.806425

15.436711

15.936388

16.554023

16.711775

17.026683

17.502747

17.552956

17.780385

17.988839

18.181242

18.359889

18.526617

18.682918

18.830020

I8.968964

19.100554

19.225580

19,546650

19.458306

19.567018

19.671200

19.771214

19.867379

19.959982

20.069278

20.135493

20.259485

20.415786

20.562888

20.701812

20.833422

20.958448

21.077518

21.191174

21.299886

21.604068

21.576550

21.803980

22.012434

22.204837

22.583685

22.550216

22.706524

22.853640

22.992578

23.124224

28.0000

3.324269

4.454495

4.704667

5.598314

6.665925

7.273068

7,921152

8.926654

9.697505

10.325062

10.856408

11.318241

11.727944

12,096804

NASA/TP-3287/REV 1 103
TABLE IV.- Continued.

EFDA

EFDA

1 2S

5 O0

15 00

25 O0

35 O0

65 O0

60 O0

80 O0

100 O0

120 00

160 O0

160 O0

180 O0

200 O0

220 O0

260 O0

260.00

280.00

298.15

320.00

360.00

386.75

600.00

600.00

800.00

I000.00

1200.00

1400.00

1600 O0

1800 O0

2000 O0

2200 00

2600 O0

2600 00

2800 O0

3000 O0

3200 O0

3600 O0

5600 O0

3800 O0

4000 O0

6200 O0

4600.00

6600.00

6800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

K 1S

100 O0

298 15

336 86

600 00

600 O0

800 O0

10o0 O0

1200 O0

1400.00

1600.00

1800.00

2000.00

2200.00

TPIS89 HO/R

0.017319

0.368833

0.995849

1.587586

2.079364

2.662013

3.246328

3.669689

5.996026

6.257617

4.470568

6.647852

6.799661

6.931138

5.069606

5.153178

5.265993

5.323176

5.610722

5.570917

5.685966

10.524706

10.205876

10.066459

9.950809

9.887063

9.841496

9.807336

9.780766

9.759511

9.762120

9.727628

9.715365

9 706856

9 695765

9 687774

9 680741

9 676690

9 668896

9 663862

9 659307

9 655166

9 651386

9 647920

9.644752

9.661789

9.639064

9.636536

9.656178

9.651979

CODA89 HO/R

2.086308

2.859251

2.956843

3.790662

3.761096

3.719852

$.701862

3.72O2O3

3.780912

3.887030

6.060259

6.261801

6.492256

-1587.1050MP

0.005773

0.139435

0.671585

0.905886

1.366616

2.046142

2.895901

3.667925

4.367425

5.005562

5.586609

6.124060

6.621557

7.085204

7.519465

7.927929

8.313195

8.645055

9.024606

9.671112

I0 074314

10 629398

16 627805

17 539824

19 770558

21 578815

23 099309

24 611126

25 566669

26 596O56

27 523375

28 370610

29 148539

29.868130

30.537378

31.162667

31.769970

32.303125

32.826065

35.321865

33.793254

34.242508

34.671613

35.082298

35.476079

35.856295

36.218127

36.568631

36.906768

37.233326

-852.6856MP

2.19616I

6,91992I

5.276636

5.925366

7.458207

8.556267

9.361826

10.037793

10.615266

11.126682

11.592652

12.028310

12.444060

386.7500NT

10.00

20.00

30.00

60.00

50.00

70.00

90.00

110.00

130.00

150.00

170.00

190.00

210.00

230.00

250.00

270.00

290.00

300.00

$60.00

380.00

386.75

500,00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100 O0

2300 00

2500 O0

2700 O0

2900 O0

3100 O0

3300.00

3500 O0

3700 O0

3900 O0

6100 O0

6500 O0

6500 O0

6700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

0.132299

0.673521

1.306952

1.861204

2.292378

2.977583

3.471862

3.842133

6.I35645

6.368267

4.56254I

4.726677

6.867566

6.991797

5.102886

5 200636

5 288636

5 330841

5 689360

5 656250

10 557476

10 333606

10 I14779

9 993320

9 916028

9 862518

9 823277

9 793270

9.769579

9 750602

9 736559

9 721251

9 709915

9 700143

9 691631

9.684151

9.677526

9.671617

9.666316

9.661529

9.657189

9.653256

9.669616

9.666294

9.643232

9.640601

9.637776

9.635335

9.633060

336.8600NT

200.00

300.00

356.86

500.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2.600875

2.863668

3.783527

3.781341

3.738903

$ .706906

$ .706007

3.765075

3.828167

3.957645

6.134960

6.360879

99.0000

0.043779

0.288652

0.679695

1.118286

1.596662

2.480345

3.291876

6.026160

6.692732

5.301575

5.860563

6,577285

6.857358

7.305861

7.726613

8.123561

8.697986

8.677922

9.555070

9.976497

10.074316

12.755782

16.193866

I8.719935

20.717287

22.369207

23.777667

25.005262

26.093182

27.069980

27.956260

28.767381

29.515096

30.208603

30.855232

31.660920

32.030546

32.568157

33.077166

33.560662

34.020517

36.459466

34.879158

35.281216

35.667056

36.037960

36.596986

36.739183

37.071629

25.0000

3.829691

6.937513

5.276636

6.770573

8.036295

8.971532

9.714767

10.336453

10.877570

11.366266

11.813685

12.238175

104 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA

EFDA

KR1G

100 O0

298 15

400 O0

6O0 O0

800 O0

1000 O0

1200 O0

1600 O0

1600.00

1800.00

2000,00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

5600.00

3600.00

3800.00

6000 O0

6200 O0

6600 O0

6600 O0

6800 O0

5000 O0

5200 O0

5600 O0

5600 O0

5800 O0

6000 O0

6400.00

6800.00

7200.00

7600.00

8000.00

8600.00

8800.00

9200.00

9600.00

10000.00

11000.00

12000.00

13000.00

14000.00

15000.00

16000.00

17000.00

18000.00

19O00.00

20000.00

LI1S

i00.00

250.00

300.00

600 O0

653 69

600 O0

800 O0

I000 O0

1200 O0

1600 O0

1600 O0

1800 O0

2000 00

22OO O0

2600 O0

2600 O0

2800 O0

3000.00

LlO/90 HO/R

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500O00

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2 500001

2 500003

2 500010

2 5OOO27

2 500064

2 500160

2.500283

2,500543

2.500989

2.501716

2.502686

2.507963

2.518189

2.539013

2.567663

2.610570

2,677380

2.767613

2.882396

3.010985

3.098523

TPIS82 HO/R

0.594162

1.669371

1.875660

2.189056

3.133O74

3.247172

3.515319

3.346997

3.366367

3.382966

3.601216

3.623559

3.651356

3.685457

3.526623

3.574630

3.630346

3.693756

-745.3750MP

14.503882

17.234968

17.969618

18.983281

I9.702686

20.260345

20.716149

21.101525

21.635554

21.729811

21.993213

22.231688

22._69017

22 669123

22 834393

23 006875

23 168222

23 519783

23 662679

23,597847

23.726081

23.848056

23.964_56

26.075685

24.181885

26,283939

24.381991

24.676362

24,567261

26,654990

26.739743

24,901090

25.052652

25.195569

25.330719

25.458957

25.580965

25.697261

25.808626

25 914879

26 017016

26 255750

26 476282

26 676578

26 865256

27.043243

27,213733

27.378633

27.539958

27.697976

27.845676

-557.0984MP

0,287649

1.322026

1.665376

2.229915

2.516841

5.407889

4.352783

5.096352

5.708588

6.228561

6.681669

7.083296

7.665391

7.775886

8.080866

8.366985

8.631885

8.886671

200.00

300.00

500.00

700.00

900.00

1100.00

1300.00

1500,00

1700.00

1900.00

2100,00

2300.00

2500.00

2700.00

2900,00

3100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 00

6300.00

4500.00

4700.00

6900.00

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600 00

7DDD 00

7600 O0

7800 00

8200 O0

8600 O0

9000 00

9600.00

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

O.O000NT

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

Z.500000

2.500000

2.500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2.500002

2,500006

2,500017

2.500062

2.500095

2.500201

2 500396

2 500757

2 501310

2 502225

2 506702

2 512293

2 527097

2 552868

2 584726

2 661121

2 719670

2 821925

2.968888

3.055200

I01.0000

16.236750

17.250413

18.527477

19.368657

19.996943

20.698620

20.916255

21.276007

21.586915

21.866979

22.115188

22.562618

22.551072

22.763676

22.922122

23.088850

23.245151

23.392252

23.531177

23.662786

23.787812

23.906882

24.020538

26.129251

26.233433

24.333446

26._29612

26.522215

24.611510

26,697726

24 821718

24 978019

25 125121

25 266047

25 395660

25 520693

25 639777

25 753658

25.862214

25.966668

26 139162

26 367292

26 577251

26 772511

26 955198

27 129323

27 296749

27 459628

27.619825

27.772659

653.6900NT 35.0000

200.00 1.405976 0.981657

298.15 1.868517 1.633794

350.00 2.062779 1.967654

453.69 2.337784 2.516861

500.00 3.179505 2.821679

700.00 3.288524 3.911792

900.00 3.333655 4.744393

ii00.00 3.357450 5.415862

1300.00 3.376656 5.978171

1500.00 3.391689 6.462255

1700.00 3.611776 6.887957

1900.00 3.436713 7.268746

2100.00 3.467577 7.614169

2300.00 3.505055 7.931247

2500.00 3.549603 8.225285

2700.00 3.601535 8.500391

2900.00 3.661077 8.759809

NASA/TP-3287/REV 1 105
TABLE IV.- Continued.

EFDA MG1S

20 O0

40 O0

60 O0

80 O0

100 O0

140 O0

180 O0

220 O0

260 O0

298 15

350 O0

450 O0

600 O0

800 O0

923 O0

1000 O0

1200 O0

Iq00 00

1600 O0

1800 O0

2000.00

2200 O0

2400 O0

2600 O0

2800 O0

3000 O0

3200 O0

3400 O0

3600 O0

3800 O0

4000 O0

4200 O0

4400 O0

4600 00

4800 O0

5000 O0

5200 O0

5400 O0

5600 O0

5800.00

6000.00

SRD 92 HO/R

0.010668

0.099493

0.295747

0.533449

0.766804

1.165308

1.465181

1.693522

1.871663

2.008560

2.161055

2.381607

2.611855

2.840260

2.965598

4.065178

4.075202

4.082561

4.087731

4.091907

4.095248

4.097982

4,100260

4.102188

_.i03840

4.105272

4.106525

4.107630

4.108613

4.109492

4.110283

4.110999

4.111650

4.112244

4.112789

4.113290

4.113753

_.114181

4.114579

4.114949

4.115295

-598.8520MP

0.004347

0.031357

0.106429

0.223666

0.368352

0.692914

1.023649

1.340807

1.638764

1.904487

2.238875

2.810162

3.528819

4.312687

4.727697

5.053225

5.795336

6._24097

6.969587

7.451303

7.882608

8,273059

8.629730

8.958005

9.262071

9.545257

9.810246

10.059236

10.294050

10.516216

10.727025

10.927584

11.118843

11,301627

11.476654

11.644557

11.805892

11.961154

12.110785

12.255177

12.394686

30

50 O0

70 O0

90 O0

120 00

160 O0

200 00

240 O0

280 O0

300 O0

400 O0

500 O0

700 O0

900 O0

923.00

I100.00

1300.00

1500.00

1700 O0

1900 O0

2100 O0

2300 O0

2500 O0

2700 O0

2900 O0

3100 O0

3300.00

3500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

923.0000NT

O0 0.037776

0.188871

0.412549

0.653616

0.980146

1.325823

1.586781

1.787814

1.946761

2.014601

2.281029

2.467950

2.732278

2.942441

4.060161

4.070646

4.079057

_.085225

4.089942

4.093666

4.096680

4.099170

_.I01262

4.103044

4.104580

4.105918

107094

108135

109064

109898

110650

111332

111954

112523

113045

113526

113971

11_384

114767

115125

81.0000

0.012838

0.062749

0.160705

0.293464

8.527584

0.859253

1.184457

1.492288

1.780267

1.916930

2.535526

3.065665

3.940698

4.653155

4.727697

5.4409_2

6.121685

6.705851

7.217472

7.672589

8.082451

8.455248

8.797132

9.112839

9.406094

9.679879

9.956619

10.178314

10.406628

10.622967

10.828524

11.024322

11.211247

11.590069

11.561459

11.726013

11.884254

12.036648

12.183613

12.325522

106 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA MN1S

100.00

200.00

298.15

350.0O

500,00

600.00

800.00

980.00

1000.00

1200.00

1361.00

lqO0.O0

1_12.00

1519.00

1600 O0

2800 O0

2000 O0

2200 O0

2400 O0

2600 O0

2800 O0

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

J 9/67 HO/R

0.714414

1.537072

2.014545

2,195817

2,589690

2.781483

3.090982

3.323671

3.615487

3.776931

3.883158

4,102209

4.271859

4.358126

5.324122

5.347595

5.366374

5.381739

5.394542

5.405376

5.414663

5.422711

5.429753

5.435966

5 441489

5 446431

5 450879

5 454903

5 458561

5 461901

5 464963

5.467780

5.470380

5.472787

5.475023

5.477104

5.479047

-600.6367MP

0.352997

1.124901

1.835351

2 173051

3 026516

3 516182

4 360570

5 011168

5 084004

5.758086

6.2403_9

6.355774

6.390794

6.706026

6.982331

7.610832

8.175264

8.687478

9.156316

9.588549

9.989479

10.363333

10.713536

11.042903

11.353773

11.648114

11.927595

12.193643

12.447491

12.690209

12.922731

13.145879

13.360381

13.566880

13.765954

13.958116

14.143832

150.00

250.00

300,00

400.00

550,00

700.00

900,00

980,00

II00.00

1300.00

1361.00

1412.00

1500.00

1519.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500 O0

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900,00

O.O000NT

1.179464

1.807924

2.'021767

2.342892

2.689931

2.945453

3,223949

3.596859

3.701306

3.844900

4.070679

4.11180g

4.343170

5.312857

5.336549

5.357479

5 374422

5 388419

5 400176

5 4101gl

5 418825

5 426345

5 432954

5 438807

5 444027

5 448712

5 452940

5 456774

5 460268

5 463465

5 466400

5.469105

5.471606

5.473925

5.476082

5.478092

73.0000

0.734659

1.498705

1.847734

2.475913

3.278190

3.957539

4.732383

5.011168

5.432726

6.063080

6.2403_9

6.390794

6.651224

6.706026

7.305485

7 900231

8 437288

8 926855

9 376647

9 7926_I

10 179560

I0.5_1202

10.880668

11.200520

11.502900

11.789618

12.062217

12.322022

12.570180

12.807690

13.035429

13.254169

13.464593

13.667312

13.862869

14,051753

NASA/TP-3287/REV 1 107
TABLE IV.- Continued.

EFDA HO1S

100.00

200.00

296.15

350.00

450.00

550.00

700.00

900.00

II00.00

1300.00

1500.00

1700.00

1900.00

2100.00

2500.00

2500.00

2700.00

2896 O0

2900 00

5100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

_300 00

4500 O0

4700 O0

4900 O0

5100 O0

5300 O0

5500 00

5700 O0

5900 O0

J 3/78

0

1

1

2

2

2

2

2

2

2

HO/R

.590536

.603570

.869558

.007850

.231708

.391001

.566020

.727696

.852188

.959166

3.059711

3.159820

3,263097

3.372303

3.689552

3.616762

3.758311

3.923377

5.616696

5.359233

5.308913

5.266363

5.226592

5.188918

5.i56725

5.127526

5.100923

5.076583

5.056231

5.033632

5.014587

4.996928

6.980507

6.965200

-551.4656MP

0.256495

0.959081

1.590815

1.900258

2.435510

2.897705

3.495507

4.160705

6.720677

5.205857

5.636412

6 025448

6 382450

6 71640i

7 026602

7 322628

7 606159

7 876997

7 882476

8 261777

8 575248

8 886303

9 177727

9 451822

9 71051i

9 955414

10 187915

10 609196

I0 620282

10 822063

II O1532O

11 200737

11 378923

II 550616

150.00

250.00

300.00

400.00

500.00

600.00

800.00

I000.00

1200.00

1600 O0

1600 O0

1800 O0

2000 O0

2200 00

2600 O0

2600 00

2800 00

2896 00

5000 O0

3200 O0

3_00.00

3600.00

3800.00

6000.00

4200.00

6400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

O.O000NT

1.055985

1.660711

1.855792

2.130312

2.317395

2.455547

2.652592

2.793069

2,906966

3.009799

3.109569

3.210853

3,316792

3.629765

3.551773

3.685126

3.838670

5.617720

5.386909

5.333286

5.285973

5.263916

5.206286

5.172419

5,161778

5.113922

5.088488

5.065174

5.043725

5.023926

5.005594

4.988571

4.972722

6.957929

68,0000

0.585482

1.281374

1.602379

2.176617

2.673158

3.108582

3.843883

4.651495

4.971069

5.427019

5.835416

6.207502

6.551258

6.872586

7.176220

7.665623

7.744173

7.874997

8.065597

8.611511

8.733391

9.034315

9.316813

9.582985

9.834594

10.073137

10.299890

10.515955

10.722284

10.919712

11,108969

11.290699

II.665_75

11.633805

108 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA N 2G

100.00

200.00

298.15

350.00

500.00

700.00

900.00

II00.0o

1300.00

1500.00

1700.00

1900.00

2100.00

2500.00

2500.00

2700 O0

29O0 O0

3100 00

3300 O0

3500 O0

3700 O0

3900 O0

6100 O0

6300 O0

6500.00

6700,00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600,00

7000.00

7600.00

7800.00

8200.00

8600.00

9000.00

9600.00

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

EFDA NAIS

100.00

298.15

371.01

600.00

600,00

800.00

1000.00

1200.00

1600.00

1600.00

1800.00

2000.00

2200.00

TPIS78 HO/R

3.690326

3.695738

3.497461

3.698573

5,507605

5.540669

3.595761

5.655209

3.716626

3.776691

5.827374

5.875157

3,918097

3.956619

3,991384

6,022779

6.051255

6.077181

6.100912

6.122688

6.142791

6.161388

6.178699

6.196819

4.209933

6.226165

6.237566

6.250287

6.262454

6.276O67

6.285247

6.296095

6.311908

4.332547

6.353285

6.376756

4.397571

6.622369

4.449714

4.680167

6.516080

6.551883

6.627995

6.758925

4.912839

5.082332

5.257653

5.627860

5.586565

5.721275

5.836662

5.923118

CODAS9 HO/R

1.620059

2.605920

2.792632

3.667238

3.661671

3.629799

3.597085

3.579786

3.585213

3.617020

3.677306

3.767390

3.888110

-I062.7679MP

15.730656

18.151631

19.547763

20.108567

21.357552

22.562173

23.638277

26.165218

26.780961

25.316863

25.792581

26.220979

26.610881

26.969160

27.300687

27.608863

27.897507

28.168655

28.623998

28.665982

28.895686

29.116267

29.322830

29.522239

29.713275

29.896669

30.072920

30.242773

30 606665

30 566557

30 717610

30 865323

31 078751

31 369051

31 606581

31.866990

32 077951

32 298510

32 509787

32 712686

32 908231

33 097165

33 613723

33 860380

36 263650

36 627815

36 997170

35 353659

35 697792

36 030387

36 351507

36 661075

-776.9550MP

1 225087

3 566017

4 153695

6 627661

5 911836

6 961206

7 767505

8 621523

8 973635

9.653866

9.883084

10.274929

10.639505

150.00

250.00

300.00

600.00

600.00

800.00

1000.00

1200.00

1600.00

1600.00

1800.00

2000,00

2200.00

2600.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

6000.00

6200.00

6600.00

6600.00

6800.00

5000.00

5200.00

5600.00

5600.00

5800.00

6000 O0

6400 O0

6800 O0

7200 00

7600 O0

8000 O0

8600 O0

8800 O0

9200 O0

9600 O0

10000 00

11000 O0

12000 00

13000 O0

16000 00

15000 O0

16000 O0

17000 O0

18000 O0

19000 O0

20000 O0

O.O000NT

3.695533

3.696580

3.697562

3.500268

5.520795

3.565697

3.626070

5.686171

3.766166

3.801608

3.851880

3.897210

3.937851

3.976675

6.007656

6.037356

4.064510

6.089286

6.112032

6.132952

6.I5227I

6.170200

6.186908

6.202507

6.217162

6.230958

6.266005

6.256662

6.268292

6.279683

6.290702

6.301608

6.322259

6.362868

6.363893

6.385969

6.609696

6.635687

6.666511

4.696666

6.532680

4.572315

6.690280

6.833386

6.996219

5.169865

5.563867

5.508373

5.655709

5.780927

5.881843

5.958662

200

300

371

500

700

900

ii00

1300

1500

1700

1900

2100

2300

371.OIOONT

.00 2.286366

00 2.610697

Ol 3.634635

00 3.665660

O0 3.647696

O0 3.612159

O0 3.585865

00 3,579377

O0 3.597666

00 5.663653

O0 3.718567

.00 3.823895

.00 3.960075

106.0000

17.166669

18.931886

19.569331

20.575957

21.998086

23.016599

23.818660

24.686733

25.057376

25.561323

26.012108

26.620208

26.793667

27.137828

27.657369

27.755656

28.036875

28.298032

28.566623

28.782265

29.006238

29.219715

29.623588

29.618708

29.805891

29.985596

30.158609

30.325259

30.686121

30.661670

30.791937

30 937586

31 215856

31 678689

31 727356

31 963887

32 189669

32 605225

32 612256

32 811606

33 003690

33 189287

33630472

36 066671

36 637660

36 816284

35 176821

35 527063

35 865511

36 i92399

36 507769

36 811633

26 0000

2 589529

3 580287

6 153695

5 263725

6 675610

7 387767

8 109853

8 707937

9 Z21169

9 673988

i0 083108

10 660170

10813856

NASAJTP-3287/REV 1 109
TABLE IV.- Continued.

EFDA NBIS

100.00

200.00

298.15

350.00

450.00

550.00

700 O0

900 QO

1100 O0

1300 O0

1500 O0

1700 O0

1900 QO

2100.00

2300 O0

2500 00

2700 O0

2750 O0

2900 O0

3100 O0

3300 00

3500 O0

3700 O0

3900 O0

4100 00

4300 O0

4500 00

4700 O0

4900 O0

5100.00

5300.00

5500.00

5700.00

5900.00

J12/73

0

1

2

2

2

2

2

2

2

2

3

3

3

3

3

3

3

4

4

4

4

4

4

q

4

4

4

4

4

4

4

4

4

HO/R

.939322

.731912

,i14184

.244613

.424410

,549759

.685151

,814892

.915385

.999668

.074384

.145953

,218786

.295272

.376862

.466037

.568_60

.773906

.735207

.689435

.649210

.613583

.581807

.553291

.527556

.504216

.482950

.463494

.445626

.429160

.413936

.399820

.386694

.374458

-630,3438MP

0.571050

1.500750

2,271403

2.620977

3.208153

3.707615

4.339075

5,030429

5.605381

6.099565

6.533879

6.923071

7,276961

7.602785

7.906184

8.191415

8.461954

8,527649

8.780153

9.094408

9.386322

9.658826

9.914311

10.154757

10.381820

10.596899

10.801184

10.995699

11.181330

11.358847

11.528926

11.692161

11.849078

12.000146

150.00

250.00

300,00

400 O0

500 O0

600 00

800 O0

1000 O0

1200 O0

1400 O0

1600 00

1800 O0

2000 00

2200 O0

2400 00

2600 00

2750 O0

2800 O0

3000 00

3200 O0

3400 O0

3600 00

3800 O0

4000 O0

4200 00

4400 O0

4600 O0

4800 00

5000 O0

5200 O0

5400 O0

5600 O0

5800.00

6000.00

O,O000NT

1.414395

1.955136

2.119588

2.343493

2.491788

2.600273

2.754973

2.867758

2.959184

3.037805

3.110225

3.181987

3.256476

3.335297

3,420276

3.514986

3.597299

4.760546

4.711558

4.668694

4.630873

4.597254

4.567174

4.540102

4.515608

4.493341

4.473010

4.454374

4.437228

4.421401

_.406747

4.39313g

4.380_70

4.368646

68

I

I

2

2

3

3

4

5

5

6

6

7

7

7

8

8

8

8

8

9

9

9

I0

I0

I0

i0

I0

Ii

ii

Ii

11

11

11

12

0000

047446

912680

284280

927533

467432

931561

702352

.329719

.860818

.323060

.733530

.i04007

,443012

.757118

.050875

.328286

.527649

.613547

.940281

.242960

.524840

.788563

.036304

.269869

._90779

.700323

.899605

.089575

.271059

.444778

.611365

.771379

.925316

.073619

110 NASA/TP-3287/REV 1
TABLE IV.- Continued.

EFDA NE1G

100.00

298,15

400.00

600,00

800.00

1000,00

1200.00

1400.00

1600.00

1800.00

2000 O0

2200 O0

2400 O0

2600 00

2800 O0

3000 O0

32O0 O0

5400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000 O0

5200 O0

5_00 00

5600 O0

5800 O0

6000 O0

6400 O0

6800.00

7200.00

7600.00

8000.00

8_00.00

8800.00

9200.00

9600.00

10000.00

11000.00

12000.00

13000.00

14000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

L10/90 HO/R

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2.500001

2.500008

2,500037

2.500129

2.500379

2.500943

2.502007

2.503778

2.505840

2.51O124

2.516583

-745.3750MP

12.368248

15.099315

15.833984

16.847647

17.566852

18.124711

18.580515

18.965892

19.299720

19.59_178

19 857579

20 095854

20 313383

20 513490

20 698759

20 871242

21 032588

21 184149

21327046

21 462214

21 590447

21 712422

21 828722

21 939852

22 046251

22.148306

22.246357

22.340708

22.431627

22.519356

22.60_110

22.765456

22.917017

23.059913

23,195082

23.323315

23.445290

23.561590

23.672720

23.779119

23.881174

24.119450

24.336980

24.537092

24.722380

24.89_904

25.056335

25.208051

25.351151

25.486741

25.615647

200.00

300.00

500.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600.00

7000.00

7400.90

7800.00

8200.00

8600.00

9000.00

9400.00

9800.00

10500,00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

O.O000NT

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500001

2.500004

2.500018

2.500070

2.500225

2.500615

2.501_35

2.502876

2.505229

2.507748

2.513042

i01.0000

14.101116

15.114779

16.391843

17.233024

17.861310

18.562986

18 780622

19 138374

19 451282

19 7293_6

19 979554

20 206984

20 415438

20.607840

20.786488

20.953216

21.109517

21.256618

21.3955_3

21.527152

21.652178

21.771248

21.884904

21.993617

22.097799

22.197812

22.293978

22.386581

22._75876

22.562092

22.68608_

22.842385

22.989486

23.128411

23.260020

23.385046

23.50_116

23.617772

23.726_85

23.830667

2_,003149

24.230580

2_._39037

24.631450

24.810125

24.976916

25.133337

25.280649

25.419834

25.551979

NASA/TP-3287/REV 1 111
TABLE IV. - Continued.

£FDA NIIS

i00.00

200.00

298.15

350.00

650.00

550.00

631.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1728.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.0O

3900,00

4100.00

6300.00

6500.00

4700.00

4900.00

5100.00

5300.00

5500.0O

5700.00

5900.00

J12/76 HO/R

0.610980

1.441456

1.930640

2.119187

2.409175

2.651006

2.845751

2.943220

3.119847

3.257504

3.379819

3.696939

3.613244

6.823514

4.810512

6.798072

6.787796

4.779163

6.771810

6.765470

6.759969

4.755097

6.750800

4.766967

6.743527

_.740423

6.737607

4.735062

4.732695

4.730540

_.728556

4.726717

6.725015

4.723631

6.721955

-575.6202MP

0.285525

0.988032

1.661875

1.986768

2.555760

3.063101

3.440028

3 740878

4 503212

5 142871

5 697206

6 189020

6 633782

6 693011

7.150084

7.630904

8.066918

8.465767

8.833290

9.176050

9.491679

9.789120

10.068784

10.332678

10 582485

10 819632

Ii 045342

II 260666

II 466518

Ii 663697

11.852904

12.034759

12.209810

12.378550

12.541418

150.00

250.00

300.00

400.00

5O0.00

600.00

631.00

800.00

1000.00

1200.00

14o000

1600 O0

1728 00

1800 00

2000 O0

2200 O0

2400 O0

2600 O0

2800 oo

3000 O0

3200 O0

3600 O0

3600 O0

3800 O0

4000 O0

4200 O0

6400 O0

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

0.000

1

1

1

2

2

2

2

3

3

3

3

3

3

4

4

4

6

4

4

4

6

4

4

4

4

Q

4

6

4

4

4

4

6

4

ONT

.079238

.717961

.937978

.273736

.532681

.767852

.845731

.039615

.191529

.319699

.438653

.554930

.629498

.817769

.803981

.792700

.783300

.775345

.768527

.762618

.757467

.752885

.748830

.765202

.761936

.738982

.736296

.733863

.731595

.729527

.727618

.725850

.724209

.722681

.721254

70.0000

0.625012

1.340789

1.673901

2.280110

2.816161

3.298651

5.640028

4.140442

6.835643

5.429103

5.969874

6.416556

6.693011

6.889798

7.396662

7.853984

8.270589

8.653134

9.006770

9.335558

9.642761

9.931040

10.202591

10.459248

10.702560

10.933847

11.154242

11.364724

11.566166

11.759257

11.94_715

12.123103

12.296941

12.660693

12.620774

112 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA 0 2G

I00.00

200.0O

298.15

350.00

500.00

700.00

900.00

Ii0O.00

1300 O0

I500 O0

1700 O0

1900 O0

2100 O0

2300 O0

2500 O0

2700 O0

2900 O0

3100 O0

3300.00

3500.00

3700,00

3900.0O

4100.00

4300,00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600.00

7000.00

7400.O0

7800,00

8200.00

8600,00

9000.00

9400.00

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

TPIS89 HO/R

3.489123

3.495137

3.501495

3.508882

3.551665

3.639121

3.731674

3.815719

3.888800

3.952255

4.0O8278

4.058711

4.1O4921

4.147958

4.188487

4,226976

4.263723

4.298872

4.332639

4 365021

4 396145

q 426051

4 454828

4 482523

4 509199

4 534936

4.559775

4.583750

4.606892

4.629290

4.650898

4.671734

4.701593

4.738615

4.772369

4.802587

4.829089

4.851715

4.870390

4.885080

4.895871

4.902860

4.906548

4.895189

4.867992

4.829019

_.781777

4.729123

4.673267

4.615849

4.558078

4.5O0793

-I043.9706MP

17.354809

19.775907

21.172174

21.734160

22.992010

24.200377

25.126177

25.883321

26.526828

27 087951

27 586146

28 034727

28 443149

28 818542

29 166134

29 489908

29 793293

30 078914

30 348596

30 604508

30 847967

31 080137

31 302249

31 515100

31 719469

31 916117

32.105605

32.288500

32.465252

32.636372

32.802030

32.962807

33.195264

33.490436

33.770234

34.036248

34.289742

34.531837

34.763330

34.985097

35.197774

35.401984

35.740474

36.186379

36.593639

36.966851

37.310205

37.627460

37.921458

38.194766

38.449664

38.688081

150.00

250.00

300.00

400.00

600.00

800 O0

i000 O0

1200 O0

1400 00

2600 O0

1800 00

2000 O0

2200 O0

2400 O0

2600 O0

2800 00

3000 O0

3200 O0

34O0 O0

3600 O0

3800 O0

4000 O0

4200 O0

4400 O0

4600 00

4800 O0

5000.00

5200.00

5400,00

5600.00

5800.00

6000.00

6400.00

6800.00

7200.00

7600.00

8000.00

8400.0O

8800.00

9200.00

9600.00

i0000.00

11000.00

12000.00

13000.00

14000.00

15000 O0

16000 O0

17000 O0

18000 00

19000 DO

20000 O0

O.O000NT

3.493373

3.497638

3.501952

3.519793

5.593159

3.686070

3,775012

3.853551

3.921591

3.981115

4.034094

4.082250

4.126789

4.168466

4.2O7940

4.245555

4.281482

4.315926

4.349005

4.380748

4.411238

4.440574

4.468805

4.495973

4.522191

4.547451

4.571846

4.595428

4.618198

4.640180

4.661413

4.681872

4.720513

4.755917

4.787922

4.816305

_.840888

4.861554

4.878223

4.890959

4.899827

4.904978

4.903109

4.883299

4.849736

4.806234

4.755976

4.701484

4.644665

4.586949

4.529334

4.472524

104.0000

18.770264

20.556023

21.193606

22.203259

23.643049

24.689365

25.521715

26.217014

26.816249

27.343898

27.815911

28.243435

28.634645

28.995523

29.330820

29.644041

29.938144

30.215569

30.478241

30.727696

30.965415

31.192382

31.409748

31.618315

31.818692

32 011727

32 197811

32 377611

32 551487

32 719897

32 883043

33 04143O

33.344846

33 632134

33 904901

34 164452

34 412168

34 648886

34 875410

35 092636

35 300981

35.50ii36

35,968583

36,394555

36,784126

37,142022

37.471915

37.777177

38.060470

38.324334

38.570778

38.801623

NASA/TP-3287/REV 1 113
TABLE IV.- Continued.

EFDA P IS

100.00

195.40

200.00

220.00

240.00

260.00

280.00

298.15

317.30

400.00

600.00

800.00

1000.00

1200.00

1400 O0

1600 O0

1800 O0

2000 O0

220O O0

240O O0

2600 O0

2800.00

3000.00

3200.00

3400.00

3600.00

3800 O0

400000

4200 O0

4400 O0

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600.00

5800.00

6000.00

TPIS89 HO/R

1.068012

1.559100

1.894880

1.956601

2.014049

2.067748

2.118500

2.162187

2 206055

2 597605

2 778902

2 869550

2 923939

2 960199

2.986098

3.005523

3.020631

3.032718

3.042607

3.050847

3.057820

3 063797

3 068977

3 073510

3 077509

3 081064

3 084244

3 087107

3 089697

3 092051

3.094201

3.096172

3.097985

3.099658

3.101208

3.102647

3.103986

3.105237

-644.6561MP

1.061037

1.927095

1.970772

2.154284

2.526916

2.490428

2.645582

2.779776

2.915678

3.501544

4.594014

5.407117

6.053733

6.590256

7.048600

7.448665

7.803570

8.122474

8.412001

8.677106

8.921587

9.148420

9 359981

9 558196

9 744649

9 920657

10 087328

10 2456O3

10.396288

10.540076

10.677571

10.809301

10.935730

11.057268

11.174280

11.287090

11.395990

11.501241

317.3000NT

1.533412

1.879783

1.926638

1.986051

2.041251

2.093618

2.142909

2.166494

2.455847

2.706385

2.830701

2.899767

2.943717

2.974145

2.996458

3.013522

3.026993

3.037898

3.046906

3.054475

3.060920

3.066477

3.071316

3.075570

3.079337

3.082697

3.0857'12

3.088433

3.090901

3.093150

5.095207

3.097097

3.098838

3.I00_48

3.101940

3.103328

3.104622

150.00

195.40

210.00

230.00

250.00

270.00

290.00

300 O0

317 30

500 O0

700 O0

900 O0

II00 O0

1300 O0

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700 O0

2900 O0

3100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500 O0

4700 O0

4900 O0

5100.00

5300.00

5500.00

5700.00

5900:00

75.0000

1.545531

1.927055

2.063616

2.241618

2.409763

2.568834

2.720596

2.793149

2.915678

4.093770

5.026478

5.746916

6.533371

6.827744

7.254981

7.631117

7.967061

8.270568

8.547347

8.801722

9.037049

9.255980

9.460651

9.652805

9.833885

10.005098

10.167462

10.321849

10.469004

10.609575

10.744126

10.873151

10.997087

11.116319

11.231191

11.342011

11.449056

114 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA

EFDA

PBIS

I00.00

298.15

350.00

450.00

550.00

600.65

700.00

900.00

II00,00

1300.00

1500.00

1700.00

1900,00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

RBlS

100.00

250.00

300.00

312.47

500.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

TPIS91 HO/R

2.123998

2,771311

2,841075

2.952299

3.064940

3.087399

5,996166

3.909447

3.841007

3.785008

3.739113

3.702049

3.6?2925

3.651005

3,635615

3.626113

3,621868

3,622258

3.626659

3,634652

3.645015

CODAS9 HO/R

2.416258

2.913661

3.025634

3.901025

3.831855

3.783747

3,76_I02

5.768877

3,802343

3.874351

3.996769

6.183049

6.467417

-826.2666MP

2,313907 200

5.022293 300

5.472222 400

6.200129 500

6.801783 600

7,071885 600

7.687729 800

8.681085 1000

9.458720 1200

10.095676 1400

10.635997 1600

11.099658 1800

11.509741 2000

11.876204 2200

12.207606 2400

12.510320 2600

12.789197 2800

13.048000 3000

13.289698 3200

13.516665 3400

13.750811 3600

-900.7145MP

3.231459 200

5.687527 298

6.232037 312

6.556112 400

8.174986 600

9.455759 800

10.403900 1000

11.159243 1200

11.791120 1400

12,559713 1600

12.831525 1800

13.285569 2000

15.716491

600.6500NT

,00 2.579226

.00 2.775995

.00 2.899734

.00 3.000340

.00 3.086869

.65 4.050934

.00 3.949855

.00 3.873443

.00 3.811638

.00 3,760891

.00 3.719538

.00 3.686542

.00 3.661107

.00 3.642534

.00 3.630167

.00 5.623372

.00 3.621525

.00 3.623996

,00 3,630170

.00 3.639426

.00 3.651141

312._700NT

.00 2.802550

.15 3.021011

.47 3.057311

.00 3.869140

.00 3.803391

.00 3.770968

.00 3.763501

.00 3.781462

.00 3.832800

.00 3,928449

.00 4.081018

.00 4.304583

42

3

5

5

6

7

7

8

9

9

i0

10

Ii

Ii

12

12

12

12

13

13

13

13

25

5

6

6

7

8

9

I0

11

12

12

15

13

.0000

.957058

.039446

.855503

.513705

.068543

.071885

.218261

.091089

.791651

.375278

.87_677

.310793

.697829

.045847

.562216

.652481

.920906

.170826

._04893

.625234

.833579

.0000

.0_5637

.213447

.356112

.316005

.871198

.960088

.800396

.487668

.073970

,591346

.062385

.503201

NASA/TP-3287/REV 1 115
TABLE IV. - Continued.

EFDA

EFDA

S IS

I00.00

298.15

368.30

388.36

400.00

432.25

500.00

600.00

700.00

800.00

1000.00

1200.00

1400.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600 O0

3800 O0

4000 O0

420O O0

4400 O0

46O0 O0

4800 00

5000 O0

5200 O0

5400 00

5600 O0

5800 O0

6000 O0

SIIS

100 O0

250 O0

300 00

500 O0

700 O0

900 O0

1100 00

1300 O0

1500 O0

1690 O0

1700 O0

1900 O0

2100 O0

2300 00

250O O0

2700 O0

2900 O0

3100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

TPISB9 HO/R

0.829875

1.779771

1.979437

2.156844

2.724038

2.831352

3.126089

3.322816

3.423112

3.476904

3.551262

3.600834

3.636242

3.662799

3.683454

3.699978

3.713497

3.724764

3.734297

3.742468

3.749550

3.755746

3.761214

3.766O74

3.770422

3.774335

3.777876

3.781095

3.784034

3.786728

3.789207

3.791495

3.793613

3.795581

3.797412

3.799121

TPIS91 HO/R

0.321125

1.108905

1.304604

1.846894

2.158976

2.364789

2.515707

2.634921

2.734246

2.816240

6.371177

6.044884

5.780741

5.562537

5.379245

5.223107

5.088506

4.971273

4.868250

4.777000

4.695616

4.622579

4.556667

4.496887

4.442420

4.392589

4.346826

4.304652

4.265661

4.229506

4.195887

4.164549

-530.6386MP

0.678452

2.077342

2.074199

2.587128

2.667065

2.881791

3.317841

3.907455

4.428001

4.888795

5.673248

6.325376

6.883246

7.37O611

7.803267

8.192243

8.545543

8 869157

9 167684

9 444731

9 703182

9 945375

10 173233

10 388358

10 592098

10 785596

I0 969834

Ii 145656

Ii 313798

ii 474903

II 629536

II 778196

Ii 921329

12 059330

12 192554

12.321321

-386.9706MP

0.I39275

0.751818

0.972450

1.779554

2.454722

3.023609

3.513463

3.943704

4.327931

4.658918

4.696560

5.386716

5.978270

6.494078

6.950104

7.358051

7.726422

8.061829

8.369381

8.655120

8.916295

9.161551

9.391066

9.606656

9 809848

I0 001936

i0 184O26

10 357073

10 521903

i0 679234

I0 829700

I0 973857

200 O0

300 O0

368 30

388 36

428 15

453 15

550 O0

650 O0

717 O0

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

4100.00

4300.00

4500,00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

388.3600NT

1,402368

1.786030

2.110387

2.689823

2.810107

2.951660

3.242931

3.381097

3.433849

3 518214

3 578301

3 619900

3 650406

3 673734

3 692150

3 707059

3 719375

3 729721

3 738534

3 746131

3 752708

3 758563

3 763713

3 768306

3 772429

3 776149

3 779523

3 782597

3 785410

3 787993

3.790373

3.792574

3.794615

3.796512

3.798281

1690.O000NT

200.00 0.867760

298.15 1.297906

400.00 1.616762

600.00 2.021476

800.00 2.270963

1000.00 2.445277

1200.00 2.578371

1400.00 2.686570

1600.00 2.778638

1690.00 6.389519

1800.00 6.198967

2000.00 5.906209

2200.00 5.666680

2400.00 5.467072

2600.00 5.298174

2800.00 5.153403

3000.00 5.027936

3200.00 4.918152

3400.00 4.821283

3600.00 4.735178

3800.00 4.658136

4000.00 4.588799

4200.00 4.526065

4400.00 4.069035

4600.00 4.416963

4800.00 4,369231

5000.00 4.525317

5200.00 4.284781

5400.00 4.247248

5600.00 4.212396

5800.00 4.179948

6000.00 4,149663

71 0000

1 443140

2 087916

2 474199

2 587128

2 855108

3 018379

3 621664

4 175842

4 510313

5 300796

6 013028

6 614370

7 134615

7 593002

8.002658

8.372940

8.710746

9.021311

9.308698

9.576120

9.826182

I0,060989

10.282297

10.491575

10.690062

10.878817

ii 058749

II 230645

II 395193

II 552996

II 704584

II 850428

II 990948

12.126518

12,257476

60.0000

0.534247

0.964400

1.392804

2.132395

2.750560

3.277031

3.735095

4.140930

4,505828

4.658918

5.055758

5.693191

6.244516

6,728772

7,159522

7.546728

7,897898

8,218813

8.514008

8.787101

9.041017

9.278155

9,500500

9,709716

9.907206

10.094168

10.271626

10.440468

10.601464

10.755289

10,902535

11.043726

116 NASA/TP-3287/REV l
TABLE IV.- Continued.

EFDA

EFDA

SNIS

I00 00

298 15

350 O0

45O O0

505 12

600 00

800.00

I000 O0

1200 O0

1400 O0

1600 O0

1800 O0

2000 00

2200 O0

240O 00

2600 00

2800 O0

3000 00

3200 00

3400 00

3600 O0

3800 O0

4000 O0

4200 O0

4400 00

4600 00

5900 O0

SRIS

100.00

140.00

180.00

220.00

260.00

298.15

550.00

450.00

600.00

800.00

820.00

i000.00

1041.00

1200.00

1400.00

1600.00

1800.00

2000.00

2290.00

2400.00

2600.00

2800.00

3000,00

3200.00

5400.00

5600.00

3800.00

4000,00

4200,00

4400.00

4600.00

4800,00

5000,00

5200.00

5400,00

5600.00

5800.00

6000.00

TPIS91 HO/R

1.585181

2.550655

2.664533

2.845360

2.935187

4.464875

4.199065

4.032038

5.920980

3.844192

3.789727

3.750511

3.722107

3.701592

3.686967

3.676819

3.670120

3.666106

3.664196

5.663942

3.664993

5.667067

3.669940

3.673428

3.677378

3.681666

4.658883

SRD 92 HO/R

1.790767

2.111676

2.315215

2.457789

2.564304

2.645569

2.736562

2.872478

3.021667

3.169154

3.306562

3.364875

4.301721

4.321375

4.339757

4.353544

4.364267

4.372845

4.379864

_.385713

4.390662

4.394904

4.398581

4.401798

4.404636

4.407159

4.409417

4.411449

4.413287

4.414958

_.416484

6.417882

4.419169

4.420357

6.421457

4.422478

4.423429

4.424316

-760,4778MP

1.303745

5.604849

4.022452

4.714676

5.048560

5.832700

7.077606

7.995320

8.719983

9.518290

9.827852

10.271829

10.665435

11.019174

11.340590

11.635278

11.907496

12.160558

12.397092

12.619217

12.828667

13.026874

13.215040

13.394179

13.565157

13.728716

15.631127

-788.7764MP

1 498681

2 156898

2 713770

3 192956

3 612575

5 9692?3

6 400805

5 105768

5 953693

6 844167

6 922579

7 584461

7 719919

8 332795

9 000391

9 580826

10 094245

10 554524

10 971641

II 552997

ii 704242

12 029784

12 553130

12 617113

12 884057

13 135892

13 374236

13 600462

13 815745

14 021088

16 217375

16.405369

14.585742

16.759088

16.925935

15.086751

15.241959

15.591935

505.1180NT

200.00 2.249080

300.00 2

400.00 2

500,00 2

505.12 4

700.00 4

900.00 4

ii00.00 3

1300 O0 3

1500 O0 3

1700 00 S

1900 O0 3

2100 00 3

2300 O0 3

2500 00 3

2700 O0 3

2900 00 3

3100 OO 3

3300 OO 3

3500 O0 3

3700 O0 3

3900 00 3

4100 O0 3

4300 O0 3

4500 00 3

4700 O0 3.683904

6000 O0 4.660340

IO_I.0000NT

120 00 1.972085

160 O0 2.223392

200 00 2.592197

240 O0 2,514509

280 O0 2.608748

500 00 2.649151

400 00 2.809660

500 O0 2.927651

700 O0 3.100586

820 OO 5.181890

900 O0 3.333208

1041 O0 3.377443

Ii00 00 4.309677

1300 00 4.331273

1500 00 4.347110

1700 00 4.359221

1900 O0 4.368782

2100.00 4.376522

2300 O0 4.382916

2500 O0 4.388287

2700 O0 4.392862

2900 O0 4.396806

3100 00 4.400241

3300 00 4.403260

3500 00 4.405954

3700 00 4.408319

3900 O0 4.410459

4100 O0 4.412390

4300.00 4.414142

4500 O0 4.415738

4700 O0 4._17198

4900 O0 4.418539

5100 O0 4.419775

5500 O0 4.420917

5500 00 4.421977

5700 O0 4.422962

5900 DO 4,423880

.555372

.759032

.926951

.648420

.315558

.106581

.971184

.879202

.814692

.768535

.735167

,711005

.693643

,681405

.673091

.667817

.664918

.663886

.664324

.665917

.668416

.671617

.675353

.679487

52.0000

2.642369

3.620338

4.384865

5.018817

5.048560

6.509258

7.566643

8.376665

9.032129

9.582477

10.056950

10.474187

10.846761

11.183536

11.490983

11.773970

12.036243

12.280748

12.509859

12.725431

12.929096

13,122145

13.305681

13.480639

13.647822

13.807919

15.709441

75,0000

1.841990

2.446424

2.961800

3.409300

3.804266

3.985653

4.771125

5.611328

6.425568

6.922579

7.231620

7,719919

7.957288

8.679091

9.500060

9.844931

10.330330

10.767967

Ii.166402

11.532083

11.869989

12.184041

12,477386

12.752586

13.011755

15.256659

13.488786

13.709404

13.919600

14,120313

16.312364

14.496469

14.673259

14,843293

15.007070

15.165032

15,317579

NASA/TP-3287/REV 1 117
TABLE IV.- Continued.

EFDA

EFDA

TAIS

100.00

200.00

298.15

350.00

450.00

550.00

700.00

900.00

1100.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3258.00

3300.00

3500.00

3700.00

3900.00

4100.00

4300.00

4500.00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

THIS

100.00

298.15

400.00

600.00

800.00

1000.00

1200.00

1400.00

1600.00

1650.00

1800.00

2000.00

2023.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600 O0

4800 oo

5000 O0

5200 O0

5400 O0

5600 O0

5800 O0

6000 O0

J12/72 HO/R

1.196703

1.952611

2.291677

2.405777

2.561787

2.672218

2.793739

2.906565

2.989298

3.059619

3.119687

3,169512

3.217520

3.268354

3.321485

3.377854

3.639369

3.508822

3.589566

3,663708

5.013881

5.014926

5.015858

5.016696

5.017469

5.018133

5.018757

5.019328

5.019852

5.020535

5.020781

5.021195

5.021580

5.021939

CODAB9 HO/R

1.675386

2.561547

2.725657

2.937836

3.096995

3.235308

3.363197

3.685301

3.603790

3.888128

3.928073

5.997169

4,826532

4.883330

6.937428

6.983202

5.022438

5.056661

5.086195

5,112448

5.135784

5.156664

5.175655

5.192457

5.207916

5.221026

5.234962

5.266864

5.257850

5,268022

5.277467

5.286261

5.296469

-683.2634MP

0.744842

1.846290

2.696110

3.072838

3.697632

4,222957

4.882239

5.598807

6.190638

6.695616

7.137803

7.531619

7.886562

8.210976

8.510721

8.789911

9.052167

9.300351

9.537006

9.717223

9.781444

10.076495

10.355199

10.619275

10.870181

11.109169

11.337319

11.555573

11.764753

11,965584

12.158706

12.344690

12.524066

11.697225

-763.7251MP

1.309037

3.672134

6.449270

5,597684

6.465204

7.171639

7.772757

8.300481

8.773608

8.886869

9.224837

9.662120

9.687889

10.095133

10.522626

10.919488

11.290254

11.637953

11.965259

12.274612

12.567304

12.845551

13.110540

13.363669

13.605385

13.837202

14.059726

14.273672

14.679675

14.678301

16.870059

15.055608

15.234760

150.00

250.00

300.00

600.00

500.00

600,00

800.00

1000.00

1200.00

1400.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3258.00

3400.00

3600.00

3800.00

6000.00

6200.00

6600.00

6600.00

6800.00

5000.00

5200.00

5600.00

5600.00

5800.00

6000.00

O.O000NT

1.661353

2.151620

2.296387

2.691728

2.620960

2.717338

2.855550

2.950144

3.025634

3.091154

3.145480

3.193146

3.242584

3.294624

3.369165

3.607805

3.472887

3.547573

3.635286

5.013665

5.014619

5.015405

5.016287

5.017081

5.017799

5.018452

5.019049

5.019595

5.020098

5.020562

5.020992

5.021391

5.021763

5.022110

2023.0000NT

200.00

300.00

500.00

700.0C

900.00

Ii00.00

1300.00

1500.00

1650.00

1700.00

1900.00

2023.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

5500.00

3700.00

3900.00

4100.00

4300.00

6500.00

6700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900.00

2.297189

2.565395

2.842260

3.021053

3.167822

3.300145

3.426875

3.564967

3.633006

3.900127

3.960673

6,006063

6.852618

4.911555

4.961230

5.003546

5.040026

5.071798

5.099719

5.124649

5.166506

5.166300

5.186164

5.200565

5.215127

5.228632

5.241036

5.252466

5.263032

5.272830

5.281941

5.290435

68.0000

1.325356

2.306525

2.710282

3.399900

3.970669

4.457469

5.259540

5.907504

6.652016

6.923507

7.340045

7.713330

8.052268

8.363670

8.652625

8.923048

9.177888

9.419998

9.651606

9.717223

9.931132

10.217776

10,488969

10.746292

10.991096

11.224557

11.467629

11.661250

11.866170

12.063071

12.252557

12.635166

12.611380

12.781631

65.0000

2.699O17

3.687770

5.070776

6.056813

6.836210

7.682932

8,064352

8,562817

8.884869

9.001176

9.438072

9,687889

9.868676

10.312838

10.726471

11.107942

11.466809

11.806006

12.121979

12.422784

12.708167

12.979626

13.238643

13 685746

13 722503

13 949579

14 167730

14 377630

16 579877

14.775009

14.963508

15.145809

118 NASA/TP-3287/REV 1
TABLE IV. - Continued.

EFDA

EFDA

TIIS

I00.00

298.15

qO0.O0

600.00

800.00

1000.00

1156.00

1200.00

1400.00

1600.00

1800.00

1944 O0

2000 00

2200 00

2400 O0

2600 O0

2800 O0

3000.00

3200.00

3400.00

3600.00

3800,00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

U 15

100.00

298.15

400.00

600.00

800.00

942.00

I000.00

1049.00

1200.00

1400.00

1408.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

CODA89 HO/R

0.672319

1,945969

2,240361

2,590852

2.829692

3,012204

3,220388

3.607849

3,607205

3.651298

3.728689

3.800931

4.730085

4.811779

4 879857

4 937461

4 986836

5 029628

5 067071

5 100109

5 129476

5 155751

5 179400

5.200796

5.220246

5.238006

5.254285

5,269263

5.283088

5.295889

5.307775

5.318842

5.329171

CODA89 HO/R

1.562329

2.567194

2.791806

3.145104

3.500056

3.782084

4.192851

4.777514

4.755983

_.734615

5,478750

5.512953

5.546662

5.579643

5.612532

5.645652

5.679089

5.712904

5.747102

5.781609

5.816479

5.851651

5.887108

5.922808

-580.1905MP

0.317397

1.748777

2.364962

3.345757

4.125378

4.777070

5.226652

5.361531

5.916988

6.401129

6.855375

7.125028

7.258994

7.713775

8.135459

8.528392

8.896149

9.241699

9.567525

9.875725

10.168087

10.446140

10.711207

10.964437

11.206834

Ii.439281

II,662557

II.877356

i2.084293

12.283921

12.476738

12.663190

12.843683

-765.4089MP

1 172649

3 470444

4 257677

5 458049

6 410570

7 004480

7.25S352

7.454948

8.095968

8.827417

8.854392

9.556967

10.208205

10.794262

11.327612

11.817433

12,270615

12.692750

13.088043

13.460054

13.811617

14.145078

14.462377

14.765242

19_4.00

200.00

300.00

500.00

700.00

900.00

Ii00.00

1156.00

1300.00

1500.00

1700.00

1900.00

1944.00

2100.00

2300 O0

2500 O0

2700 O0

2900 O0

3100 O0

3300 O0

3500 O0

3700 O0

3900 O0

4100 O0

4300 O0

4500 00

4700.00

4900.00

5100.00

5300.00

5500.00

5700.00

5900,00

OONT

1.489565

1.952410

2.438388

2.718312

2.926477

5.126755

3.615745

3.600934

3.624507

3.686327

3.777543

4.704199

4.772877

4.847298

4.909811

4.963063

5.008970

5.048953

5.084090

5.115212

5.142969

5.167879

5.190359

5.210747

5.229323

5.246319

5.261927

5.276311

5.289609

5.301940

5.313406

5.324094

1408.0000NT

200.00

300.00

500,00

700.00

900.00

942,00

1049.00

ii00.00

1300.00

1408,00

1500,00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700,00

3900.00

2.247878

2.571809

2.974078

3 318124

3 695414

4 137026

4 235202

769581

4 744477

4.733886

5.495533

5.529950

5.563198

5.596069

5.629028

5.6623_2

5.695933

5.729950

5.764311

5.799026

5.834035

5.869355

5.904938

65.0000

1.060676

1.760978

2.887362

3.754950

4.464458

5.069298

5.226652

5.650002

6.166449

6.623481

7.038247

7.125028

7.490828

7.928462

8.335280

8.715219

9 •071535

9. 406938

9.723710

10.023785

10.308815

10.580221

10,839236

11.086932

11.324250

11.552020

11.770976

11.981771

12.184988

12.381152

12.570733

12.754157

47 0000

2 502853

3 486395

4 900710

5 955784

6 834010

7 004480

7 454948

7 681560

8.476183

8.854392

9.201665

9.891644

10.508585

11.066969

11.577518

12.048263

12.485295

i2.893517

13.276859

13.638199

13.980482

i_.305616

14.615574

NASA/TP-3287/REV 1 119
TABLE IV,- Continued,

EFDA

EFDA

V IS

I00.00

200.00

298.15

350.00

450.00

550.00

700.00

900.00

II00.00

1300.00

1500.00

1700,00

1900.00

2100.00

2190.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.80

4100.00

4300.00

4500.00

4700.00

4900.00

5100,00

5300.00

5500.00

5700.00

5900.00

N IS J

I00.00

200.00

298.15

350.00

450.00

550.00

700.00

900.00

II00.00

1300.00

1500.00

1700,00

1900.00

2100.00

2300.00

2500.00

2700.00

2900 O0

3100 O0

3300 O0

3500 O0

3680 O0

3700 00

3900 O0

4100 O0

4300 00

4500 O0

4700 O0

4900 O0

5100.00

5300.00

5500.00

5700.00

5900.00

J 6/73 HO/R

0.588128

1 398158

1 871744

2 045306

2 291042

2 463382

2 647351

2 825582

2 969945

3 101344

3 229695

3 357490

3 488132

3 624874

4 944_21

4 973720

5 020385

5 060136

5 094405

5 124252

5 150481

5 173713

5 194433

5 213027

5 229808

5 245028

5 258895

5 271581

5 283233

5 293970

5 303897

5 313102

5 321661

5 329639

6/66 HO/R

0.784171

1.599613

2.006074

2.144959

2.334072

2.464257

2.605710

2.737918

2.842894

2.932316

3.012725

3.087515

3.158587

3.227233

3.294241

3.360054

3.425872

3.500859

3.593989

3.712021

3.860240

4.031585

5.183524

5.137053

5.095116

5.057080

5.022425

4.990719

4.961602

4.934768

4.909959

4.886955

4.865565

4.845625

-558.0605MP

0.276023

0.954115

1.608437

1.922697

2.468229

2.945595

3.562275

4.250000

4.831357

5.338360

5.791161

6 203146

6 583659

6 939429

7 092922

7 335959

7 752649

8 140572

8.503403

8.844162

9.165361

9.469108

9.757191

10.031139

10.292268

10,541719

10.780488

11.009450

11,229375

11.440949

11.644780

11.841415

12.031342

12.215005

-598.1110MP

0.371880

1.199469

1.921999

2.254939

2.818607

3.300244

3.911647

4.583019

5.142904

5.625254

6.050587

6.432228

6.779581

7.099052

7.395625

7.673068

7.934148

8.181489

8.417903

8.646134

8.868713

9.866419

9.094527

9.366173

9.622022

9.863780

10.092893

10.310599

10.517965

10.715915

10.905257

11.086699

11.260868

11.428317

150.00

250.00

300.00

400.00

500.00

600.00

800.00

1000.00

1200.00

1400.00

1600.00

1800.00

20OO.00

2190.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600.00

3800.00

4000.00

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

150.00

250.00

300.00

400.00

500.00

600.00

800.00

1000.00

1200.00

1400.00

1600.00

1800.00

2000.00

2200.00

2400.00

2600.00

2800.00

3000.00

3200.00

3400.00

3600 00

3680 O0

3800 oo

4000 OO

4200 O0

4400 O0

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600.00

5800.00

6000.00

O.O000NT

1.041553

1.668890

1.878643

2.180225

2.384025

2.532320

2.742495

2.900472

3.036459

3 165722

3 293414

3 422197

3 555531

3 689806

4 947206

4 998024

5 041025

5 077885

5 109826

5 137776

5 162439

5 184360

5 203975

5 221628

5.237599

5.252119

5.265376

5.277528

5 288709

5 299029

5 308584

5 317457

5 325719

5 333429

O.0000NT

1 266862

1 836308

2 011744

2 2_9682

2 404471

2 516284

2 675894

2 792949

2 889026

2.973459

3.050691

3.123455

3.193153

3.260893

3.327266

3.392540

3.461505

3.544607

3.649681

3.781695

3.950356

5.188449

5.159677

5.115560

5.075645

5.039358

5.006227

4.975857

4.947916

4.922125

4.898244

4.876069

4.855423

4.836154

68.0000

0.603283

1.296408

1.620059

2.204760

2.714532

3.162904

3.922119

4.551681

5.092703

5.570571

6.001541

6.396903

6.764379

7.092922

7.115454

7.548160

7.949959

8.324922

8.676374

9.007067

9.319297

9.615007

9.895846

10.163231

10.418388

i0.662382

10.896144

11.120497

11.336166

11.543797

11.743965

11.937188

12.123931

12.304612

68.0000

0.786416

1.583136

1.934369

2.548316

3.068130

3.516904

4.264142

4.874370

5.392280

5.844018

6.246189

6.609770

6.942502

7.250009

7.536634

7.805474

8.059439

8.300950

8.532877

8 757950

8 978728

9 066419

9 232443

9 495959

9 744566

9 979835

I0 203101

10 415514

i0 618064

10 811616

i0 996925

11.174657

11.345400

11.509678

120 NASA/Tp13287/REV 1
TABLE IV.- Continued.

EFDA XEIG

I00.00

298.15

400.00

600.00

800.00

I000.00

1200.00

1400.00

1600.00

1800 O0

2000 O0

2200 O0

2400 00

2600 O0

2800 O0

3000 00

3200 O0

3400 O0

5600.00

3800.0O

4000.00

4200 O0

4400 O0

4600 O0

4800 O0

5000 O0

5200 oo

5400 O0

5600 O0

5800 00

6000 O0

6400 O0

6800.00

7200.00

7600.00

8000.00

8400.00

8800.00

9200.00

9600.00

10000.00

11000.00

12000.00

13000.00

14000.00

15000.00

16000.00

17000.00

18000.00

19000.00

20000.00

L12/91 HO/R

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2,500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500001

2.500001

2.500002

2.500004

2.500015

2.500044

2.500116

2.500274

2.500594

2.501197

2.502266

2.504055

2.506911

2.511280

2.532748

2.579091

2.665269

2.806968

3.016588

5.297365

5.64177O

_.029344

_._51852

4.819852

-745.3750MP

15.177545

17.908412

18.643081

19.656744

20.575949

20.935808

21.589612

21.774989

22.108817

22.405275

22.666676

22.904952

23.122480

23 522587

23 507857

23 680339

25 841685

25 995247

24 13614S

24 271311

24 399544

24 521519

24.637819

24.748949

24.855348

24.957403

25.055455

25.149806

25.240725

25.328455

25.413207

25.574554

25.726117

25.869017

26.004195

26.132450

26.254467

26 5708_6

26 482112

26 588739

26 691159

26 931371

27 153505

27.563026

27.565342

27.765733

27.9690O0

28.178956

28.397942

28.626581

28.863890

200.00

300.00

500.00

700.00

900.00

ii00.00

1300.00

1500.00

1700.00

1900.00

2100.00

2300.00

2500.00

2700.00

2900.00

5100.00

5300.00

3500.00

3700.00

3900 O0

4100 00

4300 O0

4500 O0

4700 O0

4900 O0

5100.00

5300.00

5500.00

5700.00

5900.00

6200.00

6600.00

7000.00

7400,00

7800.00

8200.00

8600.00

9000.00

9400.00

9800.00

10500.00

11500.00

12500.00

13500.00

14500.00

15500.00

16500.00

17500.00

18500.00

19500.00

O,O000NT

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2 500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.500000

2.5O0000

2.500000

2.500000

2 500000

2 500000

2 500000

2 500001

2 500002

2 500003

2 500008

2 500026

2 500075

2.500180

2.500407

2.500850

2.501659

2.505051

2.505324

2.508874

2.519728

2.551932

2.616194

2.728276

2.902723

3.148136

3,462649

3,831814

4.230620

4.629336

i01.o0o0

16.910215

17.923876

19.200940

20.042121

20.670407

21.172084

21.589719

21.947471

22.260579

22.538443

22,78865i

23.016081

23.224535

23 416938

23 595585

23 762515

23 918616

24 065716

24 204640

24 536250

24 _61276

24 580566

24 696002

24.802714

24.906896

25.006909

25.103075

25.195678

25.284974

25,371189

25.495182

25.651484

25.798588

25.957519

26.069143

26.194199

26.313527

26.427087

26.535978

26.640450

26.813874

27.064355

27.259505

27.46_749

27.665461

27.866739

28.072956

28.287261

28.511083

28.744266

NASAFFP-3287/REV 1 121
TABLE IV.- Concluded.

EFDA

EFDA

ZNIS

100.00

298.15

400.00

600.00

692.73

800.00

1000 00

1200 O0

1400 O0

1600 O0

1800 O0

2000 O0

2200 O0

2400 O0

2600 O0

2800 O0

3000 O0

3200 O0

3400 O0

3600 O0

3800 O0

4000 O0

4200 O0

4400 O0

4600 O0

4800 O0

5000 O0

5200 O0

5400 O0

5600.00

5800.00

6000.00

ZRIS

100.00

200.00

298.15

350.00

450.00

550.00

700.00

900.00

1100 O0

1135 O0

1300 O0

1500 O0

1700 O0

1900 O0

2100.00

2125.00

2300.00

2500.00

2700.00

2900.00

3100.00

3300.00

3500.00

3700.00

3900.00

4100.00

4300 O0

4500 O0

4700 O0

4900 O0

5100 O0

5300 O0

5500 O0

5700 O0

5900 O0

CODA89 HO/R

1.197906

2.281995

2.492029

2.756627

4.135493

4.087360

4.025194

3.983750

3.954147

3.931945

3.914677

3.900862

3.889559

3.880140

3.872170

3.865339

3.859418

3.854238

3.849667

3,845604

3.841968

3.838696

3.835736

3.833045

3.830588

3.828335

3.826263

3.824350

3.822579

3.820935

3.819404

3.817974

J 6/79 HO/R

1.065607

1.851582

2.217452

2.341861

2.514480

2.638323

2.781025

2.937702

3.084422

3.535563

3.523127

3.524361

3.543274

3.579601

3.633293

_.825243

4.840987

4.856281

4.869310

4.880541

4.890324

4.898920

4.906534

4.913325

4.919420

4.924920

4.929908

4.934453

4 938611

4 942429

4 945948

4 949202

4 952219

4 955024

4 957639

-680.3768MP

0.788982

2.724915

3.427141

4.490704

4.894621

5.486465

6.391340

7.121327

7.733084

8.259572

8.721651

9.133363

9.504608

9.842628

10.152882

10.439584

10.706058

10.954971

11.188492

ii 408416

II 616238

II 813220

12 000438

12 178814

12 349144

12.512124

12 668362

12 818393

12 962692

13 101680

13 235734

13 365194

-661,1334MP

0 624811

1 642310

2 457387

2 822965

3 433796

3 950881

q 604378

5 322556

5 926452

6.023_13

6.502238

7.006386

7.448354

7.844403

8.205168

8.248174

8.630662

9.034958

9.409210

9.757572

10.083392

10.389408

10.677889

10.950735

11.209552

11.455713

11.690397

11.914627

12.129293

12.335178

12.532973

12.723288

12.906669

13.083603

13.254528

692.7300NT

200.00 1.942387

300.00 2.286765

500.00 2.635393

692.73 2.868068

700.00 4.131764

900.00 4.052824

1100.00 4.002588

1300.00 3.967810

1500.00 3.942306

1700.00 3.922803

1900.00 3.907406

2100.00 3.894942

2300.00 3.884645

2500.00 3.875996

2700.00 3.868628

2900.00 3.862277

3100.00 3.856745

3300.00 3.851883

3500.00 3.847577

3700.00 3.843737

3900.00 3.840290

4100.00 3.837180

4300.00 3.834359

4500.00 3.831789

4700.00 3.829438

4900.00 3.827278

5100.00 3.825288

5300.00 3.823448

5500.00 3.821742

5700.00 3.820156

5900.00 3.818677

150.00

250.00

300.00

400.00

500,00

600.00

800.00

1000.00

1135.00

1200.00

1400.00

1600.00

1800.00

2000.00

2125 O0

220O O0

2400 00

2600 O0

2800 O0

3000 O0

3200 O0

3400 O0

3600 O0

3800 O0

4000 O0

4200.00

4400.00

4600.00

4800.00

5000.00

5200.00

5400.00

5600.00

5800.00

6000.00

O.O000NT

1.540279

2.066267

2.222620

2.436403

2.580549

2.689876

2.861714

3.011482

3.109897

3.529172

3.521469

3.531627

3.559240

3.604301

3.641204

4.832297

4.848953

4.863046

4.875126

4.885596

4.894756

4.902839

4.910O24

4.916453

4.922238

4.927473

4.932232

4.936577

4.940560

4.944224

4.947606

4.950738

4.953646

4.956354

4.958881

63.0000

1.883454

2.739027

3.999394

4.894621

4.937776

5.965813

6.773887

7.439550

8.005479

8.497664

8.933109

9.323541

9.677396

10.000938

10.298951

10.575170

10.832564

11.073535

11.300054

11.513756

11.716013

11.907989

12.090679

12.264939

12.431513

12.591051

12.744122

12.891231

13.032825

13.169302

13.301019

70.0000

1.153525

2.079978

2.470981

3.142278

3.702203

4.182808

4.9812O2

5.635930

6.023413

6.220050

6.763323

7.234010

7.651403

8.028615

8.248174

8.415663

8.836863

9.225558

9.586402

9.923116

10.238724

10.535714

10.816160

11 081806

ii 334137

Ii 574423

II 803760

12 023104

12 233288

12 435047

12 629030

12 815814

12.995913

13.169791

13.557862

122 NASAFFP-3287/REV l
TABLE V. - FORMAT FOR 9-CONSTANT FUNCTIONAL FORM

General format:

Record Contents Format Columns

l"

4

5

Species name or formula

Comments and data source

Number of T intervals

Optional identification code

Chemical formula (symbols and numbers)

Zero for gas/nonzero for condensed

Molecular weight

Heat of formation at 298.15K, J/mol

Temperature range

Number of coefficients for Cp°/R

T exponents in empirical equation for Cp°/R

{H°(298.15) - H°(0)},J/mol

First five coefficients for Cp°(T)/R

Last two coefficients for Cp°(T)/R

Integration constants b_ and b2

Repeat 3, 4, and 5 for each interval

AI6

A62

12

A6

5(A2,F6.2)

I2

F13.5

F13.5

2Fll.3

I1

8F5. l

F15.3

5D16.9

2D16.9

2D16.9

1-16

19-80

1-2

4-9

11-50

51-52

53-65

66-80

1-22

23

24-63

66-80

1-80

1-48

49-80

Example:

C12 Chlorine gas. TPIS 1989, vl, pt2, p88.

2 TPIS89 CL 2.00 0.00 0.00 0.00 0.00 0 70.90540

200.000 I000.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0

3.46281724d+04 -5.54712949d+02 6.20759103d+00 -2.98963673d-03

-I.79353467d-09 4.26005863d-13 O.O0000000d÷O0 1.53407075d+03

1000.000 6000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0

6.09256675d+06 -I.94962688d+04 2.85453491d+01 -1.44996828d-02

-6.35852403d-I0 3.32735931d-14 O.O0000000d+O0 1.21211722d+05

0.000

9181.110

3.17303416d-06

-9.43835303d+00

9181.110

4.46388943d-06

-1.69077832d+02

Empirical equations for above example (from eqs. (I) to (3)):

C °

Heat capacity: ._P = at T-2 + a2T -I * a s + afT + asT z ÷aeT 3 ÷ a.zT4

R

T T2 T T4

Enthaipy: H°(T) = -alT "2 ÷ a2T -I lnT + a_ + a 4 _. + a s _ + a_ __ + _ _ ÷ -- RT 3 4 5 T

= T -z Entropy: S°(T) -a I _ - azT -1

R 2

T 2 _ T 4

+ a3 In T ÷ a4T + as _ + a_ __ ÷ a7 __ ÷ b 2

2 3 4

NASA/TP-3287/REVI 123
TABLE VI. - COEFFICIENTSFOR THE 9-CONSTANT FUNCTIONAL FORM

Ag(cr) Silver Cubic Crystal. CODAIA,1989, p228.

I CODA89 AG 1.00 0.00 0.00 0.00 0,00 1 107.86820 0.000

200.000 1235.080 7 -2.0 -I.0 0.0 1.0 2.0 3.0 q.O 0.0 5745.000

-7.09923647d+04 7,25478802d+02 1.066518384-01 5.52954155d-03 -4.42559085d-06

2.09166812d-09 -3.88892646d-13 O.O0000000d_O0 -4.61401426d+03 5.07421604d+00

Ag(1) Silver Liquid. CODATA,1989, p228.

1 CODAS9 AG 1.00 0.00 0.00 0.00 0,00 2 107.86820 0.000

1235.080 6000.000 1 0.0 0.0 0.0 0.0 0.0 0,0 0.0 0.0 5745.000

4.01707377d+00 0.00000000d*00 0,00000000d+00 0.00000000d_00 0.00000000d+00

0.00000000d+00 0,00000000d_00 0,00000000d+00 -4.67226997d+02 -1.77152707d_01

Al(cr) Aluminum Cubic Crystal. CODATA 1989, p217.

1CODAg9 AL 1.00 0.00 0.00 0.00 0.00 1 26.98154 0.000

200,000 933.510 7 -2.0 -I.0 0.0 1.0 2.0 3,0 4.0 0.0 4540.000

-6.25181143d÷04 6.54393435d+02 -7.13188382d-01 1.08872528d-02 -1.45874182d-05

9.96115088d-09 -i.77492801d-12 0.00000000d_00 -3.98543952d÷03 5.55110020d+00

AI(1) Aluminum Liquid, CODATA 1989, 9217.

i CODAS9 AL 1.00 0.00 0.00 0.00 0,00 2 26.98154 O.O00

955,610 5000.000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4540.000

5.81_62551d+00 0.00000000d+00 0.00000000d_00 0.00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -9.57632315¢|+01 -1.75255342d+01

Ar Argon. NSRDS-NBS 35, vl, 1971. Temperature cutoff.

3 L 6/88 AR 1.00 0.00 0.00 0.00 0.00 0 39.94800 0.000

200.000 I(]00,000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6197.428

2.50000000d+00 0.00000000d÷00 0.00000000d÷00 0.00000000d+00 0.00000000d_00

0.00000000d+00 0.00000000d_00 0.00000000d+00 -7.45375000d_02 4.37967491d+00

1000.000 5000.000 1 0.0 0.0 0.0 0.0 0.0 0 0 0.0 0.0 6197.428

2.50000000d¢00 0.00000000d+00 0.00000000d+00 0 00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -7 45375000d+02 4.37967491d+00

6000.000 20000.000 7 -2.0 -i.0 0.0 1.0 2.0 5 0 4.0 0.0 6197.428

-1.OG649969d),09 6.89368419d_05 -1.7809334_d+02 2 4482575_d-02 -1.80435466d-06

6.80204522d-ii -I.00794996d-15 0.00000000d+00 -5 42354627d_06 1.55654961d+03

B(b) Boron beta. JANAF Jun.1983, p174. 100.000

2 J6/83 B 1.00 0.00 0.00 0.00 0.00 1 10.81100 0.000

200.000 600.000 ? -Z.O -i.0 0.0 1.0 2.0 5 0 4.0 0.0 1214.000

2.59827121d+05 -4.77079481d+03 3.Q6414062d+01 -1 28734841d-01 2.89787722d-04

-3.30728004d-07 1.50015720d-]0 0.00000000d+00 2 I4695669d_04 -i.85083320d+02

600.000 2350.000 7 -2.0 -1.0 0.0 1.0 2,0 3 0 4.0 0.0 1214.000

-8.607635qgd+02 -8.05085485d+02 _.07980166d+00 -6 42428118d-04 4.846511794-07

-1.25292027d-I0 1.53608271d-I_ 0.00000000d+00 5 59818191d+05 -2.50596499d+01

B(1) Boron liquid. JANAF Jun.1983, p174. 2550.000

i J6/83 B 1.00 0.00 0.00 0.00 0.00 2 10.81100 0.000

2550.000 6000.000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 1214.000

3.81862551d_00 0.00000000d+00 0.000000D0d+00 0.00000000d+00 0.00000000d+00

c_.OOUOOO00d+OO 0.00000000d+00 0.00000000d_00 3.36060307d+05 -2.07516750d+01

_a(cr) Barium Crystal. Alcock, JPCRD 1992.

Z 5I_D 92 BA 1.00 0.00 0.00 0.00 0.00 I 137.32700 0.000

80.000 298.150 5 -2.0 0.0 1.0 2.0 3.0 0 0 0.0 0.0 6906.992

-l.121d1305d+03 2.79403116d+00 3.08977919d-05 -8 8123052_d-06 1.74153378d-08

0.00000000d+00 0.00000000d_00 0.00000000d+00 -9 _0685800d÷02 -9.I097871_d+00

298.150 1000.000 2 0.0 1.0 0,0 0.0 0.0 0 0 0.0 0.0 6906.992

2.77334463d_00 2.03752236d-03 0.00000000d+00 0 00000000d+00 0.00000000d+00

0.000(|0000d_00 0.00000000d+00 0.00000000d+00 -9 17433810d+02 -8.90970626d+00

Ba(]) Barium Liquid. Alc()ck, JPCRD 1992.

1SRD 92 BA l.OD 0.00 0.00 0.00 0.00 2 157.52700 0.000

1000.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6906.992

_.81086679d+00 0.00000000d+00 O,O0000000d+O0 0,00000000d+00 0.00000000d÷00

0.00000000d+00 0.00000000d÷00 0.00000000d+00 -9.92052381d+02 -2.00027571d+01

124 NASA/TP-3287/REV 1
TABLE VI.- Continued.

Be(a) Beryllium Alpha Crystal. Alcock, JPCRD 1992.

2 SRI) 92 BE 1.00 0.00 0.00 0.00 0.00 1 0.01218 0.000

i00.000 298.150 <) -2.0 0.0 1.0 2.0 0.0 0 0 0.0 0.0 1962.068

5.53237894d+03 -1,82752802d_00 1.895c18151d-02 -2 12159225d-05 O.O0000000d+O0

O.O0000000d+O0 O.O0000000d+O0 O.OODO0000d+O0 -9 83216686d401 6.86689qlld+O0

298.150 15_3.000 q -2.0 0.0 1.0 2.0 0.0 0 0 0.0 0,0 1942.068

-7. 06475788d eOt_ 2.55055075d+00 6.84826887d-0() 1 15701346d-07 O.OOO00000d+O0

0.00000000d)-00 0.00000000d÷00 O.O0001)O00d÷O0 -1 02880367d+03 -1.39967151d)'01

Be(b) Beryllium Beta Crystal. Alcock, JPCRD 1992.

1 SRD 92 BF. 1.00 0.00 0.00 0.00 0.00 2 9.01218 0.000

1543.000 1563.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 1942.068

3.6(}815flU9d_O0 O.O0000000d_O0 O.OOOO000DdiO0 0.00000000d400 O.DOODO000d+O0

0.000[)0000d)-00 0.00000000d_)00 0.00000000d)00 -8.52669779d)-02 -2.00289577d÷01

Be(l) BerTllium Liquid. Hodified Alcock, JPCRD 1992.

1 SRD 92 BF 1.00 0.00 0.00 0.00 0.00 3 9.01218 0.000

1563.000 6000.000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 1942.068

S.SqSGO_82dfO0 0.00000000d+00 0.00000000d_00 0.00000000d÷00 0.00000000d_00

0. O00000()Od_O0 O.O0000OOOd+O0 0. O0000OOOd+O0 2.01675580d_02 -1.89530126d÷01

Br2(cr) Bro),line Rhor.]bic. IPIS 1989 vl, p% 2, p5164. JANAF, 6/82.

1 1P1589 DR 2.00 0.00 0.00 0.00 0.00 1 159.80800 0.000

200.000 265.900 7 -2.0 -I.0 0.0 1.0 2.0 5.0 _.0 0.0 24520.000

1.07933854d+06 -9.504S1870d_05 -8.9515020?dt.01 1.64592907d_00 -8.63318393d-03

2.00710278d-05 -1.74_15531d-08 0.00000000d_00 5.48268005d+0_ 2._7693618d+02

Br2(1) Bromine Liquid. TPIS 1989 vl, pt 2, p314. JANAF, 6/82.

2 TPIS89 BR 2.00 0,00 0.00 0.00 0.00 2 159.80800 0.000

265.900 332.503 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 24520.000

q.02309518d+06 -3.95253257d_0_ -2.25697676d)01 1.95846276d_00 -1.01581659d-02

2.16179654d-05 -1.70837362d-08 O.O0000000d+O0 2.13632258d+05 -2.53261320d+02

552.503 6flOO.Of)O I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 2q520.000

9. (15668oc)3d) Ut) O.O000000OdlO0 0.00000000d_00 0,00000000d-)00 0.00000000di-O0

O.O{)O0000(_d)00 O.O0000000d+O0 0.00000000d+00 -2.69985562d+03 -3.32934996d+01

C(gr) G)-_phite. TRC Tables VC,UC,TC-IOOO-IOO2,Apr 30,1983.

3 X 6/83 C 1.00 0.00 0.00 0.00 0.00 1 12.0LlO0 0.000

200.00O t, 00.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 1053.500

1.1328q,,l.Sd)Ub -l.980qOZIBd+03 1.36536969d+01 -q.6360qO56d-02 1.02132125d-0_

-I.082,",8().;5,i-(),' 4.41220215d-ii O.OOliOO000d+O0 8.99377162d+03 -7.29574863d_01

600.()u_ Wt)t)O.(INO 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 1053.500

3.3559v_. 0,_()b -2.59652393d÷03 6.94883168d_00 -3.48482394d-03 1.84_18460d--06

-5. 0551 t'}.;,.,_-1U 5.7 5060396d-1,') 0.00000000d+00 1. 398_00995d_'06 -4.477176_7d÷01

2000.t)',_, '0:;D.()00 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 1053.500

2.0368'J,"..',,I,vb -l.160960GZd+03 5.70248083d+00 -1.8G310886d-06 6.36532218d-08

-7.094835b',d IS 3.34838385d-16 0.00000000d+00 5.86651046d+03 -2.35256826d+01

Ca(a) Calcium Alpha Crystal. Alcock, JPCRD 1992.

2 SRD 92 t,', 1 00 0.00 0.00 0.00 0.00 1 40.07800 0.000

200.00U 2_8.150 6 -2.0 -I.0 0.0 1.0 2.0 3.0 0.0 D.0 5782.965

-8.3856G,,,?d,t)', 1.76528605d+04 -1._6659817d+02 6,3161667_d-01 -1.32921936d-03

l.l1775,,t_d-tl, 0.00000000d+00 0.00000000d+00 -7.82628469d+0_ 7.5696_272d+02

298.1'(; "1_.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 5782.9,75

-6.26229(,,,_.d)0b _.18556583d_03 -_.06398669d+01 1.20386393d-01 -1.80184335d-04

1.qc)517/ICd-0: -h.73132858d-ll 0.00000000d+00 -6.06434046d+04 2.31531550d+02

Ca(b) Calcium Beta Crvsfal. Alcock, JPCRD 1992.

i SRD 92 CA 1 00 0.00 0.00 0.00 0.00 2 _0.07800 0.000

71.6.000 1115.000 3 0.0 1.0 2.0 0.0 0.0 0.0 0.0 0.0 5782,9<)5

5.70111/(,8d_00 -5.81056490d-03 4.02212518d-06 0.00000000d+00 0.00000000d+00

O.OOgOgOUVd)O0 0.00000000d+00 O,O0000000d+O0 -I.51673911d+03 -2.60751190d÷01

Ca(I) Calcium Liquid. Alcock, JPCRD 1992.

i SRD 92 CA 1.00 0.00 0.00 0.00 0.00 3 _0.07800 0.000

1115.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5782.945

_.570323qbd_ 00 O.O00000OOd+O0 O.O0000000dtO0 O. O0000DOOd_O0 O.O0000000d÷O0

O.O0000000d_O0 O.O0000000d+O0 O.O0000000d+O0 -9.82218808d+02 -2.11987699d_01

Cd(cr) Cadmium Crysfal. CODATA 1989, p223.

I CODA89 CD 1.00 0.00 0.00 0.00 0.00 1 I12._I100 0.000

I00.000 594.258 7 -2.0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0 6247.000

1.3752731_d+05 -3.22158985d+03 5.12190528d+01 -I.22613669d-01 2.8588_027d-04

-3.28688363d-07 1.52046961d-I0 O.O0000000d_O0 1.30280694d_04 -1.55132402d_02

Cd(1) Cadmium Liquid. CODATA 1989, p223.

I CODA89 CD 1.00 0.00 0.00 0.00 0.00 2 112.41100 0.000

594.258 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6247.000

3.59612292d÷00 0. 00000000d+00 0.00000000d+00 0. 00000000d+00 0.00000000d_00

0.00000000d+00 0.00000000d+00 O.O0000000dtO0 -q.22039477d+02 -1.323298]6d_01

NASA/TP-3287/REV 1 125
TABLE VI.- Continued.

C12 Chlorine gas. TPIS 1989, vl, pt2, p88.

2 TPIS89 CL 2.00 0.00 0.00 0.00 0.00 0 70.90540 0.000

200.000 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 9181.110

3.46281724d+00 -5.54712949d+02 6.20759103d+00 -2.9896567_rd-03 3.17303416d-06

-I.79365467d-09 4.26005863d-13 O.0OO00000d÷O0 1.53407075d+05 -9.43835305d+00

1000.000 6000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 9181.110

6.09256675d+06 -1.94962688d+04 2.85453491d+01 -I._4996828d-02 4.46388943d-06

-6.55852405d-i0 3.32755951d-14 O.O0000000d+O0 1.21211722d+05 -1.69077832d+02

Co(a) Cobalt Alpha Crystal. JANAF, SEPT. 1967.

2 J 9/67 CO 1.00 0.00 0.00 0.00 0.00 1 58.93320 0.000

200.000 500.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 0.0 4771.000

-8.652_46060D+05 I.q62253209D+O4-9.972017980D+01 5.79472D53DD-O1-7.800971910D-04

8.554609750D-O7-3.890648690D-10 O.O00000000D+OO-6.796490570D+04 5.507032100D+02

500.000 700.100 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4771.000

-9.858622510D+05 6.807553490D+O3-1.5182BI739D+OI 2.23072_772D-OZ-g. QO3048680D-06

O.O00000000D+O00.O00000000D+O00.O00000000D+OO-5.B4561925DD+OQ 1.012261440D+02

Co(b) Cobalt Beta, Lambda trBnsition at 1394K. JANAF,9/1967.

4 J 9/67 CO 1.00 0.00 0.00 O.DO 0.00 2 58.93320 0.000

700.100 800.000 2 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0 4771.000

2.125115885D÷00 2.218475346D-03 O.O00000000D+O00.000000000D+O0 0.000000000D+00

O.O000000DOD+O00.O00000000D+O00.O00000000D+OO-6.197709_20D+O2-B.944546980D+O0

BO0.O00 1394.000 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4771.000

2.165664332D+O7-g.459479610D+O4 1.575241107D+O2-1.120514746D-01 5.19093019DD-05

O.O00000000D+O0 8.000000000D+00 O.O00000000D+O0 5.655818q90D+O5-1.067845763D+03

1394.000 1400.000 2 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0 4771.000

3.08358440qD+O2-2.164567334D-OI O.O00000000D+O00.O00000000D+O00.O00000000D+O0

O.O00000000D÷O00.O00000000D+O00.O00000000D+OO-2.1qB22009BD+O5-1.921045340D+03

1400.000 1768.000 4 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 0.0 4771.000

1.563105956D+O5-2.66022478ID÷02 1.560064075D-OI-2.995804151D-D5 0.000000000D÷00

O.O00000000D+O00.O00000000D+O00.O00000000D+OO-8.806490490D+05 1.859461480D+05

Co(1) Cobal± Liquid. JANAF, SEPT. 1967.

i J 9/67 CO 1.00 0.00 0.00 0.00 0.00 3 58.93320 0.000

1768.000 6000.000 i 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 _771.000

4.871122892D+00 O.O00000000D+O00.O00000000D+O00.O00000000D+O00.O00000000D+O0

O.ODOOOOOOOD+O00.O00000000D+O00.O00000000D+OO-l.771752_86D÷O2-2.448546078D+OI

Cr(cr) Chromium Crystal. Lambda trans. 511.5K. JANAF. June 1973

3 J 6/75 CR 1.00 0.00 0.00 0.00 0.00 I 51.99610 0.000

200.000 311.500 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4057.000

8.050977490D+O5-1._39826182D+04 8.273410890D+OI-2.075832465D-OI 2.008740848D-04

O.O000000OOD+O00.O00000000D+O00.O00000000D+O0 6.182279460D+O4-4.559918050D+02

311.500 I000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 4057.000

-2.656384317D+05 5.248549440D+OS-I.4132011IID+01 4.445712580D-O2-5.767961420D-05

5.742240540D-O8-9.198565660D-12 O.O00000000D+OO-1.672037520D+04 8.176250500D+01

I000.000 2130.000 5 -Z.O -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4057.000

4.882406160D+05 1.41_874655D+02 3.261541510D-01 2.872541027D-05 5.847978740D-09

0.000000000D+00 0.000000000D+00 O.OOO000000D+O0 1.072620755D÷02 2.056599199D+00

Cr(1) Chromium Liquid. JANAF. June 1975.

1J 6/75 CR 1.00 0.00 0.00 0.00 0.00 2 51.99610 0.000

2150.000 6000.000 1 0.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4057.000

4.730284767D+00 O.O00000000D+O00.O00000000D+O00.O00000000D+O00.O00000000D+O0

O.O00000000D+O00.O00000000D+O00.O00000000D+O0 5.755097610D+O2-2._S5203182D+O1

Cs(cr) Cesium Crystal. CODATA, 1989, p263.

I CODA89 CS 1.00 0.00 0.00 0.00 0.00 1 132.90545 0.000

100.000 501.590 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 7711.000

6.51984125d+04 -i.75663905d+05 1.99968107d+01 -6.95852875d-02 1.09368254d-04

O.O0000000d+OO O.O0000000d+O0 O.O0000000d÷O0 6.38289073d+03 -9.338251_5d+01

Cs(1) Cesium Liquid. CODATA, 1989, p263.

2 CODAB9 CS 1.00 0.00 0.00 0.00 0.00 2 132.90543 0.000

301.590 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 0.0 7711.000

-4.21852769d+04 -1.74510318d+01 5.70212472d+00 -5.11566989d-05 5.20140701d-06

-1.76574712d-10 Q.82212937d-14 O.O0000000d+O0 -1,2909_98Id+03 -2.031_0758d+01

1000.000 2000.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 0.0 7711.000

-7.26659499d+05 3.00676906d+05 1.696_1895d-01 2.91256052d-04 1.76880825d-07

7.73027452d-10 -8.90216532d-14 O.O0000000d+O0 -1.92376169d+04 1.64100574d+01

126 NASA/TP-3287/REV 1
TABLE VI. - Continued.

Cu(cr) Copper Cubic Crystal. CODATA, 1989, p226.

1 CODA89 CU 1.00 0.00 0.00 0.00 0.00 i 63.54600 0.000

200.000 1358.000 7 -2,0 -1.0 0,0 1.0 2.0 3.0 4.0 0.0 5004.000

-2.45577517d+04 1.6_806928d+02 2.08094710d+00 2.6_907840d-03 -2.71410148d-06

1.40286505d-09 -9.72432327d-14 0.00000000d+00 -1,73785101d+05 -8.15316658d+00

Cu(1) Copper Liquid. CDDATA, 1989, p226.

1CDDA89 CU 1.00 0.00 0.00 0.00 D.DO 2 63.54500 D.DOD

1358.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5004.000

3.94491076d+00 0,00000000d+00 0.00000000d+00 0.00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 O.O0000000d+O0 -2,11101378d+02 -i.83506577d+01

02 Deulerium. TPIS, 1989, vl, pi2, pp_5-6.

3 TPIS89 D 2.00 0.00 0.00 0.00 0.00 0 4.02820 0.000

200.000 1000.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 _.0 O.D 8569.103

2.12578989d+04 -2.99694507d+02 5.13031451d+00 -4.17296958d-03 5.01454580d-06

-2.12658854d-09 2.38653277d-15 0.00000000d+00 3,9_498190d+02 -1.16419095d+01

1000.000 6000.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 0.0 8569.103

8.21515641d+05 -2.36561983d+05 5.34297106d+00 6.92852217d-05 -8.52371794d-08

2.456_5364d-ll -1.96060094d-15 0.00000000d+00 1.43421244d+04 -1.71259786d+01

6000.000 20000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 _.0 0.0 8569.103

q.89968473d+08 -3.11279617d+05 7.94573202d÷01 -8.42554949d-03 q.78927371d-07

-i.39085557d-lI 1.63752128d-16 0.00000000d+00 2,46005105d+06 -6.63681004d+02

ELECTRON GAS CP/R = 2.5

3 L 6/88 E 1.00 0.00 0.00 0.00 0.00 0 0.00055 0.000

200.D00 IDOD.000 1 0.D 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6197.428

2.50000000d+00 0.00000000d+00 0.00000000d+00 O.00000000d+DO O.DOODOODOd÷O0

O.000000DOd+O0 O.O0000000d+00 0.00000000d+00 -7.45375000d+02 -1.17208127d+01

1000.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0 0 0.0 0,0 6197.428

2.50000000d+00 0.00000000d+00 0.00000000d+00 0 O0000000d+O0 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -7 _5375000d+02 -i.17208127d+01

6000.000 20000.000 1 0.0 0.0 0.0 0.0 0.0 0 0 0.0 0.0 6197.428

2.50000000d+00 O.O0000000d+O0 0.00000000d+00 0 O00000DOd+O0 O.00000DOOd÷O0

0.00000000d+00 0.00000000d+00 0.00000000d+00 -7 45375000d+02 -1.17208127d+01

F2 Fluorine gBS. TPIS 1989, vl, pt2, p73.

2 TPIS89 F 2.00 0.00 0.00 0.00 0.00 0 37.99681 0.000

200.000 1000.000 7 -2.0 -I.0 0.0 1.0 2.0 3 0 4.0 0.0 8825.106

1.01817754d+04 2.27422347d+01 1.97135403d+00 8 15160125d-03 -1.14895968d-05

7.958649_7d-09 -2.16707863d-12 0.00000000d+00 -9 58693653d+02 1.13059974d÷01

1000.000 6000.000 7 -2.0 -1.0 0.0 1.0 2.0 3 0 4.0 0.0 8825.106

-2.9_116687d+06 9.45659515d+03 -7.73861346d+00 7 64471159d-03 -2.24100723d-06

2.91584475d-i0 -1.42503371d-14 0.00000000d+00 -6 07100597d+04 8.42385515d÷01

Fe(a) Iron , Lambda transition at 1042K JANAF, MAR.1978.

4 J 3/78 FE 1.00 0.00 0.00 0.00 0.00 1 55.84700 0.000

200.000 500.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 O.D 4507.000

1.3508391600+04-7.8044781600+02 9,_40700400D+00-2.5219851940-02 5.3506634400-05

-5.0996789500-08 1.994145811D-11 0.0000000000+00 2.4168215410+03-4.7492772500÷01

500.000 800.000 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4507.000

3.5430290900+06-2.447148112D+04 6.561015020D+01-7.0439233400-02 3.1810503600-05

0.000000000D+00 0.0000000000+00 0.000000000D+00 1.345058629D+05-_.1537848900+02

800.000 1042.000 7 -2.0 -1.0 0.0 1.0 2.0 S.O q.O 0.0 4507.000

2.703955561D+09-8.193_001000+06 3.9160_77500+02 2.4262_68_0D+01-3.3218259700-02

1.6802253_30-05-2.7419606930-09 0.000000000D+00 5.4203279900+07-2.2107241550÷0_

1042.000 1184.000 3 -1.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 4507.000

6.7318225_00+05-I.1672556520+05 5.0985666300-01 0.0000000000+00 0.000000000D+00

0.0000000000+00 0.0000000000+00 0.000000000D+00-3.7351_0010D+06 8.2342482200+05

Fe(c) Iron Gamma Crystal. JANAF, MAR.1978.

1J 3/78 FE 1.00 0.00 0.00 0.00 0.00 2 55.84700 0.000

1184.000 1665.000 5 -1.0 0.0 1.0 2.0 3.0 0.0 0.0 0.0 4507.000

7.7649443500+04-2.142017878D+02 2.2751273540-01-I.0459373970-0_ 1.804124598D-08

0.0000000000+00 0.0000000000+00 0,0000000000+00-4.0216090_00÷05 1.38_5496350+D3

Fe(d) Iron Delta Crystal. JANAF, MAR.1978.

1 J 3/78 FE 1.00 0.00 0.00 0.00 0.00 3 55.84700 0.000

1655.000 1809.000 3 -1.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 4507.000

9.2822525800+03-7.7714946200+00 q.2889952100-03 0.000000000D+00 0.000000000D+00

0.0000000000+00 0.000000000D÷00 0.0000000000+00-5.549788070D+04 6.678224840D+01

Fe(1) Iron Liquid. JANAF, MAR.I978.

1 J 3/78 FE 1.00 0.00 0.00 0.00 0.00 4 55.84700 0.000

1_09.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0,0 0.0 0,0 4507.000

5.5353833240+00 0.000000000D+00 0.0000000000+00 0,600000000D÷00 0.0000000000+00

0.0000000000+00 0.0000000000+00 0.0000000000+00-1.2697951230÷05-2.9480780150+01

NASA/TP-3287/REV 1 127
TABLE VI. - Continued.

Ge(cr) Germanium Cubic. TPIS 1991, v2, ptl, p308, pt2 p268.

2 TPIS91 G£ 1.00 0.00 0.00 0.00 0.00 1 72.61000 0.000

200.000 Q00.000 5 -2.0 -I.0 0.0 1.0 2.0 0.0 0.0 0.0 4636.360

-2.39650371d+05 3.15056873d+03 -1.33393959d_01 3.6_799385d-02 -2.9_210133d-05

0.00000000d+00 0.00000000d+00 0.00000000d+00 -1.61388131d+04 7.93920158d+01

400.000 1211.400 3 -2.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 6636.360

-i.88824135d)04 2.89817304d+00 3.59165939d-04 O.O0000000d+O0 0.00000000d+00

0.0001)0000dI-00 0.00000000d+00 D.OOOOODOOd_DO -9.43386385d_02 -1.29866971d+01

Oe(1) Germanium Liquid. TPIS 1991, v2, p%1, p308, pt2 p268.

1 IPIS91GE 1.00 0.00 0.00 0.00 0.00 2 72.61000 0.000

1211.400 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4636.360

3.31949808d+00 0.00000000d+00 0.00000000d+00 0.00000000d*00 O.O0000000d+O0

O.O0000000d+O0 O.O0000000d_O0 O.O0000000d_O0 3.27899664d_03 -I.18599295d+01

H2 Hydrogen. GLUSHKO £T.AL. vl, pt2, 1978, ppSl-52.

3 TPIS78 H 2.00 0.00 0.00 0.00 0.00 0 2.01588 0.000

200.000 I000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 8468.102

4.07832231d_04 -8.00918545d+02 8.21470167d_00 -1.26971436d-02 1.75360493d-05

-1.20286016d-08 3.36809316d-12 O.O0000000d+O0 2.6R?4_4_Sd_-03 -3.0_378866d+01

1000.000 6000.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 4.0 0.0 8468.102

5.60812358d)05 -8.371_9134d+02 2.9]536304d+00 1.2522_993d-03 -3.7_071842d-07

5.93662325d-Ii -3.60699573d-15 0.00000000d+00 5.33981585d¢03 -2.20276405d+00

6000.000 Z(1000.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 5.0 0.0 8468.102

4.96621613flr08 -5.14764812d+05 7.98388750d)01 -8.41450_19d-03 4.7530604_d-07

-I.37180973d-II 1.60537460d-16 0.00000000d+00 2.48835466d+06 -6.69552419d+02

He Helium. NSRDS-NBS 35, 1971. Temperature cutoff.

3 LIO/90 HE 1.00 0.00 0.00 0.00 0.00 0 g.00260 0.000

200.000 1000.000 1 0.0 0.0 D.O 0.0 0.0 0.0 0.0 0.0 6197.428

2.5000(}000d)00 O.O0000000d+O0 O.O0000000d÷O0 0 00000000d+00 O.00000000d+O0

O.O0000000d+O0 O.O0000000d÷O0 0.00000000d+00 -7

I000.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0

2.50000000d+00 0.00000000d+00 O.O000000Od+O0 0

O.O0000OOOd+O0 O.O0000000d+O0 0.00000000d+00 -7

6000.000 20000.000 7 -2.0 -i.0 0.0 1.0 2.0 3

4.49657/17d+06 -2.76520860d+03 3.19328263d÷00 -9

-2.62522q12d-13 4.34087884d-18 0.00000000d÷00 2

Hg(cr) Mercury Tetragonal Crystal. JANAF

45375000d+02 9.28723974d-01

0 0.0 0.0 6197.428

O0000000d÷00 0.00000000d+00

05375000dF02 9.28723974d-01

0 4.0 0.0 6197._28

I1889220d-05 6.69027627d-09

I1382700d+04 -5.05672478d+00

Dec. 1961.

I J12/61 HG 1.00 0.00 0.00 0.00 0.00 1 200.59000 0.000

I00.000 254.290 _ -2.0 0.0 1.0 2.0 0.0 0.0 0.0 0.0 93_3.000

-3.18_tS_.bd+05 3._6442487d+00 -4.05486_61d-03 1.76628113(]-05 0.00000000d_00

0.000000uOd+OO 0.00000000d+00 0.00000000d+00 -1.282_5_3_d+03 -I.13201016d+01

Hg(1) Mercury Liquid. JANAF, Dec. 1961.

2 J12/61 H; 1.00 0.00 0,00 0.00 0.00 2 200.59000 0.000

23h.29U _(I0 000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 q.O 0.0 9343.000

1.05_tt?57d,O -1.99382117d+03 1.88057375d_01 -5.99466940d-02 1.22832483d-04

-i.2931551ud-D 5.53072552d-II O.O0000000d+OO 7.91675530d+03 -9.06_85332d+01

600.O_u 2U 0.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 _.0 0.0 9343.000

7.9158DXt_d*O% -3.95650498d+03 1.10646079d+01 -8.15392266d-03 _.97046569d-06

-I.51041551d-09 1.87203419d-13 O.O0000000d_O0 2.21375986d÷04 -6.07242904d+01

I2(cr) Iodine Rhombic Crystal. IPIS 1989, vl, pt2, p315.

I TPISBg I 2 D0 0.00 0.00 0.00 0.00 1 253.80894 0.000

200.000 38o.750 7 -2.0 -1.0 0.0 1.0 2.0 3.0 _.0 0.0 13196.000

-3.91590252d)06 9.17546472d+04 -8.92978650d+02 4.68534133d+00 -1.36091945d-02

2.07924325d-05 -I.29598302d-08 0.00000000d_00 -3.926596_8d_05 4.43738168de03

12(1) Iodine Liquid. TPIS 1989, vl, p%2, p315.

1 1PIS89 I 2 O0 0.00 0.00 0.00 0.00 2 253.80894 0.000

386.750 60 0.000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 13196.000

9.56821268d)00 0.00000000d+00 0.00000000d+00 0.00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -1.20445382d÷03 -3.63732610d+01

K(cr) Po%assium Cubic Crystal. CODATA 1989, p257.

I CODAS9 K 1 00 0.00 0.00 0.00 0.00 1 39.09830 0.000

200.000 336.860 4 -2.0 0.0 1.0 2.0 0.0 0.0 0.0 0.0 7088.000

-I.02203174d)05 1.33375201d+01 -5.58099071d-02 9.01300905d-05 O.O0000000d+O0

O.00000000d_O0 0.00000000d+00 O.O0000000d+O0 -2.63506242d+03 -5.61537649d+01

K(1) Potassium Liquid. CODAIA 1989, p257.

I CODA89 K 1 O0 0.00 0.00 0.00 0.00 2 39.09830 0.000

336.860 2200.000 7 -Z.O -I.0 0.0 1.0 2.0 3.0 q.O 0.0 7088.000

-3.93579278d+03 -4.5_722866d+01 4.84524269d+00 -3.08354487d-03 2.0155_768d-06

-3.70613204d-11 5.03283971d-15 O.O0000000d+O0 -8.07563697d÷02 -I.83664092d+01

128 NASA/TP-3287/REV 1
TABLE VL - Continued.

Kr Krypton. NSRDS-NBS 35, 1971. Temperature cutoff.

3 LI0/90 KR 1.00 0.00 0.00 0.00 0.00 0 83.80000 0.000

200.000 1000.000 1 0.0 O.D 0.0 0.0 0.0 0.0 0.0 0.0 6197.428

2.50000000d+00 O.DO00OO00d+O0 0.00000000d+00 O.O0000000d+O0 O.O0000000d+O0

O.O00DO000d+O0 0.00000000d+00 D.O0000000d+DO -7.45375000d+02 5.49095651d+00

1000.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6197._28

2.50000000d+00 0.00000000d+00 0.00000000d+00 O.O000000Od÷O0 O.00000000d+O0

0.00000000d÷00 D.D0000000d+00 0.000000D0d÷00 -7.45375000d+02 5.69095651d+00

6000.000 20000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 6197.428

-2.63908780d+09 1.65974315d+06 -4.20455715d+02 5.58583797d-02 -4.02626981d-06

i._9484943d-10 -2.20230087d-15 0.00000000d+00 -1.3102388]d+07 3.6522_315d+03

Li(cr) Lithium Crystal. Gurvich 1982,vlV,pt 1,p245;pt 2,p286.

2 TPIS82 Ll 1.00 0.00 0.00 0.00 0.00 1 6.94100 0.000

200.000 298.150 3 -2.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 4632.000

-9.86065231d+03 2.30432385d+00 2.67166372d-03 0.00000000d+00 0.00000000d+00

O.OO000000d+O0 0.00000000d+00 0,00000000d+00 -8.38853612d+02 -i,06788169d+01

298.150 453.690 3 -2.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 4632.000

7.23882507d+O_ 1.57031_23d-01 6.770_0615d-03 0.00000000d+00 0.00000000d+00

O.00000000d+O0 0.00000000d+00 0.00000000d+00 -1.04949734d+02 9.96176448d-01

Li(1) lithium Liquid. Gurvich Ig82,vIV,pt l,p245;pt 2,p286.

i TPIS82 LI 1.00 0.00 0.00 0.00 0.00 2 6.94100 0.000

453.690 6000.000 4 0.0 1.0 -2.0 2.0 0.0 0.0 0.0 0.0 6632.000

3.75572343d+00 -6.33230341d-04 2._6556923d+0_ 3.16073948d-07 0.00000000d+00

0.00000000d+00 0.00000000d+D0 0.00000000d+00 -7.29911669d+02 -1.70127465d+01

Hg(cr) Magnesium Hexagonal Crystal. Alcock, JPCRD 1992.

2 SRD 92 HG 1.00 0.00 0.00 0.00 0.00 1 24.30500 0.000

100.000 298.150 5 -2.0 0.0 1.0 2.0 3.0 0.0 0.0 0.0 4979.161

-5.41222513d÷03 1.45817372d÷00 1.33020467d-02 -4.09885850d-05 4.75433910d-08

D.O0000000d+O0 0.00000000d+00 0.00000000d+00 -7.75947201d+02 -6.98970235d+00

298.150 925 000 4 -2.0 0.0 1.0 2.0 0 0 0.0 0.0 0.0 4979.161

-2.86006030d+04 3.39887738d+00 -7.24396266d-04 1.40525419d-06 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -1.08951991d+03 -1.54597366d+01

Mg(1) Magnesium Liquid. Alcock, JPCRD 1992.

I SRD 92 MG 1.00 0.00 0.00 0.00 0.00 2 24 30500 0.000

923.000 6000 000 I 0.0 0.0 0.0 0.0 0 0 0.0 0.0 0.0 4979.161

4.12531827d+00 0.00000000d+00 O.O0000000d+O0 0.00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -6.58991948d+02 -1.93782858d+01

Mn(a) Manganese Alpha crystal. JANAF Sep.1967.

1 J 9/67 MN 1.00 0.00 0.00 0.00 0.00 1 54 93805 0.000

200.000 980 000 5 -2.0 0.0 1.0 2.0 3 0 0.0 0.0 0.0 4994.000

-1.233096191D+04 2.550461313D+00 2.958134143D- 3-1.694845658D-06 7.535779960D-I0

O.O00000000D+O0 0.000000000D+00 0.000000000D+00-9.197731690D+02-1.156425686D÷01

Mn(b) Manganese Beta crystal. JANAF Sep.1967.

l J 9/67 MN 1.00 0.00 0.00 0.00 0.00 2 54 93805 0.000

980.000 1361 000 5 -2.0 0.0 1.0 2.0 3 0 0.0 0.0 0.0 _994.000

-6.19820_1600+06 4.902844500D÷01-7.5696031900-02 _.819965140D-05-1.079976674D-08

0.;:00000000D+00 0.000000000D+00 0.0000000000+00-2.773218599D+04-2.7788470990+02

Hn(c) Manganese Gamma crystal. JANAF Sep.1967.

I J 9/67 MN 1.00 0.00 0.00 0.00 0.00 3 54 93805 0.000

1361.000 1412 000 3 -2.0 0.0 1.0 0.0 0 0 0.0 0.0 0.0 _994.000

-5.716587660D+06 1.276906176D+01-3.3062297500- 3 0.000000000D+00 0.000000000D+00

0.000000000D+00 0.000000000D+00 0.0000000000+00-1.3578_8658D+0_-7.887772440D+01

Mn(d) Manganese Delta crystal. JANAF Sep.1967.

I J 9/67 MN I;00 0.00 0.00 0.00 0.00 _ 54 93805 0.000

1412.000 1519 000 3 -2.0 0.0 1.0 0.0 0 0 0.0 0.0 0.0 4996.000

-4.426985750D+06 1.025240427D÷01-1.8358346_0D-03 0.000000000D+00 0.0000000000+00

0.0000000000+00 0.000000000D+00 0.000000000D+00-I.035145565D+04-6.22177_1400+01

Hn(1) Manganese Liquid. JANAF 5ep.1967.

I J 9/67 MN 1.00 0.00 0.00 0.00 0.00 5 54 93805 0.000

1519.000 6000.000 1 0.0 0.0 0.0 0.0 0 0 0.0 0.0 0.0 4994.000

5.535383324D+00 0.000000000D+00 0.000000000D+00 0.000000000D+00 0.000000000D+00

0.000000000D+00 0.000000000D+00 0.000000000D+00-9,396236720D+02-2.8536338200+01

NASA/TP-3287/REV 1 129
TABLE VI.- Continued.

Mo(cr) Molybdenum Crystal. JANAF Mar.1978.

3 J 5/78 MO 1.00 0.00 0.00 0.00 0.00 1 95.94000 0.000

200.000 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 _.0 0.0 q585.000

-4.961689500D+04 4.280941440D+02 7.671983260D-01 5.731518660D-03-6.5816418000-06

5.7081928900-09-7.9173484900-13 0.0000000000+00-3.0395847420+03-1.230466896D+00

1000.000 2200.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0 4585.000

-3.616012760D+06 1.4739864320+04-2.1355643980+01 2.117590704D-02-9.7848788700-06

2.494B712700-09-2.4209654000-13 0.000000000D+00-8.9739723400+04 1.5064154720+02

2200.000 2896.000 4 -2.0 0.0 1.0 2.0 0.0 0.0 0.0 0.0 4585.000

-5.4251511600+07 6.A56125010D+01-3.577926680D-02 6.215211850D-06 O.O00000000D+O0

O.O00000000D+O00.ODO000000D+O0 0.000000000D+00-9.5174419400+04-4.285055390D+02

Mo{l) Molybdenum Liquid. JANAF Mar.197B.

I J 3/78 MO 1.00 0.00 0.00 0.00 0.00 2 95.94000 0.000

2896.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4585.000

4.5289499920+00 0.0000000000+00 0.000000000D+00 0.000000000D+00 O.000000000DFO0

0.0000000000+00 O.O00000000D+O0 0.0000000000+00 2.0217391620+05-2.280808914D+01

N2 Nitrogen. GLUSHKO ET.AL. vl, pt2, p207, 1978.

5 TPIS78 N 2.00 0.00 0.00 0.00 0.00 0 28.01348 0.000

200.000 1000.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 _.0 0.0 8678.104

2.21037122d+04 -3.81846145d+02 6.08273815d+00 -8.53091581d-05 1.38464610d-05

-9.62579293d-09 2.51970560d-12 0.00000000d+00 7.10845911d+02 -1.07600320d÷01

1000.000 6000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 8670.104

5.87709908d+05 -2.25924255d+03 6.06694267d+00 -6.15965296d-0_ 1.49179819d-07

-1.92309442d-iI 1.06194871d-15 O.O0000000d+O0 1.28520618d+04 -1.58665484d+01

6000.000 20000.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0 8670.104

8.30971200d+08 -6.42048187d+05 2.02020507d+02 -3.06501961d-02 2.48685558d-06

-9.70579208d-Ii 1.45751673d-15 O.O0000000d+O0 4.95850665d÷06 -I.67204771d+05

Na(cr) Sodium Cubic Crystal. CDDATA 1989, p25_.

I CODAS9 NA 1.00 0.00 0.00 0.00 0.00 1 22.98977 0.000

200.000 371.010 4 -2.0 0.0 1.0 2.0 0.0 0.0 0.0 0.0 6460.000

-3.58445796d+04 6.47941467d+00 -1.89869735d-02 3.55238708d-05 0.00000000d+00

O.O0000DOOd+O0 O.O0000000d+O0 O.O00OO000d+O0 -1.50431974d+03 -2.67778503d+01

Na(1) Sodium Liquid. CODATA 1989, p254.

i CODA89 NA 1.00 0.00 0.00 0.00 0.00 2 22.98977 0.000

371.010 2500.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 6460.000

2.69483872d+04 -2.51901591d+02 5.16245895d+00 -3.05857602d-05 1.69641061d-06

-I.51964196d-i0 1.96287017d-14 O.O0000000d+O0 2.84218762d+02 -2.22576606d+01

Nb(cr) Niobium Crystal. JANAF, Dec. 1973.

3 J12/73 NB 1.00 0.00 0.00 0.00 0.00 1 92.90638 0.000

200.000 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 5241.000

-4.2548118300+04 3.8752972900÷02 1.184449627D+00 _.507436940D-05-5.232092470D-06

3.5134528500-09-9.507606910D-13 0.0000000000+00-2.864449417D+05-2.4_2974494D+00

I000.000 2000.000 7 -2.0 -i.0 0.0 1.0 2.0 5.0 4.0 0.0 5241.000

2.550146384D+07-1.0867768880+05 1.951042091D+02-1.729178828D-01 8.6803685800-05

-2.268651192D-08 2.4401924920-12 0.0000000000+00 6.4786151000+05-I.2852779050+05

2000.000 2750.000 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 5241.000

2.7819449950+08-5.202613500D+05 3.6845921500+02-I.1429067960-01 1.568122224D-05

0.0000000000+00 O.O00000000D+O00.O00000DOOD+O0 3.554615290D+06-2.8140604750+05

Nb(1) Niobium Liquid. JANAF, Dec. 1973.

i J12/73 NB 1.00 0.00 0.00 0.00 0.00 2 92.90658 0.000

2750.000 6000.000 I 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5241.000

4.0257355260+00 O.O00000000D+O00.O00000000D+O00.O00000000D+O00.O00000000D÷O0

O.O00000000D+O00.O00000000D+O00.O00000000D+O0 1.427048829D+03-1.857964562D+01

Ne Neon. NSRDS-NBS 35, 1971. Temperature cutoff.

3 LI0/90 HE 1.00 0.00 0.00 0.00 0.00 0 20.17970 0.000

200.000 i000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6197.428

2.50000000d÷00 O.O0000DOOd+O0 O.DOOO0000d+O0 0.00000000d+00 O.O0000000d+O0

O.O0000000d+O0 O.O000OO00d+O0 O.O0000000d÷0O -7._5375000d+02 3.35532272d+00

1000.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0,0 0.0 0.0 6197.428

2.50000000d+00 O.O0000000d+O0 O.O0000000d+O0 O.O000000Dd+O0 O.O0000000d+O0

O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0 -7._5375000d+02 5.35552272d+00

6000.000 20000.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 4.0 0.0 6197._28

6.26181560d+07 -3.81071521d+04 1.19019437d+01 -1.20827544d-05 8.59337454d-08

-3.24608523d-12 5.17540351d-17 O.OODO0000d+O0 5.01326057d+05 -7.79987192d+01

130 NASA/TP-3287/REV 1
TABLE VI. - Continued.

Ni(cr) Nickel Crystal lambda ±rans 631K. JANAF 0ec.1976.

J12/76 NI 1.00 0.00 0.00 0.00 0.00 1 58.69340 0.000

200.000 400.000 6 -2.0 -i.0 0.0 1.0 2.0 3.0 0.0 0.0 4786.000

-7,689620450D+05 1.43q0430670+04-1.042812025D+02 5.9264701700-01-6.9872609900-04

4.9063156900-07 0.000000000D+00 0.000000000D+00-6.544186_800+04 5.5117147200+02

400.000 631.000 6 -2.0 -I.0 0.0 1.0 2.0 3.0 0.0 0.0 4786.000

-3.3373287500+08 3.416013180D+06-1.3910605990+04 2.8190512090+01-2.8413527750-02

1.1402968890-0J 0.000000000D÷00 0.0000000000+00-1.7458742480+07 8.1600188200+04

631.000 1200.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 q.O 0.0 4786.000

1.0380283620+09-6.8252761100+06 1.857903283D+04-2.678491662D+01 2.1582582310-02

-9.215924210D-06 1.628345439D-09 O.O00000000D+O0 5.7785055400+07-I.159797799D+05

1200.000 1728.000 5 -2,0 -1.0 0.0 1,0 2.0 0.0 0.0 0,0 4786,000

3.1859287400+07-8.638579620b+64 9.0560867500+01-5.8627706009-02 6.7553254300-06

0.0000000000+00 O.O00000000D+O00.O00000000D+O0 5.5770752500+05-6.5260787300+02

Ni(1) Nickel Liquid. JANAF Dec.1976.

i J12/76 NI 1.00 0.00 0.00 0.00 0.00 2 58.69340 0.000

1728.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4786.000

4.6798909380+00 0.000000000D+00 0.000000000D÷00 0.0000000000+00 0.000000000D+00

O.ODO000DOOD+O00.O00000000D+O0 0.000000000D+00-5.2137455100+02-2.3354519430+01

02 Oxygen. Gurvich et al. vl, pt 2, p9, 1989.

3 TPIS89 0 2.00 0.00 0.00 0.00 0.00 0 31.99880 0.000

200.000 1000.000 7 -2.0 -I.0 0.0 ],0 2.0 3.0 4.0 0.0 8680.104

-3.42556269d÷04 4.84699986d÷02 I.I1901159d+00 4.29388743d-03 -6.8_627313d-07

-2.02337678d-09 1.03904064d-12 O.O0000000d+O0 -3.39145434d+03 1.84969912d+01

i000.000 6000,000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 _.0 0.0 8680.104

-i.03793994d+06 2.34483275d+05 1.81972949d+00 1.26784887d-03 -2.18807142d-07

2.05372411d-lI -8.19549062d-16 O.O00DO000d+O0 -1.68901253d+04 1.75871835d+01

6000.000 20000,000 7 -2.0 -i.0 0.0 1,0 2.0 5.0 4.0 0.0 8680.104

4.97515261d+08 -2.86602339d+05 6.69015_6_d+01 -6.16971869d-05 3.01623757d-07

-7.42087888d-12 7,277_4063d-17 0.00000000d+00 2.29548755d+06 -5.530_4968d+02

P(cr) Phosphorus Crystal(Nhite). TPIS I989. JANAF June, 1961.

I TPI$89 P 1 00 0.00 O.DD O,DO D,DO 1 30,97376 O.ODD

195 400 317.300 5 -2.0 -1.0 0.0 1,0 2.0 0.0 0.0 0.0 5360.000

-7.0465_89600+04 1.156138540D+03-5.449495540D+00 2.448899984D-02-2.5303848390-05

0.0000000000+00 0.0000000000+00 0.0000000000+00-6.0815635400+05 5.3206754400+01

P(1) Phosphorus Liquid. TPIS 1989.

I TPIS89 P I 00 0.00 0.00 0.00 0.00 2 30.97376 0.000

317 500 6000.000 1 0,0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5360.000

3,1414960110+00 0.000000000D+00 O.O00000000D+O00.O00DOODOOD÷O0 0.000000000D+00

0.000000000D+00 0.000000000D+00 0.000000000D+00-8,6214955_00+02-1.272275042D+01

Pb(cr) Lead Cubic, TPIS 1991, vl, p400, v2, p337.

I TPISgl PB 1 00 0.00 0.00 0.00 0.00 i 207.20000 0.000

200 000 600.650 7 -2.0 -1.0 0.0 1.0 2.0 5.0 4.0 0.0 6870.000

-6.14963571d+05 1.06571168d+04 -7.12985569d+01 2.66839007d-01 -5.18198386d-04

5.23863012d-07 -2.15163077d-10 0.00000000d+00 -4.97404840d+00 3.85580206d+02

Pb(1) Lead Liquid. TPIS 1991, vl, p400, v2, p537.

I TPIS91 PB I O0 0.00 0.00 0.00 0.00 2 207.20000 0.000

600 650 3600.000 5 0.0 1.0 -2.0 2.0 3.0 0.0 0.0 0.0 6870.000

4.36429808d+00 -1.23639276d-03 -3.79817933d÷04 4.94677577d-07 -5.25181763d-II

0.00000000d+00 0.00000000d+00 0.00000000d+00 -8.88753046d÷02 -1.61955968d+01

Rb(cr) Rubidium Cubic Crystal. CODATA 1989. p260. JANAF 12/83.

i CODA89 RB I OO 0,00 0.00 0.00 0.00 1 85.46780 0.000

100 ODO 312.470 6 -2.0 -1.0 0.0 1.0 2.0 3.0 0.0 0.0 ?489.000

-1.69367859d+05 5.11676589d+03 -5.68676003d+01 5.40554509d-01 -9.54799517d-04

1,01751224d-06 O.OODOOOODd+O0 O.O000DOOOd+OD -2,16454707d+0_ 2.80535066d+02

Rb(1) Rubidium Liquid. CODATA 1989. p260.

2 CODAS9 RB I O0 0,00 0,00 0.00 0.00 2 85.46780 0.000

312 470 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 3 0 4.0 0.0 7489.000

2.$6239429d+84 2.86935048d+02 1.54498856d÷00 5 16831217d-03 -6.07029270d-06

3.35063626d-09 -5.18539891d-13 O.O00DO000d+O0 -i 93550099d+03 1.06955958d+D0

1000.000 2100.000 7 -2.0 -I.0 0.0 1.0 2.0 3 0 4.0 0.0 7489.000

-3.67_8669d+05 1.77978869de03 -5.42604680d-01 5 32511098d-03 -4.26280615d-06

1.69980461d-09 -4.41814026d-14 0.00000000d+00 -i 11153067d+04 1._7790546d+01

NAS A/TP-3287/REV 1 131
TABLE VI. - Continued.

S(a) Sulfur Alpha Crystal. TPIS 1989.

i TPISS9 S 1.00 0.00 0.00 0.00 0.00 1 32.06600 0.000

200,OOq 368,300 4 -2.0 0.0 I.O 2.0 0.0 0.0 0.0 0.0 qql2.000

-1.035710779D+0q 1.866766938D+00 4.2561q0250D-03-3.2652522700-06 O.O00000000D+O0

O.O00000000D+O00.O00000000D+O0 0.000000000D+00-7.516389580D+02-7.9610669800÷00

S(b) Sulfur Bela Crys%al. TPIS 1989.

i TPISS9 S 1.00 0.00 0.00 0.00 0.00 2 32.06600 0.000

368,300 388,360 2 0.0 1._ 0.0 0.0 0.0 0.0 0.0 0.0 4q12.000

2.08051q131D+00 2.440879557D-03 O.O00000000D÷O00.O00000000D+O00.O00000000D+O0

O.O00000000D+O00.O00000000D+O0 0.0000000000+00-6.8527147300+02-8.607846750D+00

S(1) Sulfur Liquid. TPIS 1989.

5 TPISB9 S 1.00 0.00 0.00 0.00 0.00 3 32.06600 0.000

388.360 428.150 4 0.0 1.0 -2.0 2.0 0.0 0.0 0.0 0.0 4412.000

2,376860693D+03-7.888076026D+00-6.3665507650+07 7.376076522D-03 0.000000000D+00

O.O00000000D+O0 0.000000000D+00 0.0000000000+00-6.356594920D+05-1.186929589D÷04

q28.150 q52.250 3 0.0 1.0 2.0 0.0 0.0 0.0 0.0 0.0 4412.000

6.928522306D+05-3.2546559810+01 3.824448176D-02 0.000000000D+00 0.000000000D+00

O.O00000000D+O00.O00000000D+O0 0.000000000D+00-9.832222680D+05-5.154806751D+04

432.250 453.150 3 0.0 1.0 2.0 0.0 0.0 0.0 0.0 0.0 4412.000

1.6499456970+02-6.8435349770-01 7.315907973D-04 O.O00000000D+O00.O00000000D+O0

O.O00000000D+O00.O00000000D+O0 0.0000000000+00-2.6388q69290+04-7.681730097D+02

453.150 717.000 4 0.0 1.0 -2.0 2.0 0.0 0.0 0.0 0.0 4412.000

-2.4qi0097530+01 6.0905528890-02 1.972984578D+06-3.744069103D-05 O.O00000000D+O0

O.O00000000D+O00.O00000000D+O00.O00000000D+O0 1.1130134400+04 1.363174183D+02

717.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4412.000

5.848693429D+00 O.O00000000D+O00.O00000000D+O00.O00000000D+O00.O00000000D+O0

0.000000000D+00 0,0000000000+00 0.000000000D+00-8.284589830D+02-I,736128257D+01

Si(cr) Silicon Cubic. TPIS 1991, vl, p237, v2, p220.

2 TPIS91SI 1.00 0.00 0.00 0.00 0.00 1 28.08550 0.000

200.000 298.150 3 -2.0 0.0 1.0 0.0 0.0 0.0 0.0 0.0 3217.471

-2.32353821d+04 2.10202168d+00 1.80922055d-03 O.O0000000d+O0 O.O0000000d+O0

O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0 -7.85063521d+02 -1.05842732d+01

298.150 1690.000 3 -2.0 0.0 1.0 0.0 0.0 0,0 0.0 0.0 3217.471

-5.23255975d+04 2.85016942d÷00 3.97516697d-04 O.O0000000d+O0 O.O0000000d400

O.O0000000d+O0 O.O0000000d+O0 O.O000000Od+O0 -1.04294723d+03 -1.qsBg6419d+Ol

Si(1) Silicon Liquid. TPIS 1991, vl, p237, v2, p220.

1TPIS91 SI 1.00 0.00 0.00 0.00 0.00 2 28.08550 0.000

1690,000 6000,000 1 0.0 0,0 0,0 0,0 0.0 0.0 0.0 0,0 3217.471

3.27138941d+00 O.O0000000d+O0 0.O0000000d+O0 O.O0000000d+O0 O.00000000d+O0

0.00000000d+00 O.O0000000d+O0 O.O0000000d+O0 4.88266711d÷03 -1.32661107d+01

Sn(cr) Tin CrI,_e_ragonal. TPIS 1991, p±l, p350, p_2, p300.

1 IPISgl SN 1.00 0.00 0.00 0.00 0.00 1 118.71000 0.000

200.000 505.118 7 -2.0 -I.0 0.0 l.O 2.0 3.0 4.0 0.0 6323.000

-9.97024407d+05 1.86499589d+04 -1.39295611d+02 5.65260001d-01 -1.22911721d-03

1.39820635d-06 -6.46558qTOd-10 0.00000000d÷00 -8.47956756d+04 7._1772689d+02

Sn(1) Tin Liquid. TPIS 1991, ptl, p350, pt2, p300.

1TPIS91 SN 1.00 0.00 0.00 0.00 0.00 2 118.71000 0.000

505.115 4700.000 4 0.0 1.0 -2.0 2.0 0.0 0.0 0.0 0.0 6323.000

3.02892173d+00 2.53171865d-04 9,84784_31d÷04 -1.96042822d-08 0.000000006+00

O.O0000000d+O0 O.O0000000d+O0 O.O00000DOd+O0 2.20965170d+02 -9.08978377d+00

Sr(a) Strontium Alpha Crystal. Alcock, JPCRD 1992.

2 SRD 92 SR 1.00 0.00 0.00 0.00 0.00 1 87.62000 0.000

100.000 298.150 7 -2.0 -I.0 0.0 1.0 2.0 5.0 4.0 0.0 6558.289

-4.15030815d+03 1.55984581d+02 -2.62349821d-01 2.94539370d-02 -1.21295032d-04

2.40106673d-07 -1.70879069d-10 0.00000000d+00 -1.45579970d+03 5._3525498d+00

298.150 820.000 7 -2.0 -I.0 0.0 1.0 2.0 5.0 Q.O 0.0 6558.289

1.29434497d+05 -1.64609315d+03 1.11106993d+01 -1.97561897d-02 2.91069831d-05

-2.16329158d-08 6.507751_qd-12 O.O0000000d+O0 7.15997756d+03 -5.67135375d+01

Sr(b) Strontium Beta Crystal. Alcock, JPCRD 1992.

I SRD 92 SR 1.00 0.00 0.00 0.00 0.00 2 87.62000 0.000

820.000 1041.000 2 0.0 1.0 0.0 0.0 0.0 0.0 0.0 0.0 6558.289

3.19032631d+00 6.85732655d-04 O.OOnCOOOOd+O0 O.O0000000d+O0 O.O0000000d+00

0.00000000d+00 O.O0000000d+OO 0.00000000d+00 -8.56099126d+02 -I.15723843d+01

Sr[1) S_rontium Liquid. Alcock, JPCRD 1992.

I SRD 92 SR 1.00 0.00 0.00 0.00 0.00 3 87.62000 0.000

10_1.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 6558.289

4.45005178d+00 0.00000000d÷00 0.00000000d+00 0.00000000d+00 0.00000000d+00

O.ODDO0000d+O0 O.O0000000d+O0 0.00000000d÷00 -9.43194037d+02 -I.88970359d+01

132 NASA/TP-3287/REV 1
TABLE VI. - Continued.

la(cr) Tantalum Crystal. JANAF Dec. 1g72,

3 J12/72 TA 1.00 0.00 0.00 0.00 0.00 I 180.94790 0,000

200.000 1000.000 7 -2.0 -1.0 0.0 1.0 2,0 3.0 4.0 0.0 5681.000

1.5199_Ofi3d+04 -q,92714147d+02 6.85560442d+00 -1.36662520d-02 2,56146572d-05

-2.23563067d-08 7.38982999d-12 O.O0000000d+O0 1.23607677d+03 -3.25207475d+01

I000.000 2000.000 7 -2.0 -l.O 0.D 1.0 2.0 3.0 4.0 0.0 5681.000

-1.00139000d÷08 _,69301495d+05 -8.98629582d+02 9,07878690d-01 -5.04024569d-04

1.46307763d-07 -I.73347779d-ll 0.00000000d+00 -2.76010352d÷06 5.93530091d+03

2000.000 3258.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 q.O 0.0 5681.000

1.28624_07d+05 5.62481594d+02 -2.26408665d÷00 6.79174712d-03 -2.94897588d-06

5,06066667d-10 -8.3912_813d-15 D.00000000d+00 -1.57096759d+03 1.97998287d+DI

Ta(1) Tantalum Liquid. JAIIAF Dec. 1972.

I J12/72 TA 1.00 0.00 0.00 0.00 0.00 2 180.94790 0.000

3258.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 O.D 5681,000

5.03216666d_00 0.00000000d+00 0.00000000d_00 0.00000000d+00 0.00000000d+00

0.00000000d÷00 0.00000000d+00 O.O0000000d÷O0 -7.4360_205d+02 -2.59736267d+01

lh(_) Thorium Alpha Crystal. CODATA 1989, p239.

1 CODA89 TH 1.00 0.00 0.00 0.00 0.00 1 252.03810 0.000

200.000 1650.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0 6350.000

-I._5324716d+04 1.50522244d+02 2.27069_76d+00 2.05861456d-03 -9.21661476d-07

Q.31679639d-I0 -7.95065689d-14 0.00000000d+00 -1.66753636dF03 -6.85717696d+00

Th[i)) Thorium Beta Crystal. CODATA 1989. p239.

I COOAS9 IH 1.00 0.00 0.00 0.00 0.00 2 232.03810 0.000

1650.000 2023.000 6 -2.0 -1.0 0,0 1.0 2.0 3.0 0.0 0.0 6350.000

-q.48357108d_06 1.19995994d+04 -1.09903656d+01 8.36771354d-03 -1.87025554d-06

2.02506449d-I0 O.O0000OOOd+O0 O.O000000Od_O0 -7.67962666d+0_ 8.90805067d+01

Th(1) Thorium Liquid. CODATA 1989. p239.

I CODA89 TH 1.00 0.00 0.00 0.00 0.00 3 232.03810 0.000

2023.000 6000,000 1 0,0 0.0 0.0 0,0 0.0 0.0 0.0 0.0 6350.000

5.53249680d+00 0.00000000d÷00 0.00000000d÷00 0.00000000d_00 0.00000000d+00

O.00000000d+O0 O.O0000000d+O0 O.O0000000d+O0 -2.19182510d+03 -2.76007195d+01

Ti(a) Titanium Alpha Crystal. CODATA 1989, p230.

2 CODA89 TI 1.00 0.00 0.00 0.00 0,00 i 47.88000 0,000

200.000 900.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 _.0 0.0 482_.000

3.59859866d+04 -8.27230199d+02 7.68909544d÷00 -1.14396776d-02 1.39210439d-05

-4.69104858d-09 -9.85215763d-13 O.00000000d+O0 2.93661954d+03 -3.98513673d+01

900.000 1156.000 _ -2.0 0.0 1,0 2.0 0.0 0.0 0 0 0.0 _824,000

-2.87623571d+06 4.57315324d_01 -7,69238133d-02 3,79991938d-05 D.ODODO000d÷O0

0.00000000d+00 O.O0000000d+O0 O.O0000000d+O0 -2.03802387d+04 -2.51627018d+02

l_(t_) Titanium Beta Crvstal. CODATA 1989, p230.

! CODAS9 TI 1.00 0.00 0.00 0.00 0.00 Z 47.88000 0.000

1156.000 1944.000 7 -2,0 -i.0 0.0 1.0 2.0 3.0 4 0 0.0 _824,000

-1.62589190d+06 6,28107830d+03 -8,06015068d_00 9.34863930d-03 -3.77346316d-06

1.06605590d-09 -I.13836962d-13 O.00000DOOd+O0 -3.75203373d+04 6.17294291d+01

Ti(1) Titanium Liquid. CODATA 1989, p230,

I CODAS9 TI 1.00 0.00 0.00 0.00 O.O0 3 _7.88000 0.000

Igqq. O00 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0 0 0.0 482_.000

5,62871414d+00 0,00000000d+00 0.00000000d÷00 0.00000000d+00 O.00DOD000d÷OD

0.00000000d+00 0.00000000d+00 0.00000000d+00 -2,37735466d+03 -3.079443q8d+01

U(a) Uranium Alpha Crystal. CODATA, 1989, p234.

i CODASg U 1.00 0.00 0.00 0,00 O.O0 I ?_3.02890 0.000

200,000 942.000 7 -2.0 -I,0 0.0 1.0 2.0 3.0 4.0 0,0 6364.000

-1.54089926d+0_ 2.31880168d÷02 1.22794467d÷00 7.13611700d-03 -1.01803851d-05

1.13688431d-08 -3.66936726d-12 0.00000000d+00 -1.98692173d÷03 -2.03597510d÷00

U(b) Uranium Beta Crystal. CODATA, 1989, p234.

1 CODA89 U 1.00 0.00 0.00 0.00 0.00 2 238.02890 0,000

942.000 1049.000 I 0.0 0.0 0.0 0,0 0.0 0.0 0 0 0.0 6364.000

5.09951879d+00 0.00000000d÷00 0.00000000d+00 O.O000DO00d+DO O.O0000DOOd÷O0

Q flONOfOOOd+O0 O.O0000000d÷O0 0.00000000d+00 -1.67208015d+03 -2.37805012d+01

U(c) Uranium Gamma Crystal. CODATA, 1989, p234.

1CODAS9 U 1.00 0.00 0.00 0.00 0.00 3 238.02890 0.000

1049.000 1408.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0 0 0.0 6364.000

4.60640495d+00 0.00000000d+00 0,00000000d+00 0,00000000d+00 0.00000000d+00

0.00000000d+00 0.00000000d+00 0.00000000d+00 -5.85918728d+02 -i.98080904d+01

U(1) Uranium Liquid. CODA3A, 1989, p23_.

1CODAS9 U 1.00 0.00 0.00 0.00 0.00 4 238.02890 0.000

1408.000 4000.000 7 -2.0 -1.0 0.0 1.0 Z.O 3.0 4.0 0.0 6364.000

-9.46457587d÷04 8.52609383d+02 4.20918_45d+00 8.40688688d-0_ -i.30945011d-07

1,98486896d-ii -1.23147704d-15 0.00000000d+00 -5.95605859d+03 -1.66728821d+01

NASA/TP-3287/REV 1 133
TABLE VI. - Concluded.

V(cr) Vanadium Crystal. JANAF Jun.1973.

3 J 6/73 V 1.00 0.00 0.00 0.00 0.00 1 50.94150 0.000

200,000 600.000 7 -2,0 -i.0 0.0 1.0 2.0 3.0 4.0 0.0 4640,000

2,845123688D+05-5,0949289000+03 3,7150158200+01-1.1760298440-01 2,2558212580-04

-2.2606402550-07 9.2895862400-11 0.000000000D+00 2.254376406D+04-I.9682401530÷02

600.000 1400.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 q.O 0.0 _640.000

1.371575505D+06-7.844377820D+03 2.094284102D+01-2.054425914D-02 1.3223154640-05

-4.0382786100-09 5.0809500500-13 O.O00000000D+O0 4.373041330D+04-1.2922266280+02

1400.000 2190.000 5 -2.0 -1.0 0.0 1.0 2.0 0.0 0.0 0.0 4640.000

3.7797189100+07-9.218606100D+04 8.718887310D+01-3.3819695400-02 5.503768190D-06

O.O00000000D+O00.O00000000D+O00.O00000000D+O0 6.047333670D+05-6.3713089700+02

V(1) Vanadium Liquid. JANAF Jun.1973.

1J 6/73 V 1,O0 0.00 0.00 0.00 0.00 2 50.94150 0.000

2190.000 GO00.O00 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 _640.000

5.5570322240+00 O.O00OO0000D+O00.O00000000D+O00.O00000000D+O00.O00000000D÷O0

O.O00000000D+O0 0.0000000000+00 0.0000000000+00-1.8996164760+03-3.0705315040+01

H(cr) Tungsten Crystal. JANAF Jun.1966.

4 J 6/66 H 1.00 0.00 0.00 0.00 O.OD 1 183.85000 O.DOD

200.000 1000.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 4973.000

-6.8245414100+03-2.2542492110+02 4.976604670D+00-6.926436530D-03 1.2022730150-05

-9.3441337300-09 2.8188871880-12 0.000000000D+00-3.510623140D+00-2.3613350210+01

1000.000 2600.000 7 -2.0 -1.0 0.0 1.0 2.0 3.0 4.0 0.0 4973.000

5.529261560D+05-2.0411592880+05 5.870543020D+00-1.920319341D-05 1.0674799010-06

-2.3547123500-I0 2.1603076820-14 O.O00000000D+O0 1.1636133070+04-3.318832690D+01

2600.000 3200.000 5 -2.0 0.0 1.0 2.0 3.0 0.0 0.0 0.0 4973.000

-I.7932994680+08 2.3565967810+02-1.612066051D-01 4.1432159500-05-3.632045330D-09

O.O00000000D+O0 0.000000000D+00 0.0000000000+00-3,246304260D+05-1,5390185870+03

3200.000 3680.000 4 -2.0 0,0 1.0 2.0 0.0 0.0 0.0 0.0 4973.000

-1.6031146780+08 1.2458223340+02-5.7883564800-02 7.991884200D-06 O.O00000000D+O0

0.000000000D+00 0.0000000000+00 0.000000000D+00-2.286082028D+05-8.568272780D+02

H(1) Tungsten Liquid. JANAF Jun.1966.

1J 6/66 H 1.00 0.00 0.00 0.00 0.00 2 183.85000 0.000

3680.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 4973.000

4.2773416590+00 O.O00000000D+O00.O00000000D+O00.O00000000D+O00.O00000000D÷O0

O.O00000000D+O00.O00000000D+O00.O00000000D+O0 2.754025587D+03-2.086488631D+01

Xe Xenon. NSRDS-NBS 35, 1971. FIXEDN = 5 with FILL,

3 L12/91XE 1.00 0.00 0,00 0.00 0.00 0 131.29000 0.000

200,000 i000.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 _.0 0.0 6197.428

6.60802392d-03 -9.53610408d-05 2.50000053d+00 -1.49716621d-09 2.21314503d-12

-1.64711078d-15 4.8_969606d-19 O.O0000000d÷O0 -7.45374544d+02 6.164_1696d+00

1000.000 6000.000 7 -2.0 -1,0 0.0 1.0 2.0 3.0 4.0 0.0 6197.428

1.10419906d+03 -3.31828724d+00 2.50387762d+00 -2.2519116_d-06 6.86935273d-10

-1.04849430d-13 6.294389_1d-18 D.O0000000d+O0 -7.24304574d+02 6.13680991d+00

6000.000 20000.000 7 -2.0 -i.0 0.0 1.0 2.0 3.0 _.0 0.0 6197.428

1.12165502d+09 -4.37739937d+05 3.09526795d+01 9.40975389d-03 -1.78186678d-06

1.11007715d-10 -2.27006881d-15 O.O0000000d+O0 3.75008887d+06 -3.30380169d+02

ZnCcr) Zinc Crystal. CODATA 1989, p221.

1CODA89 ZN 1.00 0,00 0.00 0.00 D.O0 1 65.39000 0.000

200.000 692.730 7 -2.0 -1.0 0.0 1.0 2.0 3.0 _.0 0.0 5657.000

3.70205418d+05 -5,915_3178d+03 3.95947111d+01 -i.I_372581d-01 1.93434_97d-0_

-1.67536697d-07 6.07811933d-ii O.O0000000d+O0 2.68171703d+04 -2.11483251d÷02

Zn(1) Zinc Liquid. CODATA 1989, p221.

1 C00A89 ZN 1.00 0.00 0.00 0.00 0.00 2 65.39000 0.000

692.730 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5657.000

5.77653043d+00 O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0

O.O0000000d+O0 O.OO000000d÷O0 O.O0000000d+O0 -_.31734581d+02 -1.56707793d+01

Zr(a) Zirconium Alpha Crystal. JANAF Jun.1979.

1J 6/79 ZR 1.00 0.00 0.00 0.00 0.00 1 91.22400 0.000

200.000 1135.000 7 -2.0 -1.0 0.0 1.0 2.0 5.0 _.0 0.0 5_97.000

-I.15369959d+04 2.62620863d+01 2.93205442d+00 5.74336614d-04 -7.65172100d-07

1.59720357d-09 -6.09713165d-13 O.O0000000d+O0 -I.08415351d+03 -1.21577680d+01

Zr(b) Zirconium Beta Crystal. JANAF Jun.1979.

I J 6/79 ZR 1.00 0.00 0.00 0.00 0.00 2 91.22400 0.000

1135.000 2125.000 7 -2.0 -I.0 0.0 1.0 2.0 3.0 4.0 0.0 5497.000

-I.06298870d+06 _.26326338d+03 -3.158058_4d+00 5.00550900d-03 -2.556975_0d-06

7.69131718d-I0 -8.13924831d-14 O.OO000000d+O0 -2.63535516d+04 3.06135955d+01

Zr(1) Zirconium Liquid. JANAF Jun.1979.

1J 6/79 ZR 1.00 0.00 0.00 0.00 0.00 3 91.22400 0.000

2125.000 6000.000 1 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 5497.000

5.03216666d+00 O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0 O.O0000000d+O0

0.00000000d+00 0.00000000d+00 O.0OO00000d÷O0 -1.10079587d+03 -2.5_B06600d+01

134 NASA/TP-3287/REV 1
TABLE VII.- FORMAT FOR THE 7-CONSTANT POLYNOMIAL FORM (OLD FORMAT)

Record Contents Format Columns

...... , ,,i, =, L ....

4

Speciesname

Reference/datecode

Chemical formula, symbols and numbers

"G" forgaseousspecies,"C _ forcondensed

Temperature range

Molecular weight

Integer1

Coefficientsai (i--1,5)in eq. (1)for T >_1000 K

Integer2

CoefficientsbI and b2 ineqs. (2)and (3)for T > 1000 K

Coefficientsai (i--1,3)in eq. (1)for T <_I000 K

Integer3

Coefficientsai (i--4,5)in eq. (1)for T _<I000 K

Coefficientsbi and b2 ineqs. (2)and (3)for T _<1000 K

H° (298.15)/R,K

Integer4

A12

A6

4(A2,F3.0)

A1

2F10.3

F13.5

I1

5E15.8

11

2E15.8

3E15.8

I1

2E15.8

2E15.8

E15.8

11

1-12

19-24

25-44

45

46-65

66-78

80

1-75

8O

1-30

31-75

80

1-30

31-60

61-75

80

Example:

C12 TPIS89CL 2. 0. 0. O.G 200.000 6000.000 70.90540 1

4. 74727508e+00-4. 88581710e-04 2. 68444871e-07-2. 43476083e-11-1. 03683148e-15 2

-1.51101862e+03-3.44551305e-01 2.73638114e+00 7.83525700e-03-1.45104963e-05 3

1.25730834e-O8-4.13247145e-12-1.O5880114e+03 9.44555879e+00 O.O000000Oe+O0 4

Empiricalequationsforabove example (from eqs. (I)to (3)):

C °

Heat capacity: _ = a 1 + a2T + a3 T2 + a4 T3 + asT 4

R

Enthalpy: H°(T) = al , a2 T T 2 T 3 T 4 bl

RT "2 + a3 --3 + a4 n4 + as --5 + --T

Entropy:

T 2 T 3 T 4

S°(T) = aI In T + a2T + a3 __ + a4 __ + as __ + b2

R 2 3 4

NASA/TP-3287/REV 1 135
TABLE VIII. - COEFFICIENTS FOR THE 7-CONSTANT FUNCTIONAL FORM

Ag(cr) CDDA89AG I. 0 O. O.C 200.000 1235.080 107.86820

2,24016573e+00 1,97q35560e-O3-8.70808062e-07 2.18224028e-i0 0.00000000e+00

-6.8062n72qe+O2-8.Oqq65718e+O0 2.22530515e+00 5.622q7272e-O3-1.36678556e-05

1,Sq871758e-OS-6.10518075e-12-8.203qq6qOe+O2-8,7549426qe÷O00.O0000000e+O0

Ag(1) CODA89AG 1. 0 0. O.C 1235.080 6000.000 107.86820

_.01707377e+00 O.O0000O(}Oe+00 0.00000000e+00 0.00000000e+00 0.00000000e+00

-_.66518420e+O2-1.77117176e+Ol 0.00000000e÷00 0.00000000e+00 0.00000000e+00

0.00000000e+00 O.O0000000e÷O0 0.00000000e+00 0.00000000e+00 0,00000000e+00

Al(cr) CODA89AL 1. 0 O. 0.C 200.000 955.610 26.9815_

0.00000000e÷00 0.00000000e+00 O.O0000000e+O00.O0000000e÷O0 0.00000000e+00

0.00000000e+00 0.00000000e+00 1.01040191e+00 1.20769743e-02-2.62083556e-05

2.6q282415e-OS-9.01916513e-12-6.5665q196e+O2-5.00q7125qe+O0 0.00000000e+00

AI(1) CODA89AL I. 0 0. O.C 955.610 6000.000 26.9815_

3.81862551e+00 0.00000000e+00 0.00000000e+00 0.00000000e÷00 0.00000000e+00

-9.49651808e+Ol-l.7522970qe+Ol 3.81862551e+00 0.00000000e+00 0.00000000e+00

0.00000000e+00 O.O0000000e+OO-9._9651808e+O1-1.75229704e+01 0.00000000e+00

Ar L 6/88AR 1 0 O. O.G 200.000 6000.000 59.94800

2.50000000e+00 D.ODO00DOOe+00 0.00000000e+00 O.OODO000De+O00.O00OO00De+O0

-7.q5375000e+02 4.37967_91e+00 2.50000000e+00 O.O0000000e+00 0.00000000e+00

O.O0000000e+O0 O.00000000e+OO-7,45375000e+02 _.57967491e+00 O.O0000000e+O0

B(b) J6/83 B i 0 O. 0.C 200.000 2350.000 10.81100

1.83_9409_e+00 1.79198702e- 3-7.97879_98e-07 2.02764512e-10-1.92028345e-14

-7.83202899e+OZ-l.O6433298e+ 1-I.15931693e+00 1.157771q5e-O2-1.O6985988e-05

2.76106_43e-09 7.31746996e- 3-7.13339210e+01 4.36q39895e+O0 0.00000000e+00

1

2

5

4

1

2

3

1

2

5

1

2

5

4

1

2

3

4

1

2

5

4

B(1) J6/83 B I

3.81862551e÷00 0.00000000e+00

3.36099275e+OS-2.07526_73e+Ol

0.00000000e+00 0.00000000e_00

Ba(cr) SRD 92BA 1

0.000000000+00 0.00000000e+00 0.00000000e÷00 0.00000000e+00 0.00000000e+00

0.000000000+00 0.00000000e+00 2.773344_3e÷00 2.03752236e-03 0.00000000e+00

0.00000000e+00 O.00000000e+O0-9.17Q33810e+D2-8.90970626e+O0 0.00000000e+00

Ba(1) SRD 92BA I O. O. O.C I000.000 6000.000 137.32700

q.81086679e+O00,000000DOe+O0 0.00000000e+00 0.00000000e÷00 0.00000000e+00

-9.92062381e+O2-2.00027571e+01 0.00000000e400 O.O0000000e+00 0.00000000e_00

0.00000000e+00 0.000000000÷00 D.0ODOOOODe+O0 0.00000000e+00 0.00000000e÷00

Be(a) SRD 92BE I O. O. O.C 298.150 1545.000 9.01218

8.06036q68e-Ol 5.373259q6e-O3-_.862q1757e-06 2.39834017e-O9-Q.57186552e-15

-q.lO525129e+O2-q.79961716e+OO-1.3477q902e+DO 1.925_0834e-O2-5.54165425e-05

3.08895143e-O8-1.008147q4e-11-1.96_46005e+02 _.qO835822e+00 O.OO000000e+O0

Be(b) SRD 920E 1 O, 0 O.C 1545.000 1563.000 9.01218

3.60815009e+00 O.O0000000e+ 0 0.00000 OOe+O0 0.00000000e+00 0.00000000e÷00

-8.52229192e+O2-2.0029102qe+ i O.O0000000e+O00.O0000000e+O00.O0000000e+O0

0.00000000e+00 0.00000000e+ 0 0.00000000e+00 O.O0000000e+O0 0.00000000e+00

O. 0. O.C 2350.000 6000.000 10.81100 1

0.00000000e+00 0.00000000e÷00 0.00000000e+00 2

0.00000000e+00 0.00000000e+00 0.00000000e+00 5

O.00000000e+O0 0.00000000e+00 0.00000000e÷00

O. O. O.C 298.150 1000.000 157.32700 1

2

5

1

2

3

1

2

5

Q

i

2

5

Be(1) SRD 92BE I O. 0 0.C 1565.000 6000.000 9.01218 1

5.5q560882e+00 0.00000000e-00 0.00000000e+00 0.0000()(100_-400 0.00000000e÷00 2

2.07475580e÷O2-1.89534126e+01 0.00000000e+00 0.00000000e+00 0.00000000e+00 5

0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e÷00 0.00000000e+00 q

Br2(cr) TPIS89BR 2 O. 0 O.C 200.000 265.900 159.80800 1

D.00000000e+00 0.00000000e+00 0.00000000e÷00 0.00000000e÷00 0.00000000e+00 2

0.00000000e+00 0.00000000e+00 9.125Q599_e+OO-B.26160881e-02 6.99861517e-0_ 5

-2.qO843064e-06 5.21106016e-O9-5.50_O8820e+OS-5.O1727996e+01 0.00000000e+00

Br2(1) TPIS89BR 2 0. O. O.C 265.900 532.505 159.80800 1

0.00000000e400 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

0.00000000e+00 0.00000000e+00 1.04252957e+01 l.l1181227e-Ol-1.06856988e-03 5

S,25976572e-O6-S.27q90598e-O9-5.50620403e+O3-4.go757085e+01 0,00000000e+00

Br2(1) TPIS89BR 2 O. 0 O.C 332.503 6000.000 159.80800 I

9.05669727e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

-2.69988017e+OS-3.32936281e+Ol 9.05669727e+00 0.00000000e+00 O.00000000e+O0 3

0.00000000e÷00 O.O0000000e+OO-2.69988017e+O3-5.32936281e+01 0.00000000e+00

C(gr) X 4/83C 1 O, 0 O.C 200,000 5000.000 12.01100 1

1.45571829e+00 1.71702216e-O3-6.97562786e-07 1.35277032e-10-9.67590652e-15 2

-6.95138814e÷O2-g.52583033e+OO-3.10872072e-Ol _.40353686e-03 1.9039qllge-06 3

-6.585_6966e-09 2.9896_2_8e-12-1.0865079_e+02 I.I1582955e+00 0.00000000e+00

136 NASA/TP-3287/REV l
TABLE VIII.- Continued.

Ca(a) SRD 92CA I. O. 0. O.C 298.150 716 000 40.07800

O.O00OO000e+O00,O00OO000e÷O0 0.00000000e÷00 0.00000000e+00 0.00000000e+00

0.00000000e+00 O.O00OO000e+O0 3.03325649e÷OO-l.41800064e-03 7.26687574e-06

-6.68790594e-09 2.49903889e-IZ-8.93310508e+O2-1.20II4288e÷010.O0000000e+O0

Ca(b) SRD 92CA I. 0 0. O.C 715.000 1115 000 40.07800

5.70111768e+OO-5.81056q90e-03 4. 2212518e-06 O.OOOO0000e+O0 0.00000000e+00

-1.51676361e+O3-2.6075813_e+01 5.70111768e+OO-5.81056690e-03 6.02212518e-06

O.O0000OOOe+O0 O.00000000e+OO-1.51676361e+03-2.60758134e+01 O.00000000e+O0

Ca(1) SRD 92CA I, 0 O. 0 C 1115.000 6000 000 40,07800

6.57032365e+00 O.O0000000e+O0 0. 0000000e+00 0.00000000e+00 O.O0000000e+0g

-9.822q3309e_O2-2.11988645e+Ol 0.00000000e400 0.00000000e400 0.00000000e+00

O.O0000000e+O0

Cd(cr)

0,00000000e+00

0.00000000e+00

-I.34215659e-07

Cd( I )

3

-4

0

O.O00OO000e+O0 O.00000000e+O00.O0000000e+O0 0.00000000e+00

CODA89CD I. 0 0. 0 C 100.000 596 255 112.41100

0.O0000000e+O0 0.00000000e_00 0.00000000e+00 0,00000000e+00

0.00000000e+00 3.74321671e+OO-l.3186380Ie-02 6.92507661e-05

9.12182153e-ll-9.19406477e+O2-1.32372861e+Ol 0.00000000e+00

CODASgCD I. 0 0 0 C 596.258 6000 000 112.41100

,59612292e+00 0.00000000e_00 0.00000000e+00 0.00000000e+00 0.00000000e÷00

.21081626e+02-l.3Z280192e+Ol 3.59612292e+00 0.00000000e400 0.00000000e+00

,00000000e+00 O.00000000e+OO-4.21081626e+O2-1.32280192e+Ol 0.00000000e+00

i

2

3

4

I

2

3

q

I

2

S

4

I

2

5

q

I

2

5

q

C12

4.74727508e+00-6

-1.51101862e+03-3

1.25730836e-08-4

Co(a)

0.00000000e÷00 0

0.00000000e+00 0

_.90692092e-08-2

Co(b)

-2.24784527e+02 7

5.2_697778e+0_ 1

2.29351393e-09 0

Co(b)

TPIS89CL 2.

.88581710e-06 2.68444871e-OT-2.43476083e-ll-l.O36831Q8e-15

.66551305e-01 2.75638114e._00 7.85525700e-O3-1.q510G963e-05

.132_7165e-12-1.D5880114e+03 9.44555879e+00 0.00000000e+00

J 9/67C0 1 0 0 0 C 200 000 700 100 58.95320

.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00

.00000000e+00 1.17055166e+00 1.28077766e-O2-3,49362597e-05

.5_738201e-ll-6.g_569_42e+O2-5,70222736e+O00.O0000000e+O0

J 9167C0 I 0 0 0 C 700 I00 1394 000 58.93320 1

.72645140e-OI-9.73106908e-O_ 5.60893248e-O7-1.11198553e-10 2

.12212928e+03 1.84717559e+00 4.25_3128e-O3-3.94671909e-06 3

.O0000000e+OO-6.09742067e+O2-7.86282629e+00 0,00000000e+00 6

J 9/67C0 1 0 0 0 C 1594 BOO 1768 000 58.93320 1

0 0 0 G 200 000 6000 000 70.90540 I

2

5

6

i

2

5

q

1.25065928e+Oq-3.07370762e+Ol

-3,95275260e_O6-6,51398350e+Oq

0.00000000e+00 O.O0000000e+O0

Co(l)

4.87112289e+00 0

-i.698_9531e+02-2

O.00000000e+O0 0

Cr(cr)

J 9/67C0 1

.O0000000e+O0

.44787531e+01

.O0000000e÷O0

J 6/73CR I

0.00000000e+00 0.00000000e+00

O.O0000000e+O00.O0000000e+O0

-2.30807086e-06 2

Cr(cr)

4,59782637e+00-6

-1.51489668e+O3-Z

-9.15990578e-10 1

Cr(1)

2.87553057e-OZ-l.19356936e-05 1.85463555e-09

0,00000000e+O0

0.O0000000e+O0

0 0 0.C

0. 00000000e+00

O. 00000000e+00

O. O0000000e+O0

0 0 O.C

0. 00000000e-+ 00

2

0,00000000e4-00 O.O0000000e+O0 3

0.00000000e+00 O.O0000000e+O0 4

1768 000 6000 000 58.95320 1

0,000 =O000e+OD O.O0000000e+O0 2

0.00000000e+00 0.00000000e+00 3

0.00000000e+00 O.O0000000e+O0 4

200 000 311 500 51.99610 1

0.00000000e_00 0.00000000e÷00 2

7.84826024e+OO-l.16ZZ6020e-01 8,12369251e-04 3

.35328142e-Og-S.98013946e÷D2-2,75733139e+Ol 0.00000000e÷00 6

J 6/73CR I 0 0. O,C 311 500 2130 000 51,99610 1

.81791132e-03 5.86129756e-O6-Z.07036867e-09 2.82102268e-13 2

.2_54748e+01 1.82863_71e+00 _.19562267e-OS-Z.SZ755082e-06 3

.55203040e-12-7.05502663e+O2-8.69806103e_00 0.00000000e+00 4

J 6/73CR 1 0 0. 0.C 2130 000 6000 000 51.99610 1

4.73028_77e+00 O.O0000000e400 0.00000000e+00 0.000 O000e+O00.O0000000e_OO 2

5.75359221e_O2-Z.45_18309e+01 O.O00OO000e+O0 0.00000000e+00 0.00000000e+00 3

0.00000000e÷00 0.00000000e+00 0.00000000e+00 0.00000000e÷00 0.00000000e+00 4

Cs(cr) CODA89CS 1 O. O. O.C 100 ODO 301 590 132.90543 1

0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

0,00000000e+00 O.O0000000e+O0 3.31157194e+oo-g.67974793e-03 1.19926576e-0_ 3

-5,20608084e-07 8.33615927e-IO-9,80846435e+OZ-8.10866871e+00 O.OOOO0000e+O0 4

Cs(1) CODA89CS 1 O. O. O.C 301 590 2000.000 132.90543 1

5.11512955e+00-3.83970291e-03 2.01555257e-06 3.64202599e-lO-5.4397450ie-14 2

-l.13841767e+O3-1.70567624e+Ol 3.20358130e+00 6.5_560206e-O_-l.gg609_O2e-05 3

1,88Z62490e-OS-6.10371782e-12-8.61341855e+OZ-8.43100388e+00 0.00000000e+00 4

Cu(cr) CODA89CU 1 0. O. O,C 200 000 1358.000 63.54600 1

3.42008910e+OO-l.61201394e-03 3.05145917e-O6-2.11162788e-09 6.99858397e-13 2

-9.90295636e+O2-1.51932294e+Ol 1.76672074e+00 7.34699432e-O3-1,56712960e-05 3

1,50539591e-OS-5.z_g61335e-12-7.43_82087e+OZ-7.70_5404_e+O00.O0000000e+O0 4

Cu(1) CODA89CU I O. O. 0.C 1358 000 6000.000 63.54600 1

5 ,_91076e+00 0.00000000e+00 0.00000000e+00 0,00000000e+00 0.00000000e+00 2

-2.10636669e+OZ-l.83585676e+Ol O,O0000000e+O00.O0000000e+OO 0.00000000e+00 3

0.00000000e+00 0.00000000e+00 0.00000000e+00 0,00000000e÷00 0.00000000e+00 4

NASA/TP-3287/REV 1 137
TABLE VIII.- Continued.

02 IPIS89D 2. O. 0. O.G 200.000 6000.000 4.02820

2.73068929e+00 1.48004781e-O3-4.79314848e-07 7.89496274e-ll-4.88380823e-15

-7.95267504e+02 1.64266094e÷00 3.49546974e+00 2.58348159e-O4-1.31762502e-06

2.42912018e-O-1.05982498e-12-1,04631580e+O3-2.5190553qe+O00.O0000000e+O0

ELECTRON GAS L 6/88E 1 O. O. O.G 200 000 6000.000 0.00055

2.50000000e+00 9.69530988e-14-5.49145356e-17 1.20090954e-20-8.8980ilSOe-25

-7.45375000e+O2-1,17208127e+OJ 2.50000000e+00 O.O0000000e+OO O,O0000000e+OO

0.00000000e÷00 O.O0000000e÷OO-7.45375000e+O2-1,17208127e+Ol 0,00000000e+00

F2 TPIS89F 2 O. O. O.O 200 000 6000.000 37.99881

3.86166219e+00 7.88367679e-O4-1.819829qOe-O7-9.17436560e-12 2.65193472e-15

-I,23238655e+03 2.04119869e+00 3.20832415e+00 1.25919179e-03 3.89747979e-06

-7,22184984e-09 3.31837882e-12-I.O3425794e+03 5.61903603e+00 0.00000000e+00

i

2

3

4

I

2

3

4

I

2

3

4

Fe(a) J 3/78FE I O. O. O.C 200 000 1042.000 55.84700 1

4.69080173e+O3-9.90659991e+00 2.69427446e-03 5.54445321e-O6-3.01659823e-09 2

-l.41547586e+O6-2.49294387e+04 2.41337476e+OO-l.577807_4e-03 2.14701339e-05 3

-3.80171438e-08 2.20426984e-11-7.74380998e+O2-1.O6560296e+01 O.O0000000e+O0 4

Fe(a) J 3/78FE 1

6.59678809e+O2-1.14058217e+OO

-2.52106802e+O5-3.65665236e+05

0.00000000e+00 O.00000000e+O0

Fe(c) J 3/78FE i

6.10109990e+O1-1.60945061e-01

-l.65335454e+O4-3.13710668e+02

0.00000000e+00 0.00000000e+00

Fe(d) J 3/78FE 1

0 0. 0.C 1042 000 I184.000 55.84700 1

4,96308997e-04 O.O0000000e+O00.O0000000e+O0 2

O.OOOO0000e+O00.O0000000e+O00.O0000000e+O0 3

0.00000000e+00 0.00000000e+00 0.00000000e+00 4

0 O. O.C 1184 000 1885.000 55.84700 1

1.68369493e-Oq-7.74563702e-08 1.33091290e-II 2

0.00000000e+00 O.00000000e+O00.O00OO000e+O0 3

O.O0000000e+O00.O0000000e+O00.O0000000e+O0 4

0 0 O.C 1665 000 1809,000 55.84700 1

-4.35904698e+02

1.87925534e+05 2.45057619e+03

O.O0000000e+O0 0,00000000e+00

Fe(1) J 3/78FE I

5.53538332e+00 0.00000000e+ 0

-l.27428941e+O3-Z.94772271e+01

0.00000000e+00 0.00000000e+00

Ge(cr) TPIS91GE i

-I.II030403e+04 2.88119900e+00

7. 68489448e-01-4. 46898892e-04

O. 000000000+00

O. O0000000e+O0

0 0 O.C

0. O0000000e+O0

O. O0000000e+O0

O. 00000000e+00

0 0 O.C

3.68813487e-04

8.67070913e-08 0.00000000e+00 2

0.00000000e+00 0.00000000e+00 3

O.O0000000e+O00.O0000000e+O0 4

1809 000 6000.000 55.84700 1

O.O0000000e+O00.O0000000e+O0 2

O.O0000000e+O0 0.00000000e+00 3

0.00000000e+00 0.00000000e+00

200 000 1211.400 72.61000 1

O.O0000000e+O00.O0000000e+O0 2

-g,23515621e+02-1

-5.69555985e-05 1

Oe(1)

3.31949808e+00 0

3.27896209e÷03-I

0.00000000e+00 0

H2

2.93286579e÷00 8

-8.13065597e+02-I

2.01572094e-08-7

He

2.50000000e÷00

-7._5375000e+02

O.O0000000e+O0

Hg(cr)

O.O0000000e+O0

0.00000000e+00

O.O0000000e+O0

•28754049e+OI-2.29964192e+O3-1.31267063e+02 3.26104791e+00

,68383845e-O7-2.310_3788e+O2-1.52845964e+01 0.00000000e+00

TPIS91GE I 0 0 O.C

.O0000000e+O00.O0000000e+O0

.18601086e+0_ 0.00000000e+00

.O0000000e+O00.O0000000e+00

TPIS78H 2 O. 0 O.G

.28607967e-O4-1.46402335e-07

.02432887e÷00 2.34433112e+00

,37611761e-12-9.17935173e+02

LIO/9OHE 1 O. 0 O.O

O.O0000000e+O00.O0000000e+O0

9.28723974e-01 2.50000000e+00

O.O0000000e+OO-7.45375000e+02

JI2/61HG I O. 0 O.C

0.00000000e+00 0.00000000e+00

0.00000000e+00 2.43103385e+00

O.

3

4

1211.400 6000.000 72.61000 1

O.O0000000e+O0 O.00000000e+O0 2

O.O0000000e+O00.O0000000e+O0 3

O.O0000OOOe+O0 0.00000000e+00 4

200.000 6000.000 2.01588 1

1.54100359e-ll-6.88804432e-16 2

7.98052075e-03-1.94781510e-05 3

8.83010238e-01 O.O0000000e+O0 4

200.000 6000.000 4.00260 1

0.O0000000e+O00.O0000000e+O0 2

O.00000000e+O00.O0000000e+O0 5

9.28723974e-01 O.O0000000e+O0 Q

200.000 234.290 200.59000 1

0.00000000e+00 0.00000000e+00 2

4.24646658e-03 0.00000000e+00 3

O0000000e+OO-l.t7886806e+O3-7.11248114e+O00.O0000000e+O0 4

Hg(1) JI2/61HG I O. O. O.C 234.290 2000.000 200.59000 1

3.03853487e÷00 3.16006666e-04 6.q3901172e-O8-2.92306991e-11 4.86860918e-15 2

-8.88170502e+O2-8.172430IBe+O0 3.79685248e+OO-2.09026109e-03 2,22267107e-06 3

-l.08605655e-lO-4.28087248e-13-1.O5834631e+O3-1.19626936e+Ol 0.00000000e+00 4

I2(cr) TPIS89I 2. 0. O. 0.C 200.000 386.750 253.80894 1

0.00000000e+00 0.O0000000e+O00.O0000000e+O00.O0000000e+O00.O0000000e+O0 2

O.00000000e+O00.OOOOOO00e+OO-l.O5757713e+Ol 2.28905653e-Ol-l.12461645e-03 3

2.41678452e-O6-1.84901377e-O9-8.99721615e+02 3.88598964e+010.O0000000e÷O0 4

12(I) TPIS89I 2. 0. O. O.C 386.750 6000.000 253.80894 1

9.56821268e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

-l.20651948e+03-3.63733927e+01 9.56821268e+00 O.O0000000e+O00.O0000000e+O0 3

0.00000000e+00 O.O0000000e+OO-l.ZOqS1948e+O3-3.63733927e+Ol 0,00000000e+00 4

138 NASA/TP-3287/REV 1
TABLE VIII.- Continued.

KCcr) CODASgK i 0 0. 0.C

0.00000000o+00 0.00000000e+00 0.00000000e400 0

0.00000000e+00 0.00000000e_OO-2.08951123e+O0 6

3,27255823e-07 0,00000000e4-00-6.36098059e+02 9

K(1) CODA89K 1 0 O. 0.C

4.64g54931e+OO-2.Tg174106e-03 1.80836337e-06 3

-1.0]_67797e+O3-1.71767347e+01 4.22910563e+00-7

3.56227270e-Og-l.O5902602e-12-g.q511751qe+02-1

Kr

2.50000000e+00

-7._5375000e+02

0.00000000e+00

Li(cr)

0.00000000e+00

0.00000000e+00

-3.33741023e-08

Li(l_

LIO/90KR 1 0 O. O.G

0.00000000e+00 0.00000000e+00 0

5.49095651e+00 2.50000000e+00 0

O.00000000e+OO-7.45375000e+02 5

TPISg2LI 1 0 0. 0.C

O.O0000000e+O0 0.00000000e+00 0

O.O0000000e+O0 6.10909942e-01 1

7.76629665e-ll-6.Z512IZOSe+02-3

TPIS82LI 1 0 0. O.C

3.89314223e+OO-8.q2787696e-O4 4.45546328e-07-3

-8.22019556e+O2-1.78183077e÷Ol 4.62266638e+00-4

4.2q9600S5e-09 1.23517473e-12-9.58811267e+02-2

Hg(cr) SRD 92MG I 0 0. O,C

200.000 536 860 39 09830

.00000000e+00 0.00000000e+00

.16320193e-O2-2.40731903e-04

.11736910e+00 0,00000000e+00

336.860 2200.000 39 09830

,41244868e-11-4.4878218qe-15

.06885543e-O4-2.12965848e-06

.52340054e+01 0.00000000e+00

200.000 6000 000 83 80000

.00000000e+00 0.00000000e+00

.O0000000e+O00.00000000e+O0

.49095651e+00 0.00000000e+00

200.000 455 690 6 94100

,00000000e+00 0.00000000e+00

,41041217e-O2-1.74958170e-05

.26449967e+00 O.O0000000e+O0

453.690 3000 000 6 94100

.65337454e-II 3.89279220e-15

.06164205e-03 5.91666170e-06

.12778501e+01 0.00000000e+00

298.150 923 000 2q 30500

0.000000000+00 0.00000000e+00 O.O0000000e+O0 0.00000000e+00 0.00000000e+00

0.00000000e+00 0.00000000e+00 1,47884944e+00 9.27430526e-O3-1,g5050788e-05

1.98215527e-OS-7.04927374e-12-7.16649299e+O2-6.57222695e+00 0.00000000e+00

Hg(1) SRD 92MG I 0 0. O.C 923 000 6000 000 24 30500

4.12531827e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00

-6.58934541e+O2-1.93786894e+Ol 4.12531827e+00 0.00000000e)00 0.00000000e÷00

0.00000000e'00 0.00000000e+OO-6.58934341e+O2-1.93786894e+O] 0.00000000e+00

i

2

3

q

I

2

3

4

I

2

3

4

I

2

3

4

i

2

3

4

I

2

3

4

]

2

3

4

Mn(a) J 9/67MN I 0 0, 0,C 200 000 980 000 54 93805 1

0.000000_0e+00 0.00000000e+00 0.00000000e+00 0,00000000e÷00 0.00000000e+00 2

0,00000000e_00 0.00000000e+00 1.57061288e+00 1.00045828e-O2-1.80197969e-05 3

1.73642703e-08-6.17921338e-12-7.25514346e+O2-6.28244690e+00 0.00000000e÷00

J 9/67MN I 0. O. O.C 980 000 1361.000 54 93805 1

2.57015025e-02-3.18989086e-05 1.78851041e-O8-3.74830537e-12 2

1.74432225e+01 3.77430212e+00 7,59739847e-04 0.00000000e+00 3

O.OOO00000e+OO-l.14043577e+O3-1.81351282e+Ol 0.00000000e+00 4

J 9/67MN ] 0 O. 0.C 1361 000 1412 000 54 95805 1

1.28138734e-O2-4.26503238e-06 0.00000000e+00 0.00000000e+00 2

2.82542050e+01 0.00000000e+00 0.00000000e+00 0.00000000e+00 3

Mn(b)

-3.40535059e+00

4.7969022/e+02

0.00000000(.+00

Mn(c)

-4. 3563650Up, [)D

2. 584150')J,.* 03

0. O00000C t)o, 00

Mn(d)

-I .42048_ 'qe' O0

] . 3967¢,h 30,, _U J

O.O00OOOUU_+OO

Mn(l)

5.535383:2e*oG

0,00000000e+00 0.00000000e+00

J 9/67MN I. 0 O. 0.C

8.45822323e-O3-Z.54935141e-06

1.15609126e+01 0.00000000e+00

0.00000000e+00 0.00000000e+00

J 9/67MN i. 0 0. 0.C

0.00000000e+00 0.00000000e+00

-9.59295J_l_L2-_.85_4840ie+Ol 0.00000000e+00

O.000000Uu,)OO 0 00000000e+00 0.00000000e+00

Mo(cr) J 3/78M0 1. 0 O. O.C

0.00000000e+00 0.00000000e+00 4

1412 000 1519.000 54 93805 1

O.O0000000e÷O0 0.00000000e+00 2

0.00000000e+00 0.00000000e+00 3

0.00000000e+00 0.00000000e+00 4

1519 000 6000.000 54 93805 1

0.00000000e+00 0.00000000e+00 2

O,O0000000e+O0 0.00000000e+00 3

0.00000000e+00 0.00000000e+00 4

200 000 2896.000 95 94000 1

5.38432825_,00-6.01622180e-03 6.01q82526e-O6-2.32962338e-09 3.52007808e-13 2

-l.626572ZOe)U3-2.62488891e+Ol 1.32884141e+00 9.S2553689e-O3-2.10929825e-05 3

2.095095ZSe-OS-7.GO703244e-12-6.84364789e+O2-6.29286538e+00 0.00000000e+00 4

Mo(J) J 3/78M0 I. 0 0. 0.C 2896 000 6000.000 95 94000 1

4.52894999e_00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

2.0214066/e_O3-2.2BO74752e+O10.00000000e+O00.O0000000e+O0 0.00000000e+00 3

0.00000000e_00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 4

N2 TPIS78N 2. 0 0. 0.G 200 000 6000.000 28 01348 1

2.95257626e+00 1.39690057e-03-4.9263169Ie-07 7.860 0367e-il-4.60755321e-]5 2

-9.239486_5e402 5.87189252e+00 3.53100528e+00-l.25660987e-O4-5.02999q37e-07 3

2.43530612e-Og-l.40881235e-lZ-l.O4697628e+03 2.96747668e+00 0,00000000e+00 4

Na(cr) CODA89NA i. 0 0. 0.C 200 000 571,010 22 98977 1

0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 O.O0000000e+O0 2

0.00000000e+00 0.00000000e+00 1.23954242e+00 2,00562189e-O2-7.36418252e-05 3

1.02712149e-07 O.O0000000e÷00-8.13320916e+02-4.50651391e+00 0.00000000e+00

Na(1) CODASgNA i. 0 O. 0.C 371 010 2300.000 22 98977 1

4.59858543e+OO-2.42459906e-03 1,32453794e-O6-4.12375317e-11 6.40167081e-15 2

-9.98535534e+O2-1.86257127e÷Ol 4.32382419e+OO-l.41145451e-O3-1.31068846e-07 3

9.17457679e-lO-2.35065070e-I3-9.36522263e+O2-1.72722638e+01 0.00000000e÷00 6

NASAfrP-3287/REV 1 139
TABLE VIII. - Continued.

Nb(cr) JI2/73NB i 0 0. O.C

_.21Q99986e+OO-Z.9068649Ie-03 3. 2396990e-06-I

-l.28682102e+03-1.91976179e+01 1.91200557e+00 6

1.61804090e-08-6. 06602063e-12-7,69037196e+02-8

Hb(I) J12/73{|B I 0 O, O.C

4.02573533e+00 0.00000000e400 0, OO00000e+OD

1.q2706DqTe+O3-1,85790552e+01 O, O000000e+O0

0.00000000e+00

Ne

Z.50000000e+O0

-7.q5375000e+02

O.O000OO00e+O0

Ni(cr)

O.O0000000e+O0

O.O0000000e+O0

-2.75971639e-07

Ni(cr)

0.00000000o÷00 0. 0000000e+00

LIO/gONE i 0 0, O.G

O.O0000000e+O00.O0000000e+O0 0

3.35532272e+00 2,50000000e+00 0

O.O0000000e+OO-7,65375000e+O2 3

JI2/76NI I 0 O. O.C

O.DOOOO00De+OD O. 0000000e+00 0

O,O0000000e+O0 3.92097614e+00-2

1,98530861e-10-8,62387206e+02-1

JI2/76NI I 0 O. O.C

9.58208572e+OO-l,789G5122e-02 1.97185112e-05-9

-2,61782185e+O3-q.74612393e+01 4.85684877e+02-2

200.000 2750.000 92.90638

.27909749e-09 2.09229006e-13

.92396275e-O3-1.5608IZOle-05

.00990261e+00 0.00000000e+00

2750 000 6000.000 92.90638

O.O0000000e_O00.gO000000e÷O0

O.O0000000e÷O0 0.00000000e+00

0,00000000e+00 0.00000000e_00

200 000 6000.000 20.17970

.000 0000e+00 O.O0000000e+O0

.O0000000e_O00.O000DO00e+O0

.35552272e+00 0.00000000_+00

200 000 631.000 58.69000

.00000000e+00 0,00000000e+00

.34184719e-02 1.30230I_Se-04

.56856186e+01 0.00000000e+00

631 000 1728.000 58.69000

.l1957952e-0g 1.58728609e-12

.30395350e+00 q.1062263_e-03

-3.23350101e-06

Ni(1)

4.67989094e+OO

-3.22238346e+O2-Z.33517797e401

0.00000000e+00

02

3.66096083e+00

-1.21597725e+03

-9.68129508e-09

P(cr)

0.00000000e+00

0.00000000e+00

9.49617381e-lO-8,11709085e+O6-Z.25628960e+03 O.O000OO00e+O0

JI2/76NI i 0 O. O.C 1728 000 6000.000 58.69000

0.00000000e+00 0.00000000e+00 0.000 O000e+OO O.O0000000e+O0

O.O0000000e+O0 0

O,O0000000e+O00.O0000000e+O0 0

TPIS890 2 0 O. O.G

6.56365523e-O4-1.61149485e-07 2

3.q153618qe+OO 3.78265636e+00-2

3.2q372836e-IZ-l.06394356e+03 3

TPIS89P 1 0 O. O,C

0,00000000e+00 0.00000000e÷00 0

0.00000000e+00 8.02_69681e-01 1

2.tllOq876e-O7-2,09658894e-lO-6.66362570e+02-2

P(1) TPIS89P 1 0 0. 0.C

3.16169601e*00 0.00000000e+00 0.00000000e+00 0

-8.621q8566e-+OZ-l.ZTZZ7_TZe÷Ol 3.14149601e÷00 0

O.O0000000e+O00.O0000000e+OO-8.6ZlqS564e+02-1

Pb(cr) TPIS91PB 1 0 0. 0.C

0,00000000e+00 0,00000000e+00 0.00000000e+D0 0

,O0000000e+O00.O0000000e+O0

.O0000000e+O00.O0000000e+O0

200 000 6000,000 31.99880

.05797658e-11-1.299132_Se-15

,99673415e-03 9.86730200e-06

.65767573e+00 O.O0000000e+OD

195.600 $17.300 30.97376

,O0000000e+O00,O0000000e+O0

.857793Q7e-D2-8.340807qSe-05

.91281027e+00 O,O0000000e+O0

317,300 6000.000 30.97376

.O000000De+O00.O0000DOOe+O0

.O0000OOOe÷O00.O0000000e÷O0

.27227472e+01 O.O0000000e+O0

200.000 600.650 207.20000

.00000000e+00 0.00000000e+00

O.O0000000e+O00.O0000000e+O0 3.36016248e+OO-6.S152551qe-03 2.10604611e-05

-3.35897357e-08 1.91850988e-11-9.38593007e+O2-1.07608687e+01 O.O000000De+O0

Pb(1) IPISglPB 1 0 O. O.C 600,650 3600,000 207.20000

4.18191355e+OO-9.86150979e-04 3.55339809e-O7-1.75808349e-ll-3.23884_19e-15

-7.56065769e+O2-1.51099545e+Ol 3.qO679935e+O0 2.03221927e-O3-6.17617470e-06

3.08397022e-Og-8.16531438e-13-5.92027769e+O2-1,13377955e+01 0,00000000e+00

Rb(cr) CODA89RB I 0 O, O.C 100.000 312.670 85.46780

O,O0000000e_O00.O0000000e+O00.O0000000e+O00.O0000000e+O00.O0000000e+O0

O.O0000000e+O00.O0000000e+O0 3.55260604e÷OO-1.610q8104e-O2 1.70845564e-04

-6.79689051e-07 9.88583067e-lO-9.7582939Ze+O2-9.76695812e+O00.O00OO000e+O0

Rb(1) CODA89RB 1 0 O. O.C 312.670 2100.000 85.q6780

3.26193993e+00 1.47642720e-O3-2.00176211e-06 1.00852921e-09 4.16113662e-lq

-7.30886458e+OZ-8.79096805e+O0 5.46059088e+OO-l.0089&208e-02 2.07999263e-05

-1.8878123qe-08 6.49377252e-12-1.06594333e+O3-1.87978631e+Ol O.O0000000e+O0

S(crl) TPIS893 I 0 O. O.C 200.000 368,300 32.06600

O.O0000000e+O00,O0000000e+OO O.O0000000e+O00.O0000000e+OO O.O0000000e+O0

O.O0000000e+O00.O0000000e+O0 3.71369512e-01 1.53373501e-O2-3.35q41107e-05

2.89269500e-08 O.O0000000e+OO-5.53213850e+O2-1.5962qq98e+O00.O0000000e+O0

S(cr2) IPIS8gS I 0 O. O.C 368.300 $88.360 32.06600

O,O0000000e+O00.O0000000e+O00,O000OO00e+O0 0.00000000e+00 O.OOOO0000e+O0

0.00000000e+00 0.00000000e+00 2.08033146e+00 2.66137556e-03 0.00000000e+00

O.O000000Oe+O0 O.O0000000e+OO-6.B5306695e+OZ-8.60715_87e+00 0.00000000e+00

S(1) TPIS893 i 0 O. O.C 388,360 6000.000 32.06600

3.50078qlOe+O0 3.81662100e-O4-1.55569962e-07 2.72783689e-ll-l.7281255_e-15

-5.gOS]3035e+02-1.52167270e+Oi-7.2740568_e+01 4.81222534e-Ol-l.07862233e-03

1.03257728e-06-3.5888Q690e-10 8.29134856e÷03 3.152697_3e+02 0.00000000e+00

Si(cr) TPISglSI 1 0 0. O.C 200.000 1690.000 28.08550

1,755_7582e+00 3.17285_97e-03-2.78236_O2e-06 1.26_58065e-09-2.17128_64e-13

-6.28657363e+02-8.553Ql177e+00-l.29176912e-01 l.g7203139e-02-2.76510160e-05

2._1878251e-OB-7.93_SZglZe-12-6.15516_lTe+O2-3.5957BOOEe-Ol O.O0000000e+O0

I

2

3

4

I

2

3

4

1

2

3

4

I

2

3

I

2

3

1

2

3

6

I

2

3

q

i

2

3

I

2

3

4

i

2

3

6

I

2

3

4

1

2

3

4

I

2

3

Q

1

2

3

I

2

3

1

2

3

4

I

2

3

! 40 NASA/TP-3287/REV 1
TABLE VIII. - Continued.

Si(1) TPIS91SI 1

3.27138961e+00 O.O0000000e+O0

6.88286795e+O3-1.32665677e+OI

0.00000000e+00 0.00000000e+00

Sn(cr) TPIS91SN 1

O.O000000Oe+O00.O0000000e+0O

O.O000OO00e+O00.O0000000e+O0

O, 0 O.C 1690 000 6000.000 28,08550

0.00000000e+00 O.O00000OOe+O00.O0000000e+O0

O.O0000000e+OO O.O0000000e+O0 0,00000000e+00

0.00000000e+00 D.O00DDO00e+O00.OOODOODOe+O0

O. 0 O.C 200 000 505.118 118.71000

0.00000000e+00 O.O0000000e+O00.OOOO0000e+O0

2.96216499e_OO-1.73632774e-03 1.74091602e-05

-3.62710022e-08 2.91162756e-ll-9.01862907e+O2-1.O7168937e+01 O.O0000000e+O0

Sn(1) TPIS91SN 1 0. 0 O.C 505 118 4700.000 118.71000

3.41798639e+OO-2.13956362e-O4 l.)8624849e-O7-4.50904210e-11 3,63163537e-15

-9.50693870e+Ol-l.16564066e+Ol 6.03781588e400-l.O9309103e-02 1.72515982e-05

-I.26580001e-08 3.66069018e-12-6.28932703e+O2-2.40877225e+01 0 O0000000e+O0

Sr(a) SRD 923R 1 O. 0 0.C 298 150 820.000 87.62000

O,O0000OOOe+O00.O00OO000e+OO O.O0000000e+O00.O0000000e+0O 0 O000OO00e+O0

O.O0000000e+O00.O00000OOe+O0 2,61121855e+00 3.06925896e-O3-4.q3980854e-06

4.03526789e-O9-1.qBOg7835e-12-8.83002675e+O2-g.o1331093e+O0 0 O0000000e+O0

Sr(b) SRD 925R 1 0 0 O.C 820 000 1061.000 87.62000

5.19032631e+00 6.83752655e-06 O. O000000e÷O0 Q.O0000000e+O0 0 O0000000e+O0

-8.56080629e+OZ-l.IS725466e÷Ol 3. 9032631e+00 4.83732655e-06 O.O0000000e400

0.00000000e+00 0.O0000000e+00-8.56080629e+02-1.15723_66e+01 0 0000000De+00

Sr(1) SRD 925R 1 0 0 O.C 1041 000 6000.000 87.62000

4.45005178e+00 0.00000000e400 0.00000000e_00 0.00000000e+00 0 00000000e+00

-9.63175560e+O2-1.88969962e+01 O.0OO0000De+O00.O000DO00e+O00,O00ODO00e+O0

O.O0000000e+O00.O0000000e+O00.O00QO000e+O00.O0000000e+O00.0OO00000e+O0

Ta(cr) JI2/72TA 1 0 0 O,C 200.000 3258.000 180.94790

2,89594963e+00 5.33759133e-OT-3.59146721e-O8-7.20761661e-11 3.13302008e-16

-8.71255826e÷O2-1.16Q60280e+01 2.32998499e+00 4.45028602e-O3-q.52262819e-06

9.87829159e-O9-3.78308606e-12-8.26091667e+O2-9.27093666e+O00.ODO00000e+OO

Ta(1) JI2/72TA 1 0 0 O,C 3258 000 6000.000 180.94790

5.03216666e+00 O.O00000OOe+DO O.OODO00OOe+O00.OODO0000e+O00.OOODOO00e+O0

-7.46223758e+O2-2.59736577e+01 O.0OO00000e_O00.OOOO0000e+O00.O00OOODOe+O0

O.O00000OOe+O00.O0000000e+O0 0.00000000e+00 0.00000000e÷00 O.O0000000e+O0

Th(a) CODA89TH I 0 0 O,C 200 000 1650.000 232.03810

2.68373118e+00 1.47036888e-O3-6.27773953e-07 2.04762385e-lO-3.65532090e-16

-8.48608536e+O2-9.64661965e+O0 2.72997787e+00 1.95817381e-O3-Z.55796677e-06

2,92240279e-O9-1.15807462e-12-8.83606615e+O2-9.81629986e+O00.OOOO0000e+O0

l h(b) CODA891H i 0 O. O.C 1650 000 2023.000 232.03810

3.95235367e+OO-3.O5562000e-03 3.66314418e-O6-1.3260909Ie-09 1.79849780e-13

-1.78233192e+D2-1.68000708e+01 O.OOOO0000e+O0 0.00000000e+00 O.O000DO00e+O0

D.OOODOODOe+00 O.O0000ODDe+OD D.OODO000De+OD

Th(1) CODA89TH I 0 O. O.C

5,53269680e+00 O.O0000000e+ 00.OOOO0000e400

-2.19180941e+O3-2.76001205e+ i O.O0000000e+O0

O,O0000000e+O00.O0000000e+ 00.O0000000e+O0

Ti(a) CODASgTI 1 0 O. O.C

2.97987171e+O1-5.67369024e-02 3.08687350e-05

-9.27557025e+O3-1.56730793e+02 1.32829640e+00

2,17468998e-OB-7.66060428e-12-7.06881064e+O2-6.19722912e+O0

0.00000000e+00 O.OOOOOO00e+O0

2025 000 6000.000 232.03810

0.00000000e+00 0.00000000e÷00

O.O0000000e+O00.O0000000e+O0

O.O0000000e÷O00.O0000000e+O0

200 000 1156.000 67 88000

O.O0000000e+O00.O0000000e400

1.06776117e-O2-Z.19816539e-05

O.O000DO00e+O0

Ti(b) CODA89TI I

6,55050938e+OO-5.78666836e- 3

-1.86695726e÷O2-1.97953060e+ 1

O,0OO00000e+O00.O0000000e+O0

Ti(l) CODA89TI i

5,62871416e+00 0.00000000e+ 0

-2.37509598e+O3-3.07872691e+ I

O.O0000000e+O0 O.O0000000e+ 0

U(a) CODA89U 1

0.00000000e+00 0.00000000e+ 0

O,O0000000e+O00.O0000000e+O0

0 0. 0.C 1156 000 1946.000 67 88000

6.58628776e-06-2.60523686e-09 6.06930218e-13

O. O0000000e+O0

O. O0000000e+O0

0 O. O.C

O. O0000000e+O0

0.00000000e+00

O. O0000000e+O0

0 O. O.C

0. 00000000e+00

2.59603330e÷00

O.O0000000e+O00.O000OO00e+O0

O.O0000000e+O00.O0000000e+O0

1966 000 6000.000 47 88000

O.O0000000e÷0O 0.00000000e+00

O.O0000000e*O00.O000OO00e+O0

O.O0000000e+O00.O0000000e+O0

200 000 942.000 238 02890

0.00000000e+00 0.00000000e+00

3.07896699e-O3-3.79092ISOe-06

6,28660576e-O9-2,06728510e-12-8,88811048e+O2-9.55446643e+O00.O0000000e+O0

U(b) CODA89U I 0 O. 0.C 942.000 1049.000 238 02890

5.09951879e+00 O.O0000000e+O00.O0000000e+O00.O0000000e÷O00.O0000000e+O0

-l,67210741e+O3-2.3780340ge+Ol 5.09951879e+00 O.O0000000e+O0 0.00000000e+00

0,00000000e+00 O.00000000e+OO-l.67210741e+O3-2.37803606e+Ol 0.00000000e+00

U(c) CODA89U 1 0 0. O.C 1049.000 1408.000 238 02890

4,60640495e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00

-5.85965991e+OZ-l.98081297e+Ol 0.00000000e+00 0.00000000e+00 0.00000000e+00

O.O0000000e+O00.O0000000e+O00.O0000000e+O00.O0000000e+O00.OO000000e+O0

I

2

3

4

I

2

3

4

I

2

3

6

i

2

3

4

I

2

3

6

1

2

3

4

i

2

3

4

I

2

3

4

i

2

3

4

i

2

3

6

1

2

3

6

I

2

3

6

i

2

3

6

1

2

3

4

1

2

3

4

1

2

3

4

1

Z

3

4

NASA/TP-3287/REV 1 141
TABLE VlII.- Concluded.

U(1) CODA89U 1 O. 0 O.C 1408.060 4000.000 258 02890 1

5.78808331e+O6-_.O7320558e-O_ 3.58822296e-O7-7._210363Ie-ll 5.8178_231e-15 2

"-l.066616q2e+O3-2.73Q91825e+Ol 0.00000600e+00 O.O0000000e+O00.O0000000e+O0 3

O.O0000000e+O00.O0000000e+OO O.O0000000e+O00.O0000000e+O00,O0000000e+O0 4

V(cr) J 6/73V 1 0. 0 0,C ?NO.noN 2]90.000 50 94150 1

4.48215589e+OO-_.E5728053e-03 5.38325211e-06-2._,.'_,,,,,.I!_, • uO _,25981192e-13 2

-l.28420195e+OS-Z.12401625e+Ol 8.64273023e-01 1.403012]Oe-O2-3,152Z8495e-05 3

3.16728638e-OS-l,l_327_59e-ll-6.59969586e+O2-4.4835226Be÷O00,O0000000e+O0

V(1) J 6/73V I

5.55703222e+00 O.O0000000e+O0

-l.89958163e+OS-S.O7034308e+Ol

O.OO000000e+O00.O0000000e+O0

H(cr) J 6/66H i

3.qO55690e+OO-2.72526866e-03

-l.16651320e+O3-1,8048694_e+Ol

O. 0 O.C 2190.000 6000.000 50 94150 1

O.O0000OOOe+O0 0,00000000e+00 O.OOOO0000e+O0 2

O.O0000000e+O0 0.00000000e100 O.O0000000e+O0 3

O.O0000000e÷O0 0,00000000e+00 O.O0000000e+O0 4

O. 0 O.C 206.000 3680.000 183 85000 1

5.258_7851e-O6-1.37908465e--Og 2.10706661e-13 2

1.63062672e+00 8.86791910e-'O3--2.117275qle-05 3

2.25276259e-OS-8.54546896e-12-7.33745920e÷O2-?.26762635e+00 0.00000000e+00

H(1) J 6/66N I O. 6 O.C 3680.000 6000.006 183 85000 1

6.27734166e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 0.00000000e+00 2

2.75282232e+O3-2.08636176e+Ol O.O0000000e+O0 0.00000600e400 O.OOOO0000e+O0 3

O.O0000000e+O00.OOO00000e+O00.O0000000e+O00.O0000000e+O00.O0000000e+O0 4

Xe LI2/91XE 1 0 0 O.O 200.000 6000.000 131 29000 1

2.50005322e+OO-l,05136544e-07 6.75326897e-ll-l.70964909e-lq I._7681049e-18 2

-7,_5394186e+02 6.16412898e+00 2.50000000e+OO-8.99141330e-l_ 2.52196860e-16 3

-2.92186662e-19 1.18969218e-Z2-7,45375000e+02 6.16441993e+00 O.O00000OOe+O0

Zn(cr) CODA89ZN 1 0 0 0.C 200,000 692.730 65 39000 1

O.O00OO000e÷O00.O0000006e+O00.OOflOOOOOe÷00 O.O0600000e+O0 0.60000000e+00

O,O0000600e+O00.0OO00000e+O0 1.85068929e*00 9.17791610e-O3-2.61047009e-05

3.38568767e-O8-1.39630709e-ll-7.89403133e+O2-7.38526333e+O00.O0000000e+O0

Zn(l) CODA89ZN 1 0 0 O.C

3.77653063e+00 O.O0000000e+OO O,00000000e+O0 0

-4.31695298e+O2-1.56708_37e+Ol 3.77653643e+00 0

0.00000000e+00 O.00000060e+O6-4.31695298e+02-1

Zr(a) J 6/79ZR 1 0 O. O.C

2.28119546e+00 1.66971686e-D3-1.0Q657616e-08 0

-6,61803147e+O2-8.57377198e+O0 2.18288840e+00 5

1.31132729e-O8-Q.83818355e-12-8.08441355e+02-8

692.730 6000.000 65.39000

.OO000000e+O00.06000000e+O0

.O00000OOe+O00.O0000000e+O0

.567084_7e+010.O0000000e+O0

200.000 1135.000 91.22400

.O0000000e+O00.O0000000e+O0

._2886393e-O3-1.21463952e-05

.94741836e+00 0.00000000e+00

Zr(b) J 6/79ZR 1

4.06876245e+OO-l.58_89721e-03

-6.91172261e+O2-1.78593403e+OI

0.00000000e+00 0.00000000e+00

Zr(1) J 61792R 1

5.03216666e+00 O.O000DO00e+O0

-l.lO084626e+O3-2.56797587e+Ol

O.O0000000e÷O00.O0000000e+O0

2

3

4

I

2

3

4

I

2

3

0 O. O.C 1135.000 2125.000 91.22400 1

1.02995129e-O6-1,55767557e-lO 2.30286611e-14 2

O.O00OO000e+O00.O0000000e+O0 0.00600000e+60 3

O.O0000000e+O00.O0000000e+O00.O0000000e+O0

0 O. O.C 2125.000 6000.000 91.22400 1

O.O0000000e+DO O.O0000000e+O0 0.00000000e+00 2

O.O0000000e+O00.O0000000e+O00.O0000000e+O0 3

O.O0000000e+O0 O.O0000000e÷O00.O0000000e+O0

142 NASA/TP-3287/REV 1
TABLE IX.1. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Ag(cr,0

r C o HO(T)-H°(O) S°(O _G°OS-H°(O)W PPCO _°(ryr T

K JIm_l.K _/m_ J_oI-K J/moI-K _ol J_oI.K K

0 0.000 0.000 0.000 0,000 -5.745 INFINITE 0

200 24.147 3.298 32.611 16.120 -2.447 44.845 200

298.15 25.350 5.745 42.550 23.281 0.000 _2.550 298.15

300 25.359 5.792 42.707 23.400 0.047 42.550 300

400 25.811 8,350 50.064 29,188 2.605 43.551 400

500 26.350 10.957 55.879 33.96_ 5.212 45._54 500

600 26.976 13.623 60.738 38.032 7.878 _7.607 600

700 27.641 16.354 64,946 41,583 10.609 _9.790 700

800 28.315 19,152 68.681 44.741 13.407 51.922 800

900 28.990 22.017 72.055 47,592 16.272 53.975 900

1000 29.665 24.950 75.144 50.194 19.205 55.939 1000

1100 30.345 27.950 78.003 52.594 22.205 57,817 1100

1200 31.034 31,019 80,673 54.824 25.274 59.612 1200

1235.08 33.400 43.112 90._77 55.571 57.367 60,223 1235.08

1300 33.400 45.280 92.188 57.357 39.535 61.776 1300

1400 33.400 48.620 94.663 59.935 42.875 64.038 1400

1500 33.400 51.960 96.968 62.328 46.215 66.158 1500

1600 33.400 55.300 99.123 64.561 49.555 68.151 1600

1700 33.400 58.6_0 101.148 66.65_ 52.895 70.033 1700

1800 33.400 61.980 103.057 68,62_ 56.235 71.816 1800

1900 33.400 65.320 104.863 70._8_ 59.575 73.508 1900

2000 53.400 68.660 106.576 72.246 62.915 75.119 2000

2100 33.400 72.000 108,206 73,920 66.255 76.656 2100

2200 33.400 75.340 109,760 75.514 69.595 78.126 2200

2300 33.400 78.680 111.244 77.036 72.935 79.5_3 2300

2400 33.400 82.020 112,666 78.491 76.275 80.885 2400

2500 33.400 85,360 114.029 79.885 79.615 82.183 2500

2600 33.400 8_.700 115.339 81.224 82.955 8_.433 2600

2700 33.400 92.040 116.600 82.511 86.295 84.639 2700

2800 33.400 95.380 117.815 83.750 89.635 85.802 2800

2900 33.400 98.720 118.987 84.945 92.975 86.926 2900

3000 33.400 102.060 120.]19 86.099 96.315 88.014 3000

3100 33.400 105.400 121.214 87.214 99.655 89.067 3100

3200 33.400 108.740 122.274 88.293 102.995 90.088 3200

3300 33.400 112.080 123.302 89.339 106.335 91.079 3300

3400 33.400 115.420 124.299 90.352 109.675 92.0_2 3400

3500 33.400 118.766 125.268 91.336 113.015 92.977 3500

3600 33.400 122.100 126.208 92,292 116.355 93.888 3600

3700 33.400 125.440 127.12_ 93.221 119.695 9_.773 3700

3800 33.400 128.780 128,014 94.125 123.035 95.637 3800

3900 33.400 132,120 128.882 95.005 126.375 96.478 3900

4000 33.400 135.460 129.727 95.862 129.715 97.299 4000

4100 33.400 138.800 130.552 96.698 133.055 98.100 4100

4200 33.400 142.140 131.357 97.514 136.395 98.882 4200

_300 33.400 1_5._80 132.143 98.310 139.735 99.646 4300

4400 33.400 148.820 132.911 99.088 143.075 100.394 4400

4500 33.400 152.160 133.661 99.8_8 I_6._15 101.125 _500

4600 33.400 155.500 134.396 100.591 149.755 i01.840 4600

4700 33.400 158.840 135.114 101.318 153.095 102.540 4700

4800 33.400 162.180 135.817 102.O29 156.435 193.226 4800

_900 33.400 165.520 136.506 102.726 159.775 103.898 4900

5000 33._00 168.860 137.180 103.408 163.115 104.557 5000

5100 33.400 172.200 137.842 10_.077 166.455 105.204 5100

5200 33.400 175.540 138.490 104.733 169.795 105.837 5200

5300 33.400 178.880 139.127 105.376 173.135 106.460 5300

5400 33._00 182.220 139.751 106.006 176.475 107.070 5400

5500 33.400 185.560 140.364 106.626 179.815 107.670 5500

5600 33._00 188.900 I_0.966 107.233 183,155 108.259 5600

5700 33.400 192.2_0 141.557 107.830 186.495 108.838 5700

5800 33.400 195.580 1_2.138 108.617 189.835 109.407 5800

5900 33.400 198.920 1_2.709 108.993 193.175 109.967 5900

6000 33.400 202.260 1_3.270 109.560 196.515 110.517 6000

NASA/TP-3287/REV l 143
T . C °

K J/moPl-K

0 0.000

230 21.340

298.15 24.200

300 24.234

400 25.734

500 26.910

600 28.044

700 29.344

800 31.005

TABLE IX.2. - THERMODYN/I_0C FUNCTIONS FROM COEFFICIENTS FOR AJ(cr,t)

_(r)-_(o) so(r} <G°('r)-H*(o)}rr H*(T)

kJ/m_ J/moI-K J/moI-K k,J/mol

0.000 0.000 0.000 -4.540

2.282 19.152 7.741 -2.258

4.540 28.300 13.073 0.000

4.585 28.450 13.167 0.045

7.088 35.640 17.921 2.548

9.721 41.512 22.069 5.181

12.468 46.517 25.737 7.928

15.336 50.934 29.026 10.796

18.349 54.956 32.020 13,809

_*(WT

J/moI-K

INFINITE

30.441

28.300

28.300

29.271

31.149

33.303

35.512

37.695

T

K

0

200

298.15

300

400

500

600

700

800

900 33.211 21.555 58.729 34.779 17.015 39.824 900

cr 935,61 34.104 22.686 59.963 35.664 18,]46 40.527 933.61

1000 31.750 35.494 73.605 38.111 30.954 42.651 1000

ii00 31,750 38.669 76.631 41.478 34.129 45.605 II00

1200 31.750 41.844 79.394 44.524 37.304 48.307 1200

1300 31.750 45.019 81.935 47.305 40.479 50.798 1300

1400 31.750 48.194 84.288 49.864 43.654 53.107 1400

1500 31.750 51.369 86.479 52.233 46.829 55.259 1500

1600 31.750 54.544 88.528 54.438 50.004 57.275 1600

]700 31.750 57.719 90.452 56.500 53.179 59.171 1700

1800 31.750 60.894 92.267 58.437 56.354 60.960 1800

1900 31.750 64.069 93.984 60.263 59.529 62.653 1900

2000 31.750 67.24_ 95.612 61.991 62.704 64.261 2000

2100 31.750 70.419 97.162 63.629 65.879 65.791 2100

1200 31.750 73.594 98.639 65.187 69.054 67.250 2200

2300 31.750 76.769 100.050 66.672 72.229 68.646 2300

2400 31.750 79.944 101.401 68.091 75.404 69.983 2400

2500 31.750 83.119 102.697 69.450 78.579 71.266 2500

2600 31.750 86.294 103.942 70.753 81.754 72.499 2600

2700 51.750 89.469 105.141 72.004 84.929 73.686 2700

2800 31,750 92.644 106,295 73.208 88.104 74.830 2800

2900 31.750 95.819 107.410 74.369 91.279 75.934 2900

3000 31.750 98.994 108.486 75.488 94.454 77.001 3000

3100 31.750 102.169 109.527 76.569 97.629 78.034 3]00

3200 31.750 105.344 110.535 77.615 100.804 79.034 3200

3300 31.750 108.519 111.512 78.628 103.979 80.003 3300

3400 31.750 111.694 112.460 79.609 107.154 80.944 3400

3500 31.750 114.869 113.380 80.561 110.329 81.858 3500

3600 31.750 118.044 114.275 81,485 113.504 82.746 3600

3700 31.750 121.219 115.145 82.383 116.679 85.610 3700

3800 31.750 124.394 115.991 83.256 119.854 84.451 3800

3900 31.750 117.569 116.816 84.106 123.029 85.170 3900

4000 31.750 130.744 117.620 84.93_ 126.204 86.069 4000

4100 31.750 133.919 118.404 85.741 129.579 86.848 4100

_200 31.750 137.094 119.169 86.528 132.554 87.609 4200

4300 31.750 140.269 119,916 87.295 135.729 88.351 4300

4400 31.750 143.444 120.646 88.045 138.904 89.077 4400

4500 31.750 146.619 121.359 88.778 142.079 89.786 4500

4600 31.750 149.794 122.057 89.493 145.254 90.480 4600

_700 31.750 152.969 122.740 90.19_ 148.429 91.160 4700

4800 51.750 156.144 123.409 90.879 151.60_ 91.824 4800

4900 31.750 159.319 124.063 91.549 154.779 92.476 4900

5000 31.750 162.494 124.705 92.206 157.954 93.114 5000

5100 31.750 165.669 125.333 92.8q9 161.129 93.740 5100

5200 31.750 168.844 125,950 93.480 164.304 94.353 5200

5300 31.750 172.019 126.555 94.098 167.479 94.955 5300

5400 31.750 175.194 127.148 94.705 170.654 95.546 5400

5500 31.750 178.369 127.731 95.300 175.829 96.126 5500

5600 31.750 181.544 128.303 95.884 ]77.004 96.695 5600

5700 31.750 184.719 128.865 96.458 180.179 97.254 5700

5800 31.750 187.894 129.417 97.012 183.354 97.804 5800

5900 31.750 191.069 129.960 97.575 186.529 98.345 5900

6000 31.750 194.244 130.493 98.119 189,704 98.876 6000

144 NASA/TP-3287/REV l
T

K

0

ZOO

298.15

3O0

40O

5O0

600

700

800

900

100o

Ii00

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

240O

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

_400

4500

4600

4700

4800

q900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

TABLE IX.3. - THERMODYNAMIC FUNCTIONS FROM COEFP1CIENT8 FOR/u

Co Hoo.).t_(_ S=(T) HGoO-).W(o)}rr _(T) _°(T)ff T

JIm_l-K kJ/mol J/mo_-K _mol.K _ J/mo_K K

0.000 0.000 0.000 0.000 -6.197 INFINITE 0

20.786 4.157 146.547 125.761 -2.040 156.748 200

20.786 6.197 154.847 134.060 0.000 154.847 298,15

20.786 6.236 154.975 13_.189 0.038 154.847 300

20,786 8.315 160.955 140,169 2.117 155.662 400

20.786 10.393 165.593 144.807 4.196 157.202 500

20.786 12.472 169.383 148.597 6.274 158.926 600

20.786 14.550 172.587 151.801 8.355 160.655 700

20.786 16.629 175.365 154.577 10.432 162.324 800

20.786 18.708 177.811 157.025 12.510 163.911 900

20.786 20.786 180.001 159.215 14.589 165.413 1000

20.786 22.865 181.982 161.196 16.667 166.830 1100

20.786 24.944 183.791 163.005 18.746 168.169 1200

20.786 27.022 185.455 164.669 20.825 169.436 1300

20.786 29,101 186,995 166.209 22.903 170.656 1400

20.786 31,179 188.429 167.643 24.982 171.775 1500

20,786 33.258 189.771 168.985 27.061 172.858 1600

20.786 35.337 191.031 170.245 29.139 173.890 1700

20.786 57.415 192.219 171.435 31.218 174.876 1800

20.786 59.494 193.343 172.557 33.296 175.819 1900

20.786 41.573 194.409 173.623 35.375 176.722 2000

20.786 43.651 195._25 174.637 37.454 177.588 2100

20.786 45.730 196.390 175.604 39.532 178.421 2200

20.786 47.808 197,314 176.528 41.611 179.223 2300

20.786 49.887 198.199 177.415 43.690 179.995 2400

20.786 51.966 199.048 178.261 45.768 180.740 2500

20.786 54.044 199,863 179.077 47.847 181._60 2600

20.786 56.123 200.647 179.861 49.926 182.156 2700

20.786 58.202 201,403 180.617 52.004 182.830 2800

20,786 60.280 202.133 181.346 54.083 183.483 2900

20.786 62.359 202.837 182.051 56.161 184.117 3000

20.786 64.437 203.519 182.733 58.2_0 184.732 3100

20.786 66.516 204,179 183.393 60.319 185.329 3200

20.786 68.595 204.819 184.032 62.597 185.910 3300

20.786 70.673 205.439 184.653 64.476 186.476 3400

20.786 72.752 206,0_2 185.255 66,555 187.026 3500

20.786 74.831 206.627 185.841 68,633 187,562 3600

20,786 76.909 207.197 186.410 70.712 188.085 3700

20.786 78.988 207,751 186.965 72.790 188.596 3800

20.786 81.066 208.291 187.505 74,869 189.094 3900

20.786 83.145 208.817 188.031 76,948 189.580 4000

20,786 85.224 209.331 188,544 79.026 190.056 4100

20.786 87.302 209.831 189.045 81.105 190.521 4200

20.786 89.381 210.321 189.534 83.184 190.976 4300

20.786 91.460 210.798 190.012 85.262 191.421 4400

20.786 93.538 211.266 190.479 87.341 191.856 4500

20.786 95.617 211.722 190.936 89,419 192.283 4600

20.786 97.695 212.169 191.383 91.498 192,702 4700

20.786 99.774 212.607 191.821 93.577 193.112 4800

20.786 101.853 213.036 192.249 95.655 195.514 4900

20.786 103.931 213.456 192.669 97.73_ 193.909 5000

20.786 106.010 213.867 193.081 99.813 194.296 5100

20.786 108.089 214.271 193.485 101.891 194.676 5200

20.786 110.167 214.667 193.880 105.970 195.050 5300

20.786 112,246 215.055 194.269 106.0_8 195.417 5400

20.786 114.325 215.437 194.650 108.127 195.777 5500

20.786 116.403 215.611 195.025 110.206 196.132 5600

20.786 118.482 216.179 195.393 112.284 196.480 5700

20.786 120.560 216.541 195.754 114.363 196.823 5800

20.786 122.639 216.896 196.110 116.44Z 197.160 5900

20.786 124.718 217.245 196.459 118.520 197.492 6000

20.817 128.879 217.928 197.141 122.681 198.140 6200

20.818 133.043 218.589 197,801 126.845 198.769 6400

20.803 137.205 219.229 198._40 131.007 199.379 6600

20.781 141.363 219,850 199.061 135.166 199,972 6800

20.759 145.517 220._52 199.664 139.320 200.549 7000

20.740 149.667 221.036 200.249 1_3.470 201.110 7200

20.726 153,814 221.604 200.819 147.616 201.656 7400

20.718 157.958 222.157 201.373 151.761 202.188 7600

20.716 162.101 222.695 201.913 155.904 202.707 7800

20.719 166.245 223.220 202.439 160.047 203.214 8000

145

NASA/TP-3287/REV 1
T

K

8200

8400

8600

88O0

9000

9200

9400

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

2000O

o:

,Jhnol-K

20.726

20.736

20.748

20.762

20.777

20.792

20.807

20.821

20.836

20.851

20.891

20.948

21.039

21.183

21.402

21.719

22.152

22.718

23.430

24.295

25.311

26.475

27.770

29.174

30.656

32.176

33.682

35.11_

56.403

37.466

H°_)-H°(O)

_/mol

170.389

174.535

17&.684

182.835

186.989

191.145

195.305

199.468

203.634

207.803

218.238

228.697

239.192

249.744

260.387

271.163

282.125

293.337

304.868

316.793

329.188

342.129

355.685

369.917

384.872

400.579

417.045

434.249

452.136

470.614

TABLE

J/moi-K

223.731

224.231

224.719

225.196

225.663

226.120

226.567

227,005

227,435

227.856

228.874

229.847

230,780

231,678

232.5_7

233.392

234.220

235.035

235.844

236.653

237.466

238,287

239.121

239.971

240.838

241.723

242.625

243.5_3

244.472

245.407

IX.3. - Conc_uaed,

tG°0")-H°(O))K

Olmot-K

202.952

203.453

203.942

20_.419

20_.886

205.343

205.790

206.227

206.656

207.075

208.089

209.056

209,981

210.866

211.716

212.534

213.322

214.083

214.819

215.533

216.228

216.904

217.565

218.211

218.845

219._68

220.082

220.687

221.285

221.877

H°CO

_oI

164.192

168.338

172._86

176.637

180.791

184.948

189.108

193.271

197.436

201.605

212.040

222._99

232.994

243.547

254.190

264.966

275.928

287.140

298.671

310.596

322,991

335.931

3_9.487

363.719

378,674

394.382

410.848

428.051

445.938

464._16

J_oI-K

203.708

204.191

204.662

205.124

205.575

206.017

206._49

206.873

207.288

207.695

208.680

209.620

210.520

211.383

212.212

213.010

213.781

214.525

215.246

215.946

216.628

217.292

217.940

218.576

219.199

219.813

220.417

221.01_

221.603

222.186

T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

I0oo0

10500

ii000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

175O0

18000

18500

19000

19500

20000

146 NASA/TP-3287/REV l
T

K

0

200

298.15

300

400

500

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

TABLE IX.4. - THERMODYNAMIC FUNCTIONS FROM COEFFIGIENTS FOR BCT,I)

C o HO(T).HO(O) S°(T) -(G°(T)-H°(O)}/T 14°(1") "G°('I')/T

J/moPi.K RJ/mol J/moI-K JlmoI-K kJ/mol J/moI-K

0.000 0.000 0.000 0.000 -1.214 INFINITE

6.002 0.357 2.418 0,634 -0.857 6.704

11.315 1.214 5.83_ 1.762 0.000 5.834

II._05 1.235 5.904 1.788 0.021 5.834

15.667 2.598 9.795 3.301 1.38_ 6.536

18.738 4.329 13.645 4.988 3.115 7.416

20.780 6.309 17.251 6.735 5.095 8.758

22.249 8.465 20.570 8._78 7.251 10.212

23.361 10.747 23.617 10.182 9.533 11.700

2_.245 13.129 26.421 11.833 11.915 13.182

2_.978 15.591 Z9.014 13.423 14.377 14.637

25.607 18,121 31.425 14,951 16.907 16.055

26.161 20.710 33.678 16.419 19.496 17.431

26.663 23.352 35.792 17.829 22.138 18.763

27.125 26,042 37.785 19.184 24.828 20.051

27,557 28.776 39.671 20.487 27.562 21.296

27,966 31.552 41.463 21.743 30.338 22.501

28,356 34.368 43.170 22.953 33.154 23.667

28.733 37.223 44.801 24.122 36.009 24.796

29.097 40.115 46.365 25.252 38.901 25.691

T

K

0

200

298.15

300

40O

500

600

700

800

900

1000

ii00

1200

1300

1400

1500

1600

1700

1800

1900

2000 29.452 43.042 47.866 26.345 41.828 26.952 2000

2100 29.799 46.005 _9.312 27.405 44.791 27.983 2100

2200 30.139 49.002 50.706 28.432 47.788 28.984 2200

23D0 30.475 52.032 52.053 29.430 50.818 29.958 2300

2350 30.641 53.560 52.710 29.919 52.346 30.435 2350

...... ..... ...... ...... 29 [9..... ...... ......

2400 31.750 105.356 74.744 30.8_5 10_.142 31.351 2_00

2500 31.750 108,531 76.040 32.627 107.317 33.113 2500

2600 31.750 111.706 77.285 34.321 110.492 34.788

2700 31.750 114.881 78.483 35.935 113.667 36.384

2800 31.750 118.056 79.638 37.475 116.842 37.909

2900 31.750 121.231 80.752 38.948 120,017 39.367

3000 31.750 124.406 81.828 _0.360 123.192 40.765

3100 31.750 127.581 82.870 41.714 126.367 42.106

3200 31.750 130.756 83.878 43.016 129.542 43.396

3300 31.750 133.931 84.855 44.269 132.717 44.637

3_00 31.750 137.106 85.802 45.477 135.892 45.834

3500 31.750 140.281 86.723 46.643 139.067 _6.989

3600 31.750 143.456 87.617 47,768 142.2_2 48.106

3700 31.750 146,631 88.487 48.857 145._17 49.185

3800 31.750 149.806 89.334 49,911 148.592 50.231

3900 31.750 152,981 90.159 50.933 151.767 51.244

_o0o 31.750 156.156 90,962 51.923 154,942 52.227

_I00 31.750 159.531 91.7_6 52.885 158.117 53.181

_200 31.750 162.506 92.511 53,820 161.292 54.109

4300 31.750 165.681 93.259 5_.728 16_.467 55.010

4400 31.750 168.856 93.988 55.612 167.642 55.888

4500 31.750 172.031 94.702 56.473 170.817 56.743

4600 31.750 175.206 95.400 57.312 173.992 57.576

_700 31.750 178,381 96.083 58.129 177.167 58.388

_800 31.750 181.556 96.751 58.927 180.342 59.180

_900 31.750 184.731 97.q06 59,706 183.517 59.953

5000 31.750 187.906 98.047 60.466 IB6.692 60.709

5100 31.750 191.081 98,676 61.209 189.867 61,447

5200 31.750 194.256 99.292 61.936 193.042 62.169

5300 31.750 197.431 99.897 62.646 196.217 62.875

5_00 31 750 200.606 100.491 63.341 199.392 63.566

5500 31.750 203.781 101.073 64.022 202.567 64.243

5600 31,750 206.956 101.645 64.689 205.742 64.906

5700 31.750 210.131 102.207 65.342 208.917 65.555

5800 31.750 213.306 102.760 65.983 212.092 66.192

5900 31.750 216.481 103.302 66.611 215.267 66.816

6000 31.750 219.656 i03,836 67,227 ZIB.4_Z 67.429

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

147

NASA/rP-3287/REV 1
T C °

K J/_-K

0 0.000

200 26.363

298.15 28.110

300 28.141

400 29.835

500 31.529

600 33.224

700 34,918

800 36.612

TABLE IX.@.- THERMODYNAMIC FUNCIION8 FROM OOEFRCIENT$ FOR Ba(or._

I'P(T)-H°(0) BD(T) _GO('I").HO_))/'T• He(F)

YJ/mol ,Jhnol_ JIm_-K _lm_

0.000 0.000 0.000 -6.907

4.238 51.517 30.327 -2.669

6.907 62.352 39.186 0.000

6.959 62.526 39.329 0.052

9.858 70.854 46.209 2.951

12.926 77.693 51.841 6.019

16.164 83.592 56.652 9.257

19.571 88.840 60.882 12.664

23.147 93.613 64.679 16.240

-G*(ryT

Jhnof-K

INFINITE

64.862

62.352

62.353

63.477

65.655

68,164

70.749

73.3]3

T

K

0

20O

298.15

3O0

40O

500

600

700

800

900 38.306 26.893 98.023 68.142 19.986 75.817 900

cr 1000 40.000 30.808 102.147 71.339 23.901 78.246 1000

...... ;;7;;; ...... ;E;;; ..... ;17111...... ; 7111...... ; 711 ...... ......

1100 40.000 42.658 113.809 75.029 35.751 81.308 1100

1200 40.000

1300 40.000

1400 40.000

1500 40.000

1600 40.000

1700 40.000

1800 40.000

1900 _0.000

2000 40.000

2100 40.000

2200 40.000

2300 40.000

2400 40.000

2500 40.000

2600 40.000

2700 40.000

2800 40.000

2900 40.000

3000 40.000

3100 40.000

3200 40.000

3300 40.000

3400 40.000

3500 40.000

3600 40.000

3700 40.000

3800 40.000

3900 40.000

4000 _0.000

4100 40.000

4200 40.000

4300 40.000

4400 40.000

4500 40.000

4600 40.000

4700 40.000

4800 40.000

4900 40.000

5000 40.000

5100 40.000

5200 40.000

5300 40.000

5400 _0.000

5500 40.000

5600 40.000

5700 40.000

5800 40.000

5900 40.000

6000 40.000

46.658 117.290 78.408 39.751

50.658 120.492 81.524 43.751

54.658 123.456 84.4]4 47.751

58.658 126.216 87.110 51.751

62.658 128.797 89.636 55.751

66.658 131.222 92.011 59.751

70.658 133.509 94.254 63.751

74.658 135.671 96.377 67.751

78.658 137.723 98,394 71.751

82.658 139.675 100.313 75.751

86.658 141.535 102.145 79.751

90.658 143,313 103.897 83.751

94.658 145.016 105.575 87.751

98.658 146.649 107.185 91.751

102.658 148.218 108.734 95.751

106,658 149.727 110.224 99.751

110,658 151.182 111.661 103.751

114.658 152.586 113.048 107.751

118.658 153.942 114.389 111.751

122.658 155.253 115.686 115.751

126.658 156.523 116.942 119.751

130.658 157.754 118.161 123.751

134.658 158.948 119.343 127.751

138.658 160.108 120.491 131.751

142.658 161.234 121.607 135.751

146.658 162.330 122,693 139.751

150.658 163.397 123.750 143.751

154.658 164.436 124.780 147.751

158.658 165.449 125.784 151.751

162.658 166,q37 126.764 155.751

166,658 ]67.400 127.720 159,751

170.658 168.342 128.654 163.751

174.658 169.261 129.566 167.751

178.658 170.160 150,458 171.751

182.658 17].039 131.331 ]75.751

186.658 171.900 132.185 179.751

190.658 172.742 133.021 183.751

194.658 173.566 133.840 187.751

198.658 174.375 134.643 191.751

202.658 175.167 135.430 195.751

206.658 175.943 136.201 199.751

210.658 176.705 136.958 203.751

214.658 177.453 137.701 207.751

218.658 178.187 138.431 211.751

222.658 178.908 139.147 215.751

226.658 179.616 139.851 219,751

230.658 180.311 140.543 223.751

234.658 180.995 141.223 227.751

238.658 181.667 141.891 231.751

84.164 1200

86.837 1300

89.348 1400

91.715 1500

93.953 1600

96.074 1700

98.091 1800

100.013 1900

101.847 2000

103.602 2100

105.285 2200

106.900 2300

108.453 2400

109.948 2500

111.390 2600

112.782 2700

114.128 2800

115.430 2900

116.691 3000

117.914 3100

119.101 3200

120.254 3300

121.374 3400

122.464 3500

123.526 3600

124.560 3700

125.568 3800

126,551 3900

127.511 4000

128.448 4100

129.36_ 4200

130.260 4300

131.136 _400

131.993 4500

132.832 _600

133.655 4700

134.460 4800

155.250 4900

136.024 5000

136.784 5100

137.530 5200

138.262 5300

138.981 5400

139.687 5500

140.381 5600

141.063 5700

141.734 5800

142.393 5900

143.042 6000

148 NASA/TP-3287/REV 1
TABLE IX.6. -THERMODYNAMIC FUNCTIONS FROM COEFRCIENTS FOR Be(a,13,_)

T C o Ho(.I.).HO_) SO(T) _GO(T).Ho(O)}R HO(T-) _O(T)/l" T

K Jkn_l-K IcJ/m_ _moI-K J/moI-K kJ/rnol J/motoK K

0 0.000 0.000 0.000 0.000 -1.942 INFINITE 0

200 10.003 0.620 4.Z12 1.110 -1.322 10.821 200

298.15 16.443 1.942 9.503 2.989 0.000 9.503 298.15

300 16,473 1.972 9.604 3.029 0.030 9.503 300

430 19.965 3.815 14.880 5.343 1,873 10.199 400

500 21.943 5.917 19.564 7.729 5.975 11,613 500

600 23.536 8.184 25.693 10,053 6,242 13.289 600

700 24.463 10.576 27.377 12,269 8,634 15.044 700

800 25,458 13.073 30.710 14.369 11.131 36.797 800

900 26.584 15.665 33.762 16.357 13.723 18.515 900

1000 27.274 18.348 36.588 18,240 16.406 20.182 I000

1100 28.147 21.119 39.229 20.050 19.177 21.795 1100

1200 29.015 23,977 41.715 21.734 22.035 23.353 1200

1300 29.885 26.922 44.072 23.363 24.980 24,856 1300

1400 30.762 29.955 46.319 24.925 28.013 26.310 1400

1500 31.649 33.075 48.671 26.421 31.133 27.716 1500

a 1543 32.035 34.444 49.371 27.048 32.502 28.307 1543

................ ;00 - 4; 1_4 53714 37-;4;...... ;;_;J ...... 3;307..... ;;;;-

9 1543 30. --" ...... "-_- _v'_o_ 39 802 28 635 1563

1563 30.000 q1./4_ _._uu _...... " .....

................ ;;0...... ;9-7;4 _9 3;;- - 2;-_;3...... ;;-;_ ...... _; ;3_...... _63 , 15_3 29 • 29350 1600 1600 29.480 50.835 59.908 28.136 48.893

1700 29.480 53.783 61.695 30.058 51.841 31.200 1700

1800 29.480 56.731 63.380 31.863 54.789 32.942 1800

1900 29,480 59.679 64.974 33.564 57.737 34,586 1900

2000 29.480 62.627 66.486 35.173 60.685 36.144 2000

2100 29.480 65.575 67.925 36.698 63.633 37.623 2100

2200 29.480 68.523 69,296 38.149 66.581 39.032 2200

2300 29.480 71.471 70.606 39.53Z 69.529 40.376 2300

2400 29.480 74.419 71.861 40.853 72.677 41,662 2400

2500 29.480 77.367 73.065 42.118 75.425 42.895 2500

2600 29.480 80.315 74.221 43.330 78.373 4_.077 2600

2700 29.480 83.263 75.333 44.695 81.321 45.214 2700

2800 29.480 86.211 76.405 _5.616 84.269 46,309 2800

2900 29.480 89.159 77.440 46.695 87.217 47,365 2900

5000 29.480 92.107 78.439 47.737 90.165 48,384 3000

3100 29._80 95.055 79,406 48.743 93.113 49.370 3100

3200 29.480 98.003 80.342 _9.716 96.061 50.323 3200

3300 29.480 100.951 81.249 50.658 99.009 51.246 3300

3400 29.480 103.899 82.129 51,571 101.957 52,142 3400

3500 29.480 106.847 82.984 52.456 104.905 53.011 3500

3600 29.480 109.795 83.814 53,316 107.853 53.855 3600

3700 29.480 112.745 84.622 54.151 110.801 54.676 3700

3800 29.480 115.691 85.408 54.963 113.749 55.474 3800

3900 29.480 118.639 86.174 55,754 116.697 56.252 3900

4000 29.480 121.587 86.920 56.523 i19.6q5 57.009 4000

_100 29.480 124.535 87.648 57.274 122.593 57,747 4100

4200 29.480 127.483 88.359 58.005 125.541 58.468 4200

4300 29.480 130.431 89.052 58.719 128.489 59.171 4300

4400 29.480 133.379 89.730 59.417 131.437 59.858 4400

4500 29.480 136.327 90.392 60.098 134.385 60.529 4500

4600 29.480 139.275 91.040 60.763 137.333 61.185 4600

4700 29.480 142.225 91.674 61,616 140.281 61.827 4700

4800 29.480 145.171 92.295 62,051 143.229 62._56 4800

4900 29.480 148.119 92.903 62.675 146.177 63.071 4900

5000 29.480 151.067 93.499 63.285 149.125 63.674 5000

5100 29.480 154.015 94,082 63.883 152.073 64.264 5100

5200 29.480 156.963 94.655 64,470 155.021 64.843 5200

5500 29.480 159.911 95.216 65.044 157.969 65.411 5300

5400 29._80 162.859 95.767 65.608 160.917 65.968 5400

5500 29.480 165.807 96.508 66.162 163.865 66.515 5500

5600 29.480 168.755 96.839 66.705 166.813 67.051 5600

5700 29.480 171,705 97.361 67.238 169.761 67.579 5700

5800 29.480 174.651 97.874 67.762 172.709 68.097 5800

5900 29.480 177.599 98.378 68.276 175.657 68.605 5900

6000 29.480 180.547 98,873 68,782 178.605 69.106 6000

149

NASA/TP-3287/REV 1
TABLE IX.7. - THERMODYNAMIC FUNCTIONS FROM COEFRCIENTS FOR B_r,

T C o HO(T)'H°(0) 800 ") _G°('l')*H°(O))_ _(T) _ °('l')K T

K J/m_l-K _ol _moI-K J/mol_ kJ/mol _moI-K K

0 0.000 0.000 0.000 0.000 -24.520 INFINITE 0

200 53.770 7.701 87,408 48.905 -16,819 171.505 200

cr 265.90 61.640 11.477 103.677 60.514 -13.043 152.729 265.90

t 265.90 77.739 22.052 143.447 60.514 --2.46; - -;52.72; ..... 2;5_;0

298.15 75.680 24.520 152.210 69.970 0000 1522 0 298115 300 75.623 24.660 152.678 70.478 0.140 152.211 300 40O

5O0

600

700

80O

900

1000

1100

1200

1500

1400

1500

1600

1700

1800

1900

2000

2100

2200

2500

240O

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

5700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

75.302

75.302

75.302

75.302

75.502

75.502

75.502

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.502

75.302

75.302

75.302

75.3O2

75.302

75.502

75.302

75.302

75.302

75.502

75.302

75.302

75.302

75.302

75.302

75.302

75.302

7fi.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75.302

75,302

75.302

75.302

75.302

75,302

75.302

75.302

75.302

75.302

75.302

75.302

32.193

39.723

47.253

54.783

62.314

69.844

77.374

84.904

92.434

99.965

107.495

115.025

122.555

130.085

137.615

145.146

152.676

160.206

167.736

175.266

182.797

190.327

197.857

205.387

212,917

220.448

227.978

255.508

243.038

250.568

258.099

265.629

273.159

280.689

288,219

295.749

303.280

310.810

318.340

525.870

333.4O0

340.931

348,461

355.991

363.521

371.051

378.582

386.112

393,642

401.172

408.702

416.233

423.763

_31,293

438.825

446.353

453.883

174.350

191.153

204,882

216,490

226,545

235.414

243.348

250.525

257.077

263.105

268.685

273.880

278.740

283.305

287.609

291.681

295.543

299.217

502.720

306.068

309,272

312,346

315.300

318.142

320.880

323.523

326.076

328.545

330.936

333.253

335.501

337.683

339.805

341.868

343.876

345.832

3_7.739

349.598

351.413

353,185

354.916

356.608

358.265

359.882

361.46&

363.020

364.542

366.033

367,495

368.930

370.337

371.719

373.076

374.408

375.718

377.005

378.271

93.868

111.707

126.127

138.228

148.653

157.810

165.974

173.340

180.049

186.209

191.903

197.197

202.143

206.785

211.156

215.?88

219.205

222.929

226.477

229.865

233,107

236.216

239.201

242.072

244.838

247.506

250.083

252.574

254.986

257.323

259.589

261.790

263.927

266.006

268.029

269.999

271.919

273,791

275.617

277.401

279.143

280.846

282.511

284.140

285,734

287.296

288.825

290.325

291.795

293.237

294.651

296.040

297.q04

298.743

300.059

301,352

302.624

7.673 155.168 400

15.203 160.747 500

22.733 166.993 600

30.263 175.256 700

37.794 179.303 800

45.324 185.054 900

52.854 190.494 I000

60.384 195.650 1100

67.914 200.482 1200

75.445 205.070 1300

82.975 209.417 1400

90.505 213.54_ 1500

98.035 217.468 1600

105.565 221.208 1700

113.095 224.779 1800

IZ0.626 228.194 1900

128.156 231.465 2000

135.686 23_.605 2100

143.216 237.622 2200

150.746 240.526 2300

158.277 243.32_ 2400

165.807 246.024 2500

173.537 248.632 2600

180.867 251.154 2700

188.397 253.596 2800

195.928 255.962 2900

203.458 258.256 3000

210.988 260.484 3100

218.518 262.649 3200

226.048 264.753 3300

233.579 266.801 3400

261.109 268,795 5500

248.639 270.738 3600

256.169 272.633 3700

263.699 274.482 3800

271,229 276.286 3900

278.760 278.049 4000

286.290 279.771 _100

293.820 281.455 4200

301.350 283.103 _500

308.880 284.716 4_00

316.411 286.294 4500

323.941 287.841 4600

331.471 289.357 4700

339.001 290.843 4800

346.531 292.300 4900

354,062 293.729 5000

361.592 295.133 5100

369.122 296.510 5200

376.652 297.863 5300

384.182 299.192 5400

391.713 300.498 5500

399.243 301.782 5600

406.773 303.045 5700

414.303 304.287 5800

421.833 305.508 5900

429.363 306.710 6000

150 NASA/TP-3287/REV 1
TABLE IX.8. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR C(gr)

T C o HoCI')'H°(O) So(T ) _Go(.r.).Ho(_}K ).loCi-) _O(T)ff T

p

K J/moI-K W/mot JtmoI-K J/moI-K kJImol Jlmo)-K K

0 0. 000 0. 000 0. 000 0. 000 -1. 053 INFINITE 0

200 5.007 0.388 3.07q 1.154 -0.665 6,q01 200

298.15 8.528 1.054 5.734 2.201 0.000 5.734 298.15

300 8.592 1.069 5.787 2.222 0.016 5.734 300

400 11.824 2,093 8.711 3.477 1.040 6.111 400

500 14.617 3.420 11.659 4.819 2.366 6.926 500

600 16.835 4.997 14.529 6.200 3.944 7.956 600

700 18.534 6.770 17.257 7.587 5.716 9.092 700

800 19.828 8.690 19.820 8.957 7.637 10.274 800

900 20.826 10.725 22.216 10.299 9.672 11.470 900

1000 21.612 12.849 24.452 11.604 11.795 12.657 1000

II00 22.243 15.042 26.543 12.868 13.989 13.826 1100

1200 22.762 17,294 28.501 14.090 16.240 14.968 1200

1500 23.198 19.592 30.341 15.270 18.539 16.080 1300

1600 23.572 21.931 32.074 16._09 20.878 17.161 1400

1500 23.897 24.305 33.712 17.508 23.251 18.211 1500

1600 24.185 26.709 35.263 18.570 25.656 19.228 1600

1700 24.443 29.141 36.737 19.596 28.087 20,215 1700

IB00 24.676 31.597 38.141 20.587 30.544 21.173 1800

1900 24.890 34.076 39.481 21.547 33.022 22.101 1900

2000 25.089 56.575 40.763 22.476 35.521 23.002 2000

2100 25.275 39.093 41.992 23.376 38.039 23.878 2100

2200 25.&49 41.629 43.172 24.249 40.576 24.728 2200

2300 25.615 44.182 44.306 25.097 43.129 25.555 2300

2&O0 25,773 46.752 45.400 25.920 45.698 26.359 2400

=SOD 25.924 49,337 46.455 26.720 48.283 27.142 2500

2600 26.070 51.937 _7.475 27.699 50.883 27.904 2600

2700 26.211 54.551 _8.461 28.257 53.497 28.668 2700

2800 Z6.347 57.179 49.417 28.996 56.125 29.372 2800

2900 26._80 59.820 50.344 29.716 58.766 30.080 2900

3000 26.609 62.674 51.244 30.619 61.421 30.770 3000

3100 26.736 65.142 52.118 31.I05 64.088 31.645 3100

3200 26.860 67.821 52.969 31.775 66.768 32.104 3200

3300 26.982 70.513 53.798 32.430 69.460 32.769 3300

3&00 27.102 73.218 54.605 33.070 72.164 33.380 3400

3500 27.220 75.934 55.392 33.697 76.880 33.998 3500

3600 27.337 78.662 56.161 34.310 77.6D8 34.603 3600

3730 17.453 81.401 56.911 34.911 80.348 35.196 5700

_r_ 27.568 84.151 57.645 55.500 83.099 35.777 3800

3otC 2T.681 86.915 58.362 36.077 85.861 36.347 3900

q3_C =7.794 09.689 59.065 36.6_3 88.635 36.906 6000

_lC3 =7.906 92.476 59.752 37.198 91.420 37.655 4100

4:'?C _8 017 95.270 60.626 37.743 94.216 37.996 4200

_c 28.128 90.077 61.087 38.278 97.023 38.525 4300

,,C _ _ 238 100.895 61.735 38.804 99.862 39.043 4400

_5_0 23 547 103.724 62.370 39.321 102.671 39.555 4500

_r" 2_ _56 106.565 62.995 39.828 105.511 60.057 4600

_,_- _ _55 109.416 63.608 40.328 108.362 60.552 6700

._'c .t _Tq 112.278 64.210 40.819 111.226 41.039 4800

_rr iE "82 115.150 66.803 _1.303 114.097 AI.518 4900

5OCC 2_ _90 I18.034 65.585 61.778 116.980 41.989 5000

NASA/TP-3287/REV 1

151
TABLE IX.0. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Ca(a.,_,,I)

T C o H°("I')'H°(0) S°(T) _G°(T)'H°(0)}_ I'P('I') _°(T)K T

K J_-K IM/mol _mol_ J/moI-K kJ/mol J_ol-K K

0 0,000 0.000 0,000 0.000 -5.785 INFINITE 0

200 24_420 3.316 32.519 15.938 -2.467 44.852 200

298.15 25.750 5.783 42.536 23.140 0,000 .62.536 298.15

300 25.774 5.831 42.696 23.260 0.048 42.537 300

400 27.108 8.472 50.287 29,106 2.689 43,563 400

500 28.736 11.263 56.507 33,981 5.480 45.547 500

600 30,510 14.224 61.901 38.194 8.441 47.832 600

700 32.402 17.369 66.745 41.932 11.586 50.193 700

716 32.708 17.890 67.481 42.495 12.107 50.571 716

...... ...... ...... ;;7;;; ...... J7;;; ...... ...... ....... ;;j--

800 30.155 21.341 72.109 45.432 15.558 52.661 800

900 31.009 24.394 75.704 48.599 18.611 55.025 900

I000 32.532 27.565 79.044 51.478 21.782 57.261 I000

1100 34.724 30.923 82.242 54.130 25.140 59.388 1100

# 1115 35.110 31.446 82.715 54.512 25.663 59.698 1115

............................................................................................

t 1115 38.000 39.986 90.374 54.512 34.203 59.698 1115

1200 38.000 43.216 93.166 57.152 37.433 61.971 1200

1300 38.000 47.016 96.207 60.041 41.233 64,489 1300

1400 38.000 50.816 99.023 62.726 45.033 66.857 1400

1500 38.000 54.616 101.645 65.234 48.833 69.089 1500

1600 38.000 58.416 104.097 67.587 52.633 71.202 1600

]700 38.000 62.216 106.401 69.803 56.433 73.205 1700

1800 38.000 66.016 108.573 71.898 60.233 75.110 1800

1900 38.000 69.816 110.628 73.882 64.033 76.926 1900

2000 38.000 73.616 112.577 75,769 67.833 78.660 2000

2100 38.000 77.q16 114.431 77.566 71.633 80.320 2100

2200 38.000 81.216 116.199 79.282 75.433 81.911 2200

2300 38,000 85.016 117.888 , 80,924 79.233 83.439 2300

2400 38.000 88.816 119.505 82.498 83.033 84.908 2400

2500 38.000 92.616 121.056 84.010 86.833 86,323 2500

2600 38.000 96.416 122.547 85.464 90.633 87.688 2600

2700 38.000 100.216 123.981 86.864 94,433 89.006 2700

2800 38.000 104.016 125.363 88.214 98.233 90.280 2800

2900 38.000 107.816 126.696 89.518 102.033 91.512 2900

3000 38.000 111.616 127.985 90.779 105.833 92.707 3000

3100 38.000 115.416 129.231 92.000 109.633 93,865 3100

3200 38.000 119.216 130.437 93.182 113.433 94.989 3200

3300 38,000 123,016 131.606 94.329 117.233 96.081 3300

3400 38.000 126.816 132.741 95.442 121.033 97.143 3_00

3500 38,000 130.616 133.842 96.523 124.833 98.176 3500

3600 38.000 134.416 134.913 97.575 128.633 99.181 3600

3700 38.000 138.216 135.954 98.598 132.433 100.161 3700

3800 38.000 142.016 136.967 99.595 136.233 101.116 3800

3900 38.000 145,816 137.954 100.566 140.033 102.048 3900

4000 38.000 149.616 138.917 101.512 i_3.833 102.958 qO00

4100 38.000 153.416 139.855 102.636 147.633 103.847 4100

4200 38.000 157.216 140.771 103.338 151.433 104.715 4200

4300 38.000 161.016 141.665 104.219 155.233 105.564 4300

4400 38.000 164.816 142.538 105.080 159.033 106,394 4400

4500 38.000 168.616 143.392 105.922 162.833 107.207 4500

4600 38.000 172.416 144.227 106.746 166.633 108.003 4600

4700 38.000 176,216 145.045 107.552 170.433 108.782 4700

_800 38.000 380.016 145.845 108.3_1 174.233 109.546 4800

4900 38.000 183,816 146.628 109.115 178.033 110.295 4900

5000 38.000 187.616 147.396 109.873 181.833 111.029 5000

5100 38.000 191.416 148.148 110.616 185.633 111.750 5100

5200 38.000 195.216 148.886 111.345 189.433 112.457 5200

5300 38.000 199.016 149.610 112.060 193,233 113.151 5300

5400 38.000 202.816 150.320 112.762 197.033 113.833 5400

5500 38.000 206.616 151.018 113.451 200.833 114.503 5500

5600 38.000 210.416 151.702 114.128 20_.633 115.161 5600

5700 38.000 214.216 152.375 114.793 208.433 115.808 5700

5800 38.000 218.016 153.036 115.447 212.2_3 116.444 5800

5900 38.000 221.816 153,686 116.090 216.033 117.070 5900

6000 38.000 225.616 154,324 116.721 219.833 117.685 6000

152 NASA/TP-3287/REV l
T C °

K J/moPi'K

0

200

298.15

300

4O0

TABLE IX.IO. -THERMODYNAMIC FUNCTIONS FROM GOEFRCIENI"S FOR Cd(¢r,l)

H°(T)'HO(0) SOm .(GO(T).HO(0))/T 14o(1.) .GO(TyT T

kJ/mol JJmoI-K J/moi-K W.Pmol JlmoI-K K

0.000 0,000 0.000 0,000 -6.247 INFINITE 0

24.909 3.738 41.608 22.917 -2. 509 54. 152 200

26. 020 6.247 51.800 30.847 0,000 51.800 298.15

26.035 6.295 51,961 30.977 0.048 51.800 300

27.085 8.948 59.584 37.215 2.701 52.833 400

500 28.336 11.719 65.763 42.325 5.472 54.819 500

cr 594.26 29.600 14.446 70.757 46.448 8.199 56.960 594,26

............................ .... ...... ...... .......

594.26 29.900 20 5 _1"? _ 46 779 14.431 57.191 600

600 Z_._uu 20.678 .... 4_ - 60.96_ 700

700 29.900 23.668 85.852 52.040 17.421

800 29.900 26.658 89.844 56.522 20.411 64.530 800

900 29.900 29.648 93.366 60.424 23.401 67.565 900

1000 29.900 32.638 96.516 63.878 26.391 70.125 1000

Ii00 29.900 35.628 99.366 66.977 29.381 72.656 1100

1200 29.900 58.61_ 101.968 69.786 32.371 7_.992 1200

1300 29.900 41.608 104,361 72.355 35.361 77.160 1300

1400 29.900 44.598 106.577 74.721 38.351 79.183 1400

1500 29.900 47.588 108.640 76.914 41.341 81.079 1500

1600 29.900 50.578 110.569 78.958 _4.331 82.862 1600

1700 29.900 53.568 112.582 80.871 47.321 84.546 1700

1800 29.900 56.558 114.091 82.670 50.311 86.140 1800

1900 29.900 59.548 115.708 84.367 53.301 87.654 1900

2000 29.900 62.538 117.2_1 85.972 56.291 89.096 2000

2100 29.960 65.528 118.700 87._96 59.281 90.471 2100

2200 29.900 68.518 120.091 88.946 62.271 91.786 2200

2300 29.900 71.508 121.420 90.330 65.261 93.0#6 2300

2_00 29.900 7_.498 122.693 91.652 68.251 94.255 2400

2500 29.900 77.488 123,915 92.918 71.241 95.417 2500

2600 29.900 80.478 125,086 94.133 74.231 96.536 2600

2700 29.900 83._68 126.214 95.300 77.221 97.614 2700

2800 29,900 86.458 127.502 96,_24 80,211 98.655 2800

2900 29,900 89._48 128,551 97.507 83.201 99.661 2900

3000 29.900 92.435 129.365 96.552 86.191 100.634 3000

3100 29.900 95.428 130.5_5 99.562 89.181 101,577 3100

3200 29.900 98.418 131.294 100.539 92.171 102.491 3200

3300 29.900 101.408 132.21_ 101.485 95.161 103.378 3300

3400 29.900 104.398 133.107 102.402 98,151 104,239 3400

3500 29.900 107.388 133.97_ 103.291 101.141 105.076 3500

3600 29.900 110.378 134.816 104.156 10_.131 105.891 3600

5700 29.900 113.368 135.635 104.995 107.121 106.684 3700

3800 29.900 I16,358 136._33 105.812 110.111 107.456 3800

3900 29.900 119.348 137.209 106.607 113.101 108.209 3900

_000 29.900 122.338 137.966 107.382 116.091 108.944 4000

4100 29,900 125,328 138.705 108.137 119.081 109,661 4100

4200 29.900 128,318 139.425 108.873 122.071 110.361 4200

4300 29.900 131,308 I_0.129 109.592 125.061 111.045 4300

4400 29.900 134,298 140.816 110.294 128.051 111.714 4400

_500 29.900 137.288 141.488 110.980 131,041 112.368 4500

4600 29,900 140.278 142.145 111.650 134.031 113.008 4600

4700 29.900 1_3.268 142.788 112.306 137.021 113.635 4700

_800 29,900 146.258 143.418 112.947 140.011 114.249 4800

4900 29,900 149.248 144.034 113.575 143.001 114.850 4900

5000 29.900 152.238 144,638 114.191 i_5.991 115.440 5000

5140 29,900 3.55.228 145.230 114.794 148.981 116.018 5100

5200 29,900 158.218 145.811 115.384 151.971 116.586 5200

5300 29.900 161.208 146.381 115.964 154.961 117.143 5300

5400 29.900 164.198 146.939 116.532 157.951 117.689 5400

5500 29,900 167,188 147,488 117.090 160.941 118.226 5500

5600 29.900 170.178 148.027 117.638 163.931 118.755 5600

5700 29.900 175.168 148.556 118.176 166.921 119.272 5700

5800 29.900 176.158 149.076 118.704 169.911 119.7_1 5800

5900 29.900 179.148 149,587 119.223 172.901 120.282 5900

6000 29.900 182.138 150.090 119.753 175.891 120.775 6000

NASA/TP-3287/REV l

153
TABLE IX.11. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Q2

T C ° H%I'}oHO(o) SO(T) _Go(.r).Ho(O)}K HO(T)

K _m_l-K kJ/mol _moI-K J/moI-K kJ/moJ

0 0.000 0.000 0.000 0.000 -9.181

200 31.720 5.950 209.967 180.217 -3.231

298.15 33.949 9.181 223.082 192.288 0.000

300 33.981 9.244 223.292 192.479 0,063

400 35.297 12.714 233.265 201,480 3.533

500 36.065 16.285 241.231 208.661 7.104

600 36.547 19.918 247.852 214.657 10.736

700 36.874 23.590 253.512 219.813 14.400

800 37.112 27.289 258.452 224.341 18.108

900 37.294 31.010 262.834 228.379 21.829

1000 37.443 34,747 266.772 232.025 25.566

1100 37,504 38.493 270.342 235.348 29,312

1200 37.648 _2.251 273.611 238.402 33,069

1300 37.796 46.023 276.631 241.228 36.842

1400 37.919 49.809 279.436 243.859 40.628

1500 36.017 53.606 282.056 246.319 44._25

1600 38.095 57.412 284.512 248.630 48.230

1700 38.166 61.225 286.824 250.809 52.04_

1800 38.239 65.045 289.007 252.871 55.864

1900 38.325 68.873 291.077 254.828 59.692

2000 38,_31 72.710 293.045 256.690 63.529

2100 38.561 76.560 294.923 258._66 67.379

2200 38.721 80,424 296.721 260.165 71.243

2300 38.911 8_.305 298.446 261.792 75.12_

2400 39.131 88.207 300.107 263.354 79.026

2500 39.380 92,132 301.709 264.856 82.951

2600 39.656 96.084 303.259 266.304 86.903

2700 39.957 100.064 304.761 267.700 90.883

2800 40.277 104.076 306.220 269.050 94.895

2900 40.614 108.120 307.639 270.356 98,939

3000 40.963 112.199 309.022 271,622 103.018

3100 41.318 116.313 310:1371 272.850 107.152

3200 41.675 120._63 311.688 274.044 111.282

_00 42.030 124.648 312.976 275.204 115.467

3400 42,377 128.868 314.236 276.334 119.687

3500 42.712 133.123 315._69 277.434 123.942

3600 _3.030 137.410 316.677 278.508 128.229

3700 43.328 141.728 317.860 279.555 132.547

3800 43.601 146.075 319.019 280.578 136.89_

3900 43.846 150.4_8 320.155 281.579 1_1.267

4000 44.059 154.8_3 321.268 282.557 145.662

4100 _4.238 159.258 322.358 283.515 150.077

4200 44.381 163.690 323.426 284.452 15_.5u8

4300 44.486 168.133 324.472 285.371 158.952

_400 44.551 172.585 325.495 286.271 163.404

_500 4_.575 177,0_2 326.497 287.154 167.861

4600 44.558 181.499 327.476 288.020 172.318

4700 44.501 185.952 328.434 288.870 176.771

qSO0 44.403 190.398 329.370 289.704 181.217

_q00 44.266 194.832 330.284 290.523 185.650

5000 44.092 199.250 331.177 291.327 190.069

5100 _3.884 203.6_9 332.048 292.117 194.468

5200 _3.643 208.026 332.898 292.893 198.844

5300 43.374 212.377 333.727 293.655 203.196

5400 43.081 216.700 334,535 29_.405 Z07.518

5500 42.769 220.992 335.322 295.142 211.811

5600 42.4_2 225.253 336.090 295.866 216.072

5700 42.107 229.480 336,838 296.579 220.299

5800 41.770 233.674 337.568 297.279 224._93

5900 41.438 237.834 338.279 297.968 228.653

6000 41.120 241.962 338.973 298.646 232.781

_*O')n

_moI-K

INFINITE

226.125

223.082

223.082

224.433

227.023

229.958

232,929

255.817

238.580

241.206

243.695

246.053

248.291

250.416

252._39

254.368

256.210

257.972

259.660

261.281

262.838

264.338

265.784

267.179

268.529

269,835

271.101

272.329

273.522

274.683

275.812

276.913

277.986

279.034

280.057

281.058

282.037

282.995

283.933

284.852

285.754

286.638

287.506

288.358

289.194

290.016

290.823

291.616

292.396

293.163

293.917

294.658

295.388

296.105

296.811

297.506

298.189

298.862

299.524

300.176

T

K

0

200

298.15

300

400

500

6O0

700

800

900

I000

1100

1200

1300

1_00

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

_000

_100

_200

4300

4400

4500

4600

4700

_800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

154 NASA/TP-3287/REV l
TABLE IX.12. - THERMODYNAMIC FUNCTION8 FROM COEFRCIENTS FOR Co(¢%_,_)

T G o HO(T)'H°(0) 8ot.,T) .{GO(T).Ho(O))/T HoO-.) .GO(T)/T T

K JImopl'K kJ/mol J/moI-K JlmoI-K kJ/tool Jlmol-K K

0 0.000 0.000 0.000 0.000 -(4.771 INFIffITE 0

200 22.225 2.6,31 20.579 8.6,2'% -2.3(-,0 32.279 200

250 23.985 3. 596 25. 771 11,387 -1.175 30.6,71 250

298.15 26,.802 6,,771 30.067 14.065 0,000 30.067 298.15

300 2'%,833 4.817 30.221 14.16'% 0.046 30.067 300

350 25.676 6.080 3'%. 111 16.741 1.309 30.373 350

600 26.532 7 , 385 37.596 19.13(4 2,61(4 31.062 (400

450 27.388 8.733 40.770 21.36'% 3.962 31.967 6,50

500 28.200 10 • 123 43. 699 23.(453 5. 352 32.995 500

,9(43 11 552 '%6 (422 25 419 6 781 3(4.093 550 550 28 ' " " 35 228 600

7 '%8 971 27 276 8 246 " 7

600 29.665 13.01 _.'.=. zn'71_ 11 283 37.502 700

700 31.0'%5 )6.054 _._ _._;_ _V'286 37 5Sq 700.10

a 700 10 31.0'%7 10.0_/ _.o_, ......... -L ................

---5....... 5;;;.....;; - ...... ......;;-;3;......;7534 70o.lo 700 10 _ ..... "A_A 58'499 33'929 14_885 39.893 BOO

_.._o ±_'==T 7.'_ _'_80 18.230 '%2.181 9U0

34.552 Z3.UU* o_._- .... 21 803 '%(4.396 1000

800

9O0

1000 36.9(48 26,57(4 66.199 39.625

II00 39.7'%8 30.40(4 69.847 (42,207 25.633 '%6.56,5 Ii00

1200 (43.(419 36,.553 73.(455 4'%.661 29.782 6,8.637 1200

1300 48.501 39.135 77.120 '%7.016 3'%.36(4 50.686 1300

139_ 55.023 43.986 80,720 49.166 39.215 52.589 139'%

1_00 6,4.225 44.283 80.933 49.302 39.512 52,710 1'%00

1500 39.81'% (48,(456 83.813 51,509 6,3.685 5(4.690 1500

157 52 337 86 319 53 608 47 566 56.590 1600 1600 38. --" ..... '-_- =¢'&nl 51"362 58 407 1700 889 _6 13_ oo o_u _ .... " 1700 37. • • - 9'%0 59 598 1768

B 1768 37.949 58.711 90.107 56.900 ..... 535 ........... _ ................

/

.............. 1768 (40 ......

....

...... ...... 70133 59.598 60 310 1768 1800

1800 6,0.501 76.200 99.992 57.659 71.(429 •

1900 (40.501 80.250 102.182 59.9'%5 75._79 62.(456

2000 6,0.501 8'%.300 104.260 62.110 79.529 6(4.(495

2100 40.501 88.350 106.236 6'%.16(4 83.579 66.'%36

2200 '%0.501 92.'%00 108.120 66.120 87.629 68.288

2300 40.501 96.(450 109.920 67.985 91.679 70.060

2_00 40.501 100.500 111.6(46, 69.769 95.729 71.757

2500 40.501 10(4.550 113.297 71.(477 99.779 73,385

2600 40.501 108.600 11'%.886 73.116 103.829 7_.951

2700 6,0.501 112.651 116.6,_(4 74.692 107.880 76.'%59

2800 40.501 116.701 117.887 76.208 111.930 77.912

2900 (40.501 120.751 119.308 77.670 115.980 79.315

3000 40.501 124.801 120.681 79.081 120.030 80.671

3100 '%0.501 128.851 122.009 80.(44_ 124.080 81.986,

3200 _0.501 132.901 123.295 81.764 128.130 83.255

3300 6,0.501 136.951 12(4.5'%1 83.06,1 132.180 8'%.487

3_00 6,0.501 141.001 125.751 84.280 136.230 85.683

3500 '%0.501 16,5.051 126,925 85.'%81 16,0.280 86.846,

3600 40.501 1'%9.101 128.065 86.6(48 1'%_.330 87.974

3700 40.501 153.152 129.175 87.783 148.381 89.072

3800 6,0.501 157.202 130.255 88.886 152.431 90.142

3900 6,0.501 161.252 131.307 89.961 156.6,81 91.186,

6,000 40.501 165.302 132.333 91.007 160.531 92.200

4100 6,0.501 169.352 133.333 92.027 16(4.581 93.191

'%200 (40.501 173.'%02 13'%.309 93.023 168.631 96,.158

6,300 40.501 177.6,52 135.262 93.996, 172.681 95.103

'%(400 (40.501 181.502 136.193 9'%.96,2 176,731 96.027

_500 6,0.501 185.552 137.103 95.869 180.781 96.929

6,600 '%0.501 189.602 137.993 96.775 18'%.831 97.812

(4700 (40.501 193.653 138.864 97.662 188.882 98.677

(4800 40.501 197.703 139.717 98.529 192.932 99.523

4900 '%0.501 201,753 1¢0.552 99.378 196.982 100.352

5000 (40.501 205.803 141.370 100.210 201.032 101.164

5100 6,0.501 209.853 142.172 101.025 205.082 101.960

5200 (40.501 213.903 1(42.959 101.82(4 209.132 102.7(41

5300 6,0.501 217.953 1'%3.730 102.607 213.182 103.507

5'%00 40.501 222.003 I'%_,487 103.376 217.232 104.259

5500 40.501 226.053 1'%5.230 10'%.130 221.282 10_.997

5600 6,0.501 230.103 16,5.960 10(4.870 225.332 105.722

5700 '%0.501 234.154 146.677 105.597 229,383 i06.(43'%

5800 '%0.501 238.206, I(47,381 106.312 233.6,33 107.136,

5900 ¢0.501 2_2.25'% 148.074 107.016, 237.6,83 107.822

6000 40.501 2(46.30(4 1(48.75(4 107.704 241.533 108.'%99

1900

2000

2100

2200

2300

26,00

2500

2600

2700

2800

2900

3000

3100

3200

3300

3(400

3500

3600

3700

3800

3900

4000

'%100

4200

6,300

_400

¢500

46O0

6,700

6,800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

155

NASA/TP-3287/REV 1
TNBLE IX.13. • THERMODYNAMIC FUN_(_8 FROM COEFFICIENT8 FOR Cr(cr, l_

T 0 • H°(T')-H°(O) S°t'T') _G°(T)-H°(_}I'I - I'I°('I') _°(T)IT T

K J/m_l-K kJ/m_ J/mol-K J/moI-K _/m_ J/mo_K K

0 0.000 0.000 0.000 0.000 -6.057 ZNFZNZTE 0

200 19.860 1,894 14_868 5,397 -2.163 25.602 200

298.15 23.434 4.057 23.618 10.011 0.000 23.618 298.15

300 23.467 4.100 23.763 10.095 0.0¢3 23.618 300

400 25.229 6.538 30.764 14.419 2.481 24.561 400

500 26.637 9.136 36.552 18.283 5.077 26.397 500

600 27.710 11.854 41.507 21.750 7.797 28.512 600

700 28.574 16.669 45.845 26.889 10.612 30.685 700

800 29,639 17.569 49.716 27.755 13.512 32.816 800

900 30.498 20.564 53.242 30.393 16.507 34.901 900

1000 31.862 23.679 56,523 32.844 19.622 36.901 1000

1100 33.465 26.942 59.632 35.139 22.805 38.827 1100

1200 35.216 30.374 62.617 37.305 26.317 40.686 1200

1300 37.119 33.990 65.510 39.366 29.933 42.485 1300

1400 39.121 37.801 68.334 41.333 33.744 44.231 1400

1500 41.195 61.817 71.103 43.226 37.760 45.930 1500

1600 43.326 46.042 73.830 45.053 41.985 47.589 1600

1700 45.500 50.483 76.521 46,825 46.426 49.212 1700

1800 47.710 55.143 79.184 68.549 51.086 50.805 1800

1900 49.947 60.026 81.826 50.231 55.969 52.366 1900

2000 52.207 65.134 84.443 51.876 ' 61.077 53.905 2000

2100 54.486 70.468 87.045 53.489 66.411 55.421 2100

cr2130 55.173 72.113 87.823 55.967 68.056 55.872 2150

I 2130 39.330 92.615 97.448 53.967 88.558 55.872 2130

2200 39.350 95.368 98.720 55.371 91.311 57.215 2200

2300 39,330 99.301 100.469 57.294 95.244 59.058 2300

2400 39.330 103.234 102.142 59.128 99.177 60.819 2400

2500 39.330 107,167 103.768 60.881 103.110 62.504 2500

2600 39.330 111.100 105,290 62,560 107.043 64.120 2600

2700 39.330 115.053 106.775 64.170 110.976 65,673 2700

2800 39.330 118.966 108.205 65.717 114.909 67,166 2800

2900 39.330 122.899 109.585 67.206 118.842 68,605 2900

3000 39.530 126.832 110.919 68.641 122.775 69.994 3000

3100 39.330 130.765 112.208 70.026 126,708 71,335 3100

3200 39.330 134.698 113.657 71.364 130.641 72.632 3200

3300 39.330 138.631 114.667 72.658 136.574 73.887 3300

3400 39.530 142.564 115.841 73.911 138.507 75.104 3400

3500 39.330 146.497 116.981 75,125 162,440 76.284 3500

3600 59.350 150.430 118.089 76.303 146,373 77.430 3600

3700 39.330 156.363 119.167 77.647 150,306 78.544 3700

3800 39.330 158,296 120,216 78.559 154.239 79.627 3800

3900 39.330 162,229 121.237 79.660 158.172 80,680 3900

4000 39.330 166.162 .122.233 80.693 162.105 81.707 4000

6100 39.330 170.095 123.204 81.718 166.038 82.707 4100

4200 39.330 174.028 124.152 82.717 169,971 83.683 4200

4300 39.330 177.961 125.078 83.691 173.904 84.635 4300

6400 39.530 181,894 125.982 84.642 177,037 85.564 4600

4500 39.330 185.827 126.866 85.571 181.770 86.472 4500

4600 39.350 189.760 127.750 86.678 185.703 87.360 4600

4700 39.330 193.693 128.576 87.365 189.636 88.228 4700

¢800 39,330 197.626 129.404 88,232 193.569 89.077 6800

4900 39.330 201.559 130.215 89.080 197.502 89.908 4900

5000 39.330 205.492 131.009 89.911 201._35 90.722 5000

5100 39.330 209.425 131,788 90.72_ 205,368 91.520 5100

5200 39.330 213.558 132.552 91,522 209.301 92.302 5200

5300 39.530 217.291 133.501 92.303 213.234 93.068 5300

5400 39,330 221.224 134,036 93,069 217,167 93,820 5400

5500 39.330 225.157 136.758 93.820 221.100 94,558 5500

5600 39,330 229.090 135.467 94,558 225.033 95.282 5600

5700 39.330 233.023 136.163 95.281 228.966 95.993 5700

5800 39,330 236.956 136.847 95.992 232.899 96.692 5800

5900 39.330 260.889 137.519 96.690 236.832 97.378 5900

6000 39.330 244.822 138.180 97.376 2_0.765 98.053 6000

156 NASA/TP-3287/REV 1
TABLE IX.14. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENT8 FOR C_A(er, I)

T C • flO('r)-H°(0) SO(T) .{Go(rpHo(O))/T Ho(-r) .GO(T)/T T

K J_I-K kJ/mo_ J/moI-K J/moI-K kJ/rnol J/mot-K K

0 0.000 0.000 0.000 0.000 -7.711 INFINITE 0

100 25.822 2.166 55.052 33. 607 -5. 567 110.717 100

200 27.784 4.826 73.569 69.619 -2.885 87.974 200

298 15 32.210 7.711 85.230 59.367 0,000 85.230 298.15

' 7.771 85.630 59.527 0.060 85.231 300

_ _9 _'_ 7 822 85 601 59.666 __0_11 85_232 _

cr.......................... ou_.a • ' - ........................... 921551 - 59.664 2.207 ...... 85.232 ....... 301.59

$ 301.59 32.635 600 400 32.02_ 15,108 101.70B 68.938 5.397 88.216

500 30.955 16.257 8.566 91.648 500 108.740 '76.226

600 30.001 19.303 116.296 82.126 11.592 94.976 600

700 29.361 22.268 118.860 87.056 14.557 98.072 700

800 29.115 25,188 122,768 91,282 17.677 100.921 800

900 29.304 28.106 126.203 94.975 20.395 103.563 900

1000 29.9_8 31.064 129.320 98.256 23.353 105.967 1000

1100 31.059 36.111 132.223 101.213 26.600 108.223 1100

1200 32.663 37.292 136.990 103.913 29.581 110.339 1200

1300 34.707 60.655 137.681 106.408 32.94_ 112.359 1300

1600 37,251 44.269 1_0.343 108,737 36.538 114.244 1600

1500 60,278 48,122 163,016 110,933 40,611 116.073 1500

1600 Q3.790 52.321 145.725 113.022 6_.610 117.8_1 1600

1700 67,788 56.896 168.695 115,027 69.185 119.563 1700

1800 52.273 61.895 151.351 116.965 56.184 121.269 1800

1900 57.244 67.367 15_.300 118,852 59.656 122.911 1900

2000 62.702 73.360 157.381 120,701 65.6_9 126.557 2000

157

NASA/TP-3287/REV 1
TABLE #X.16. - THEFIMODYNAM_

T C ° HO(T).H°(_

K J,_ _J/m_

0 0.000 0.000

200 22.627 2.679

298.15 24.440 5.004

300 24.461 5.049

400 25.344 7.543

500 25,965 10.110

600 26.475 12.732

700 26.952 15.403

800 27.448 18,123

900 28.015 20.895

1000 28.700 23.730

1100 29.552 26.641

1200 30.617 29.647

FUNCTIONS FROM COEFFICIENTS FOIl Cu(cr.4)

S*(T) -IGP(T)-_(O)HT H°(r] -G*(T)rr

d/moI-K J/moI-K kJ/mol J/moI-K

0.000 0.000 -5.004 INFINITE

23.717 10.320 -2.525 35.540

33,150 16.367 0.000 33.150

33.301 16.470 0.045 33.150

40.469 21.612 2.539 34.122

46.194 25.975 5.106 35.985

50.974 29.754 7.728 38.094

55.091 33.086 10.399 40.234

58.722 36.068 13.119 42.325

61.986 38.769 15.891 44.329

64.972 41.242 18.726 46.246

67.746 43.527 21,637 48.076

70,361 45.655 26.645 49.825

T

K

0

200

298

300

400

500

600

700

800

900

1000

I100

1200

.15

1300 31.940 32.773 72,862 47.652 27.769 51.502 1300

cr 1358 32.844 34.651 74.276 48.759 29.647 52.444 1558

...... ...... ...... ...... ...... ...... ......

1400 32.800 49.169 84.951 49.830 44.165 53.405 1400

1500 32.800 52.449 87.214 52.248 47.445 55.584 1500

1600 52.800 55.729 89.331 54.500 50.725 57.628 1600

1700 32.800 59.009 91.319 56.608 54.005 59.552 1700

1800 32.800 62.289 93.194 58.589 57.285 61.369 1800

1900 32.800 65.569 94.967 60.457 60.565 63.091 1900

2000 32.800 68,849 96.650 62,225 65.845 64.727 2000

2100 32.800 72.129 98.250 63.903 67.125 66.286 2100

2200 32.800 75._09 99.776 65.499 70.405 67.774 2200

2500 32.800 78.689 101.234 67.021 73.685 69.197 2500

2400 32.800 81,969 102.630 68.476 76.965 70.561 2400

2500 32.800 85.249 103.969 69.869 80.245 71.871 2500

2600 32.800 88.529 105.255 71.206 83.525 73.150 2600

2700 32.800 91.809 106.493 72._90 86.805 74.343 2700

2800 52.800 95.089 107.686 73,726 90.085 75.515 2800

2900 32.800 98.369 108.837 74.917 93.565 76.642 2900

3000 32.800 101.649 109.949 76.066 96.645 77.734 3000

3100 32.800 104.929 111.024 77.176 99.925 78.791 3100

3200 32.800 108.209 112.066 78.251 105.205 79.814 5200

3300 32.800 111.489 113.075 79.291 106.485 80.807 3300

3400 32.800 114.769 114.054 80.299 109.765 81.771 3400

3500 32.800 118.049 115.005 81.277 113.045 82.707 3500

3600 32.800 121.329 115.929 62.227 116.325 85.617 3600

3700 32.800 124.609 116.828 83.150 119.605 84.502 3700

3800 32.800 127.889 117.703 84.048 122.885 85.364 3800

3900 3_.800 131.169 118.555 84.922 126.165 86.205 5900

4000 52.800 134.449 119.585 85.773 129.445 87.024 4000

_100 32.800 137.729 120.195 86.602 132.725 87.825 4100

4200 52.800 141.009 120.985 87.412 136.005 88.603 _200

4300 31.800 144.289 121.757 88.202 139.285 89.365 4300

_oo 31.8oo 147.569 122.511 88.973 142.565 90.110 4400

4500 52.a00 150.849 123.248 89.726 145.845 90.838 4500

4600 32.600 154.129 125.969 90.463 149.125 91.551 4600

_700 32.100 157.409 124.675 91.183 152.405 92.248 4700

4800 32.800 160.689 125.565 91.888 155.685 92.951 4800

_9_0 $Z 800 163.969 126.041 92.578 158.965 93.600 4900

5000 52 800 167.249 126.704 93.254 162.245 94.255 5000

5190 32.800 170.529 127.354 93.917 165.525 94.898 5100

5200 32.800 173.809 127.991 94.566 168.805 95.528 5200

5300 32.800 177.009 128.615 95.202 172.085 96.146 5300

5400 32.000 180,369 129.228 95.827 175.365 96.753 5400

5500 32.800 183.649 129.830 96.440 178.645 97.349 5500

5600 32.800 186.929 150.421 97.041 181.925 97.955 5600

5700 32.800 190,209 151.002 97.652 185.205 98.510 5700

5800 32.800 193.489 131.572 98.212 188.405 99.075 5800

5900 32.000 196.769 132.133 98.782 191.765 99.650 5900

6000 32.800 200.049 132.684 99.343 195.045 100.177 6000

158 NASA/TP-3287/REV 1
TABLE IX.10, - THERMODYNAMIC FUNCTIONS FROM COEFFK_tENTS FOR

X _ H°(T)-H°(O) PO') qaot,.t)._(_v'r +(T) _°(X).n" T K -K kd/mol J/m_-K J/mo_K I_Hmd J/moI-K K

0 0.000 0.000 0,000 0.000 -8.569 INFINITE 0

200 29.206 5.705 133.306 104.784 -2.865 147.629 200

298.15 29.195 8.569 14_,960 116.219 0,000 144.960 298.15

300 29.196 8.623 145.140 116.397 0.054 144.960 $00

400 29.243 11.545 153.545 124,683 2.976 146.106 400

500 29.368 14.474 160.082 131.133 5.905 148.271 500

600 29.624 17,423 165.457 136.419 8.854 150.701 600

700 30.011 20.403 170.051 140.903 11.834 153.144 700

800 30,504 23.429 174.089 "144.804 14.859 155.515 800

900 51.065 26.506 177.714 148.262 17.937 157.784 900

1000 31.641 29.642 181.017 151.375 21.073 159.944 1000

1100 32.212 32.834 184.059 154.210 24.265 162.000 1100

1200 32.767 36.084 186.886 156.816 27.514 165.957 1200

1300 33.289 59.587 189.550 159.232 30.818 165.824 1500

1_00 33.775 42.740 192.015 161.686 34.171 167.607 1400

1500 34.224 46.140 196.360 165.600 57.571 169.313 1500

1600 34.656 69.584 196.583 165.593 41.015 170.948 1600

1700 55.016 55.067 198.694 167.478 44.498 172.519 1700

1800 35.366 56.586 200.705 169.269 48.017 176.029 1800

1900 35.689 60.139 202.626 170.974 51.570 175.484 1900

2000 55.988 65.723 206.665 172.603 55.154 176.888 2000

2100 36.266 67.336 206.227 174,163 58.767 178.243 2100

2200 56.525 70.975 207.920 175.659 62.406 179.554 2200

2300 36.768 74.640 209.549 177.097 66.071 180,823 2300

2400 36.998 78.329 211.119 178.482 69.760 182.053 2400

2500 57.215 82.039 212.634 179.818 73.470 183.266 2500

2600 37.421 85.771 216.098 181.109 77.202 184.406 2600

2700 37.619 89.523 215.514 182.357 80.954 185.531 2700

2800 37.809 93.295 216.885 183,566 86.726 186.626 2800

2900 37.993 97.085 218.215 184.738 88.516 187.692 2900

3000 38.171 100,893 219.506 185.875 92.324 188.731 3000

3100 38.344 104.719 220.761 186.980 96.150 189.745 3100

3200 38.516 108.562 221.981 188.055 99.993 190.733 3200

3300 38.681 112.422 223.168 189.101 103.853 ]91.698 3300

3400 38,845 116.298 226.326 190.120 107.729 192.641 3400

3500 39.007 120.191 225,454 191.114 111.621 193,562 3500

3600 39.168 124.099 226.555 192.083 115.530 194.663 3600

3700 39.327 128.024 227.630 193.029 119.455 195.365 3700

3800 39.485 131.965 228.681 193.954 123.396 196.209 3800

3900 39.641 135.921 229.709 194.857 127.352 197.055 3900

_000 39.797 139.893 230.715 195.741 131.324 197.886 4000

4100 39.952 143.880 231.699 196.606 135.311 198.696 4100

4200 60.106 147.883 232.664 197.453 139.3_4 199.494 6200

4300 60.258 151.901 233.609 198.283 143.332 200.276 6300

4600 40.409 155.935 234.536 199.097 167,366 201.044 4400

4500 40.559 159.983 255.646 199,896 151.614 201.799 6500

4600 40,706 164.066 236.339 200.677 155.477 202.560 4600

4700 40.851 168.124 237.216 201.445 159.555 203.268 4700

4800 40.996 172.217 238.078 202.199 163.647 205.985 4800

4900 61.133 176.325 238.925 202.960 167,756 204,689 4900

5000 41.268 180.4_3 239,757 203.668 171.876 205.382 5000

5100 61.399 186.576 240.575 206.384 176.007 206.064 5100

5200 41.525 188.723 241.381 205.088 180.I54 206.756 5200

5300 41.646 192.881 242.173 205.780 186.312 207.397 5300

5_00 41.760 197.052 242.952 206.661 188.483 208.048 5400

5500 41.868 201.233 243.719 207.132 192.666 208.690 5500

5600 61.967 205.425 246.475 207.792 196.856 209.322 5600

5700 62.058 209.626 245.218 208.442 201,057 209.965 5700

5800 42.139 213.836 245.951 209.082 205.267 210.560 5800

5900 42.209 218.054 246.672 209.713 209.685 211.166 5900

6000 42.268 222.278 247.381 210.335 213.709 211.763 6000

6200 42.371 230.762 268.769 211.553 222.173 212.935 6200

6400 62.438 239.224 250.116 212.737 230.656 214.076 6600

6600 _2.465 247.715 251.422 213.889 239.145 215.188 6600

6800 42.652 256.207 252.690 215.012 247.658 216.272 6800

7000 42.598 266.695 253.919 216.106 256.124 217.330 7000

7200 42.304 273.164 255.115 217.173 266.596 218.363 7200

7400 42.171 281.612 256.270 218.214 273.063 219.372 7400

7600 _2.003 290.050 257.392 219.231 281.461 220.358 7600

7800 41.801 298.611 258.481 220.223 289.842 221.322 7800

8000 41.569 306.748 259.536 221.193 298.179 222.266 8000

NASA/TP-3287/REV 1

159
T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

C o

J/moPl.K

41.310

41. 027

40.722

q0.398

40.059

39.706

39.342

38.970

38.591

38.207

37.239

36.275

35.353

34.426

33.561

32,746

31,981

31.268

30.605

29.990

29.421

28.894

28. ¢*05

27. 952

27.531

27.140

26.778

26,443

26.136

25.859

TABLE IX.le. • Conolucled.

H°_)'l"l°(O) S°C) "(G°(T)-H°(O))K H°(T) _%r')/T T

_h'n_ J_0l-K d/moI.K _lmol J_o_K K

315.037 260.560 222.141 306.468 223.186 8200

323.271 261.552 223.067 314,702 224.087 8400

331.446 262.514 223.974 322.877 224.970 8600

539.558 263.446 224.860 330.989 225.834 8800

347.604 264.350 225.728 339.035 226.680 9000

355.581 265.227 226.577 347.012 227,508 9200

363.486 266.077 227.408 354.916 228.320 9400

371.317 266.901 228.222 362,748 229,115 9600

379.073 267.701 229.020 370.504 229.894 9800

386.753 268.477 229.801 378.184 230.658 10000

405,615 270.318 231.688 397.046 232.504 10500

423.993 272.028 233,483 415.424 234.262 11000

441.894 273.619 235,194 433.324 235.939 11500

459.332 275.104 236.826 450.763 237.540 12000

476.327 276.691 238.385 467.757 239.071 12500

492,901 277,792 239,876 484,332 240.535 13000

509.081 279.013 241.303 500.512 241.938 13500

524.891 280.163 242.671 516.322 243.283 14000

540.357 281.248 243.902 531.788 244.573 14500

555.503 282.275 245.242 546.934 245.813 15000

570.355 283.249 246.452 561.785 247.005 15500

584.932 284.175 247.617 576.363 248.152 16000

599.255 285.057 248.738 590.686 269.257 16500

613.343 285.898 249.819 604.774 250.323 17000

627.212 286.702 25Q.861 618.643 251.351 17500

640.879 287.472 251.868 632.310 252.344 18000

654.357 288.211 252.840 645.788 253.303 18500

667.661 288.920 253.780 659.092 254.231 19000

680.805 289.603 254,690 672.236 255.129 19500

693.803 290.261 255.571 685.233 255.999 Z0000

160 NASA/TP-3287/REV l
TABLE IX.17. •THERMODYNAMIC FUNCTION8 FROM COEFFICIENTS FOR Bectron Gs8

T j C_ I.#(T')-_(_ _cr) _GQ('I')'H"(_ h_('r) _°('ryr K -K k,J/mol J/moFK J/_n_ kJ/m_ J/moI-K

0 0.000 0.000 0.000 0.000 -6.197 INFINITE

200 20.786 6.157 12.679 -8.107 -2.040 22.88Q

298.15 20.786 6.197 20.979 0.193 0.000 20.979

300 20.786 6.236 21.108 0.321 0.038 20.979

400 20.786 8.515 27.087 6.301 2.117 21.795

500 20.786 10.393 31.726 10.939 4.196 23.334

600 20.786 12.472 35.516 14.729 6.276 25.058

700 20.786 14.550 38.720 17.933 8.353 26.787

800 20.786 16.629 41.695 _20.709 10.432 28.656

900 20.786 18.708 43.946 23.157 12.510 30.043

1000 20.786 20.786 46.134 25.367 14.589 31.545

1100 20,786 22.865 68.115 27.329 16.667 32.963

1200 20.786 24.964 49.923 29.137 18.766 36.302

1300 20.786 27.022 51.587 30.801 20.825 35.568

1400 20.786 29.101 53.128 32.341 22.903 36.768

1500 20.786 31.179 54.562 33.776 26.982 37.907

1600 20.786 53.258 55.903 55.117 27.061 38.990

1700 20.786 35.337 57.163 36.377 29.139 60.023

1800 20.786 37.415 58.552 57.565 51.218 41.008

1900 20.786 39.494 59.475 58.689 33.296 41.951

2000 20.786 41.573 60.542 39.755 35.375 62.854

2100 20.786 63.651 61.556 40.770 37.454 43.721

Z200 20.786 45.730 62.523 41.757 39.532 44.554

2300 20.786 67.808 63.467 42,660 61.611 65.355

2600 20.786 69.887 64.331 43.545 43.690 46.127

2500 20.786 51.966 65.180 64.394 45.768 46.873

2600 20.786 56.064 65.995 45.209 67.847 47.593

2700 20.786 56.123 66.780 65.993 69.926 48.289

2800 20.786 58.202 67.556 46.7_9 52.004 48.963

2900 20.786 60.280 68.265 47.479 54.083 49.616

3000 20.786 62.359 68.970 48.183 56.161 50.269

3100 20.786 64.437 69.651 48.865 58.240 50.864

3200 20.786 66.516 70.311 49.525 60.319 51.462

3300 20.786 68.595 70.951 50.165 62.397 52.043

5400 20.786 70.673 71.571 50.785 64.676 52.608

5500 20.786 72.752 72.174 51.388 66.555 53.158

3600 20.786 76.831 72.760 51.973 68.633 53.695

3700 20.786 76.909 73.329 52.543 70.712 54.218

3800 20.786 78.988 73.883 53.097 72.790 5_.728

3900 20.786 81.066 76.623 53.637 74.869 55.226

4000 20,786 83.165 74.950 54.163 76.968 55.713

4100 20.786 35.224 75.463 56.677 79.026 56.188

6200 20.786 87.302 75.966 55.177 81.105 56.653

4300 20.786 89.381 76.453 55.667 83.184 57.108

4600 20.706 91.460 76.931 56.144 85.262 57.555

6500 20.786 93.533 77.398 56.612 87.361 57.989

6600 20.786 95.617 77.855 57.068 89.419 58.416

6700 20.786 97.695 78.502 57.515 91._98 58.834

6800 20,786 99.774 78.739 57.953 93.577 59.246

_900 20.786 101.853 79.168 58.382 95.655 59.666

5000 20.786 103.931 79.588 58.802 97.736 60.041

5100 20.786 106.010 80.000 59.213 99.813 60.628

5200 20.786 108.089 80.403 59.617 101.891 60.809

5300 20.786 110.167 80.799 60.013 103.970 61.182

5600 20.786 112.246 81.188 60.601 106.068 61.549

5500 20.786 116.325 81.569 60.783 108.127 61.910

5600 20.786 116.603 81.94_ 61.157 110.206 62.26_

5700 20.786 118.482 82.311 61.525 112.284 62.612

5800 20.786 120.560 82.673 61.887 114.363 62.955

5900 20.786 122.639 83.028 62.242 116.662 63.292

6000 20.786 124.718 83.378 62,591 118.520 63.624

6200 20.786 128.875 84.059 63.273 122.677 64.273

6600 20.786 133.032 84.719 63.933 126.835 64.901

6600 20.786 137.189 85.359 66.573 130.992 65.512

6800 20.786 141.367 85.979 65.193 135.169 66.104

7000 20.786 145.504 86.582 65.796 139.306 66.681

7200 20.786 169.661 87.167 66.381 1_3.464 67.262

7400 20.786 153.818 87.737 66.951 147.621 67.788

7600 20.786 157.976 88.291 67.505 151.778 68.321

7800 20.786 162.133 88.831 68.065 155.956 68.840

8000 20.786 166.290 89.358 68.571 160.093 69,346

T

K

0

200

298.15

300

400

500

600

700

800

900

IO00

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

6000

4100

4200

4300

4600

450O

6600

4700

4800

6900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6600

6600

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV 1

161
TABLE IX,17, - Conc;uded.

T C ° H°_).HO(0) So_) _Go(.r).HO(0)}K

K JIm_l-K _ol _m_-K JlmoFK

8200 20.786 170.447 89.871 69.085

8400 20.786 174.605 90.372 69.585

8600 20.786 178.762 90.861 70.075

8800 20.786 182.919 91.339 70.552

9000 20.786 187.076 91.806 71.020

9200 20.786 191.234 92.263 71.476

9400 20.786 195.391 92.710 71.923

9600 20.786 199.548 93.147 72.361

9800 20.786 203.705 93.576 72.790

10000 20.786 207.863 93.996 73,210

10500 20.786 218.256 95.010 74.224

11000 20.786 228.649 95.977 75.191

11500 20.786 239.042 96.901 76.115

12000 20.786 249.435 97.786 76.999

12500 20.786 259.828 98.634 77.848

13000 20.786 270.222 99.449 78.663

13500 20.786 280.615 100.234 79._48

14000 20.786 291.008 100.990 80.204

14500 20.786 301.401 101.719 80.933

15000 20.786 311.794 102.424 81.638

15500 20.786 322.187 103.106 82.319

16000 20.786 332.580 103.765 82.979

16500 20.786' 342.974 104.405 83.619

17000 20.786 353.367 105.026 84.239

17500 20.786 363.760 105.628 84.842

18000 20.786 374.153 106.214 85.427

18500 20.786 384.546 106.783 85.997

19000 20.786 594.939 107.338 86.551

19500 20.786 405.332 107.878 87.091

20000 20.786 415.726 108._04 87.618

H%r)

kJImol

164.250

168.407

172.565

176.722

180.879

185.036

189.194

193.351

197.508

201.665

212.058

222.452

232.845

243.238

255.631

264.024

274.417

284.810

295.204

305.597

315.990

326. 383

336.776

3_7. 169

357.562

367. 956

378.349

588. 742

599. 135

409.528

_°F)K

J_oI-K

69.840

70.325

70.795

71.257

71.708

72.150

72.583

73.007

73,q22

73.829

74.81_

75.75_

76.654

77.516

78,344

79.140

79.907

80.646

81.360

82.051

82.719

83,367

83,994

84.604

85.196

85.772

86.352

86.878

87.4D9

87.927

T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

11000

115o0

12000

12500

13000

13500

1_000

14500

15000

15500

26000

16500

17000

175O0

18000

18500

19000

19500

20000

162 NASA/TP-3287/REV l
TABLE IX.18. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR F2

T 0 ° H°(T)'_(O) 8°(I) _G°(T)'I'P(0_K H°(I") _°(wr

K J/m_FK _ J/mol_ J/moI-K kJ/mol J/m_

0 0.000 0.000 0,000 0,000 -8,825 INFINITE

200 29.687 5.837 190,658 161,474 -2,988 205.599

298.15 31.304 8.825 202,792 173.193 0.000 202.792

300 31.338 8,883 202.986 173.376 0.058 202:793

400 32.992 12.102 212.236 181.980 3.277 204.043

500 34.259 15.468 219.742 188.805 6.643 206.455

600 35,174 18.942 226,073 194.505 10.117 209.211

700 35.838 22.495 231.548 ,199,413 13.670 212.020

800 36.341 26.105 236.368 203.737 17.280 214.768

900 36.743 29.760 240,672 207.606 20.935 217.411

1000 37,065 33,451 244.561 211.110 24.626 219.935

1100 37.352 37.172 2_8.107 214.314 28.347 222.337

1200 37.584 40.919 251.368 217.268 32.094 224.622

1300 37,798 44.688 254.384 220.009 35.863 226.797

1400 38,006 48.479 257.193 222.566 39.654 228.869

1500 38.208 52.290 259.822 224.963 43,464 230.846

1600 38.399 56.120 262.294 227.219 47.295 232.735

1700 38.574 59,969 264,628 229.352 51.144 234,543

1800 58.728 63.834 266,837 231,374 55.009 236.276

1900 38.854 67.714 268,934 233.296 58.888 237.941

2000 38.949 71.604 270.930 235.228 62.779 239.541

2100 39.011 75.502 272.832 236.878 66.677 241.081

2200 39.037 79.405 274.647 238.554 70,580 242.566

2300 39.027 83.508 276,383 240.162 74.483 243.999

2400 38.980 87,209 278,043 241,706 78,384 245.383

2500 38,898 91.103 279.652 243.191 82.278 246.721

2600 38,780 94.987 281,156 244,622 86.162 248.017

2700 38.630 98.858 282.617 246.003 90.033 249.271

2800 38.448 102.712 284.018 247.335 93.887 250.487

2900 38,238 106.547 285.364 248,624 97.722 251.667

3000 38,000 110.559 286.656 249,870 101.534 252.812

3100 37.739 114.146 287.898 251.077 105.321 253.924

3200 37.456 117.906 289.092 252,246 109.081 255.004

3300 37.154 121.637 290.240 253.380 112.812 256.055

3400 36.837 125.336 291.344 25_.481 116.511 257.076

3500 56,505 129.004 292.407 255,549 120.178 258.071

3600 36.163 132,637 293.431 256.587 123.812 259.039

3700 35.813 136.236 294.417 257.597 127.411 259.982

3800 35.457 139,799 295.568 258,578 130,974 260,901

3900 35.097 163.327 296,284 259.533 134.502 261.796

4000 34.736 146.819 297.168 260._63 137.994 262.670

4100 34.375 150.274 298.021 261.369 141,449 263.521

4200 34.017 153.694 298.845 262.251 144.869 264,353

4300 33,663 157.078 299.642 263.112 148.253 265.164

4_00 33.314 160.427 300.411 263.951 151.602 265.957

4500 32.971 163.741 301.156 264.769 154.916 266.731

4600 32.637 167.021 301.877 265.568 158.196 267.487

4700 32.311 170,269 302,576 266,348 161.443 268.226

4800 31.993 173.484 303.253 267.110 164.659 268.949

4900 31.686 176.668 303.909 267.854 167.842 269.655

5000 31.388 179.821 304,546 268.582 170.996 270.347

5100 31.099 182.945 305.165 269.293 174.120 271.024

5200 30.819 186.041 305.766 269.989 177,216 271.686

5300 30,548 189,110 306.350 270.669 180.284 272.335

5_00 30.284 192.151 306.919 271.335 183.326 272.970

5500 30.027 195.167 307.472 271.988 186.341 273.592

5600 29.775 198.157 308.011 272.626 189.332 274.202

5700 29.526 201.122 308.536 273.251 192.297 274.800

5800 29.279 204.062 309.047 273.864 195.237 275.386

5900 29.032 206.97S 309.546 274.465 198.152 275,961

6000 28.782 209.868 310.032 275,054 201.043 276.524

T

K

0

200

298.15

300

400

5O0

600

700

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV 1

163
TABLE I)(.19. - THERMODYNAMIC FUNCTION8 FROM OOEFFIGIENT8 FOR Fe(a,y,_,,l_

T J/_;-K H°(T'pH°(O) 80(1") -{G°('r)-,I"P(O)}¢T I..P(T) .,G°(T:r)/T T

K kJ/mol J/tool K J/moI-K kJ/mol d/moI-K K

0 0,000 0.000 0.000 0,000 -4.507 INFINITE 0

200 21.588 2.192 17.948 6_990 -2.315 29.525 200

298.15 25.094 4.507 27.321 12.204 0.000 27.321 298.15

300 25.139 4.553 27.476 12.298 0.046 27.321 300

400 27.587 7.181 35.021 17.068 2.674 28.335 ¢00

500 29.702 10.034 41.577 21.309 5.527 30.323 500

600 52.047 13.120 46.996 25.130 8.615 52.642 600

700 34.599 16.449 52.123 28.625 11.942 35.065 700

800 37.948 20.066 56.948 51.866 15.559 57.499 800

900 43.080 24.140 61.740 34.917 19.655 39.925 900

1000 54.591 28.684 66.518 37.835 24.177 42.342 1000

1100 46.315 35.115 72.658 40.735 30.608 44.833 1100

a 1184 41.¢10 38.428 75.562 45.106 33.921 46.913 1184

;-1_;;......_;:;;_ ......;;?;_;......_E;_;......;;S;_......;;T;_ ......;_:;_;......_;;---

1200 33.937 39.870 76.778 43.552 55.363 ¢7.308 1200

1300 34.657 43.296 79.519 46.215 38.789 ¢9.682 1500

1400 35.598 _6.809 82.122 _8.687 ¢2.302 51.907 1_00

1500 36._75 50.413 84.609 51.000 45.906 54.004 1500

1600 57.303 54.102 86,989 53.175 49,595 55.992 1600

? ]665 37.913 56.546 88.686 54.525 52.039 57.231 1665

7;;;; ......;_ ......;;T;;;......;;T;;;......;;_;_;......;_;_; ......;_T_;_......_;;;---

1700 41.406 58.827 89.847 55.243 54.320 57.894 1700

1800 42.450 63.017 92.242 57.252 58.510 59.736 1800

6 1809 42.557 63.400 92.454 57.407 58.893 59.898 1809

T_;;; ......;;T_; ......_:_ ....._;;:;;_ ......;_T;;_......_S_; ......;;T;;;......_;;;-'-

1900 46.024 81.395 102.545 59.506 76.888 61.878 1900

2000 46.024 85.997 10_.706 61.707 81.490 63,961

2100 46.024 90.600 106.951 63.809 86.093 65.955

2200 ¢6.024 95.202 109.092 65,819 90.695 67.867

2300 46.024 99.804 111.138 67.745 95.297 69.704

2400 46.024 104.407 113.097 69.594 99.900 71.472

2500 46.024 109.009 114.976 71.372 104.502 73.175

2600 46.024 113.612 116.781 73.084 109.105 74.817

2700 46.024 118.214 118.518 74.735 113.707 76.404

2800 46.024 122,816 120.192 76.329 118.309 77.938

2900 46.024 127.419 121,807 77,869 122.912 79.423

3000 46.024 132.021 123.367 79.360 127,514 80.862

3100 46.024 136.624 124.876 80.80_ 132.117 82.258

3200 46.024 141.226 126.337 82.204 136.719 83.612

3300 46.024 145.828 127.755 83.563 141.321 84.929

3400 46.024 150.431 129,127, 84.883 145.924 86.209

3500 46.024 155.033 130.461 86.166 150.526 87.454

3600 46.024 159.636 131.758 87._15 155.129 88.667

3700 46.024 164.238 133.019 88.630 159.731 89.848

3800 46.024 168.840 134.246 89.815 164.533 91.001

3900 46.024 173.443 135.442 90.969 168.936 92.125

4000 46,024 178.045 156.607 92.096 173.538 93.223

4100 46.024 182.648 137.744 95.195 178.141 94.295

4200 46.024 187.250 138.855 94.269 182.743 95.342

4300 46.024 191.852 139.936 95.319 187.545 96.367

4400 46.024 196.455 140.994 96.345 191.948 97.569

4500 46.024 201.057 142.028 97.349 196.550 98.350

_600 46.024 205.660 143.040 98.331 201.155 99.311

4700 46.024 210.262 1_4.029 99.293 205.755 100.252

¢800 46.024 214.864 144.998 100.235 210.557 101.174

4900 46.024 219.467 145.947 101.158 214.960 102.078

5000 46.024 224.069 146.877 102.063 219.562 102.965

5100 46.024 228.672 147.788 102.951 224.165 103.835

5200 46.02_ 233.274 148.682 103.822 228.767 104.689

5300 ¢6.024 237.876 149.559 104.677 253.369 105.527

5400 46.024 242.479 150.419 105.516 237.972 106.550

5500 46.024 247.081 151.264 106.340 242.574 107.159

5600 46,024 251.684 152.093 107.149 247.177 107.954

5700 46.024 256.286 152.908 107.945 25].779 108.736

5800 46.024 260.888 153,708 108.727 256.381 109.504

5900 46.024 265.491 154.495 109.496 260,984 110.260

6000 46.024 270.093 155.268 110.253 265.586 111.004

2000

2100

2200

2500

2¢00

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4¢00

4500

4600

4700

4800

4900

5000

5100

5200

5500

5400

5500

5600

5700

5800

5900

6000

164 NASA/TP-3287/REV l
T

K

0

200

298.15

300

4OO

500

600

700

800

900

TABLE IX,20. - THERMODYNAMIC FUNCTIO(_ FROM COEFFICIENT8 FOR Ge(or._

Co HO_.l-P(O)+ s_('r) -{G°(T)-W(0)Fr H°(T) "G°(Tyr

J/m_l-K kJhnol J/mot-K J/mo1-K kJ/mc_ J/moI-K

0.000 0.000 0.000 0.000 -4.636 INFINITE

21.130 2.436 22.167 9.984 -2.200 33.166

23.222 4.636 31.090 15.540 0.000 31.090

23.246 4.679 31.234 15.636 0.043 31.090

24,310 7.063 38.083 20.426 2.426 32.017

24.962 9.528 43.582 24.525 4.892 33.798

25.453 12.050 48.178 28.095 7.414 35.822

25.867 14.616 52.133 31.253 9.980 37.876

26,241 17.222 55,612 34,085 12.586 39.880

26.591 19.864 58.723 36.652 15,227 41.804

T

K

0

200

298.15

300

400

500

600

700

800

900

1000 26.926 22.540 61.542 39.003 17,905 43.639 1000

99 64 124 41 171 20 612 45.385 1100

1100 _Z'_ _'_en 66"509 43:184 23:353 _Z'_ _P _n

1200 Z_._ _'_ _'770 43.405 23.668 _.zo_ _c_,._-

cr 1211.40 2/.6U! co. Ju_ _ ....................................................

........................... T;34 ...... 97 338 43 405 60 698 47.232 1211.40 I 1211.40 27.600 6_ ..... "_o_ _'1_ 63"143 50.714 1300

1300 17. 600 67.,_u _._o ;_._ 65:903 54.257 1400

1400 Zt.600 70.540 1..... 1 •

1500 27.600

1600 27.600

1700 27.600

1800 27.600

1900 27.600

2000 27.600

2100 27.600

2200 27.600

2300 27.600

2400 27.600

2500 27.600

260O 27.600

2700 27.600

2800 27.600

2900 27.600

3000 27.600

3100 27.600

3200 27.600

3300 27.600

3400 27.600

3500 27.600

3600 27.600

3700 27.600

3800 27.600

3900 27.600

4000 27.600

4100 27.600

4200 27.600

4300 27.600

4400 27.600

4500 27.600

460O 27.600

4700 27.600

4800 27.600

4900 27.600

5000 27.600

5100 27.600

5200 27.600

5300 27.600

5400 27.6O0

5500 27.60O

56O0 27.600

5700 27.600

5800 27.600

5900 27.600

6000 27.600

73,500 103.235 54.369 68.663 57.460 1500

76.060 105.017 57.479 71.423 60.377 1600

78.820 106.690 60.325 74.183 63.053 1700

81.580 108.267 62.945 76.943 65,521 1800

84.340 109.760 65.370 79.703 67.811 1900

87.100 111.175 67.626 82.465 69.964 2000

89.860 112.522 69.732 85.223 71,940 2100

92.620 113.806 71.706 87.983 73.814 2200

95.380 115.033 73.563 90.743 75.579 2300

98.140 116,207 75.316 93.503 77,248 2400

100.900 117.334 76.974 96.265 78.829 2500

103.660 118.417 78.548 99.023 80.331 2600

106.420 119.458 80.044 101.783 81.761 2700

109.180 120,462 81.469 104.543 83.125 2800

111.940 121.431 82.831 107.303 84.429 2900

114.700 122.366 84.133 110.063 85.678 3000

117.660 123.271 85.381 112,823 86.877 3100

120.220 124.148 86,579 115.583 88,028 3200

122.980 124,997 87.730 118.343 89.135 3300

125.740 125.821 88.839 121.103 90.202 3400

128.500 126.621 89.907 123.863 91.231 3500

131.260 127.398 90.937 126.623 92.225 3600

134.020 128.155 91.933 129.383 93.186 3700

136.780 128,891 92.896 132.143 94.116 3800

139,540 129.607 93.828 134.903 95.017 3900

142.300 150.306 94.731 137.663 95,890 4000

145.060 130.988 95.607 140.423 96.738 4100

147.820 131.653 96.458 143.183 97.562 4200

150.580 132.302 97.284 145.943 98.362 4300

153.340 132.937 98.087 148.703 99.141 4400

156.100 133.557 98.868 151.463 99.899 4500

158.860 134.164 99.629 154.223 100.637 4600

161.620 134.757 100.570 156.983 101.357 4700

164.380 135.338 101.093 159.743 102.058 4800

167.140 135.907 101,797 162.503 102,74_ _900

169.900 136.465 102.485 165.263 103.412 5000

172.660 137,012 103.157 168,023 104.066 5100

175.420 137.548 103.813 170.783 104.705 5200

178.180 138.073 104.454 173.543 105.329 5300

180,940 138.589 105.082 176,305 105,940 5400

183.700 139.096 105.696 179.063 106.539 5500

186.460 139.593 106.297 181.823 107.124 5600

189.220 140.081 106,885 184.583 107.698 5700

191.980 140.561 107.461 187.343 108.261 5800

194.740 1_1.033 108,027 190,103 108.812 5900

197.500 141.497 108.581 192.863 109.353 6000

NASA/TP-3287/REV 1

165
TABLE IX._I.

•THERMODYNAMIC FUNCTION8 FROM COEFRCIENT8

K J_l_ kJtrno_ J/moFK J.'mo|-K kJ/m_ 0 0.000 0.000 0.000 0.000 -8.468

200 27.665 5.693 I19.609 90.965 -2.775

298.15 28.836 8.468 130.681 102.279 0.000

300 28.869 8.521 130.859 102.455 0.053

600 29.189 11.628 139.218 110.649 2.960

500 29.256 16.351 145.760 117.039 5.883

600 29.318 17.279 151.079 122.281 8.811

700 29.444 20.216 155.607 126.726 11.748

800 29.629 23.170 159.550 i30.588 14.701

900 29.873 26.144 163.053 136.006 17.676

1000 30.206 29.147 166.217 137.070 20.679

1100 30.567 32.105 169.112 139.853 23.717

1200 30.983 55.262 171.789 142.404 26.794

1300 31.421 30.302 174.286 144.761 29.914

1400 31.866 61.547 176.631 146.955 33.079

1500 32.305 64.755 178.845 149.008 36.287

1600 32.732 68.007 180.943 150.939 39.539

1700 33.144 51.301 182.940 152.763 42.833

1800 33.539 5_.636 184.846 154.493 66.167

1900 33.916 58.008 186.669 156.139 _9.540

2000 34.276 61.418 188.418 157.709 52.950

2100 34.618 64.863 190.099 159.212 56.395

2200 34.944 68.341 191.717 160.653 59.873

2300 35.254 71.051 193.277 162.038 63.383

2400 35.550 75.392 194.784 163.371 66.924

2500 35.832 78,961 196.241 164.657 70.493

2600 36.102 82.558 197.652 165.899 74.090

2700 36.361 86.181 199.019 167.100 77.713

2800 36.609 89.830 200.346 168.266 81.361

2900 36.848 93.502 201.635 169.393 85.034

3000 37.078 97.199 202.888 170.488 88.731

3100 37.301 100.918 204.107 171.553 92.650

3200 37.518 104.659 205.295 172.589 96.191

3300 37.728 108.421 206.453 173.598 99.953

3400 37.934 112.204 207.582 174.581 203.736

3500 38.135 116.008 208,685 175.540 107.560

3600 38.331 119.831 209.762 176.675 111.363

3700 38.525 123.674 210.815 177.389 115.206

3800 38.715 127.536 211.844 178.282 119.060

3900 38.902 131.417 212.853 179.156 122.949

4000 39.087 135.316 213.840 180.011 126.868

4100 39.269 139.234 214.807 180.848 130.766

4200 39.469 143.170 215.756 181.668 134.702

4300 39.627 147.124 216.686 182.471 138.656

4400 39.802 151.095 217.599 183,259 142.627

4500 39.975 155.086 218.495 186.032 166.616

4600 40.165 159.090 219.376 184.791 150.622

4700 60.312 163.113 220.24'1 185.536 154.665

_800 40.476 167.153 221.091 186.268 158.684

6900 40.637 171.208 221.928 186.987 162.740

5000 40.793 175.280 222.750 187.694 166.812

5]00 40.964 179.367 223.560 188.390 170.899

5200 41.090 183.468 224.356 189.076 175.000

5300 41.230 187.584 225.140 189.767 179.116

5400 41.363 191.714 225.912 190.609 183.266

5500 41.688 195.857 226.672 191.062 187.389

5600 41.604 200.011 227.621 191.706 191.563

5700 41.711 206.177 228.158 192.337 195.709

5800 41.807 208.355 228.884 192.961 199.885

5900 41.891 212.538 229.600 193,576 204.070

6000 41.962 216.731 230,306 194.183 208.263

6200 42.096 225.137 231.683 195.370 216.669

6_00 42.194 233.567 233.021 196.526 225.099

6600 42.251 242.012 234.320 197.652 233.544

6800 42.266 250.465 235.582 198.749 261.996

7000 42.239 258.916 236.807 199.819 250.448

7200 42.169 267,357 237.996 200.863 258.889

7400 62.060 275.781 239.150 201.882 267.313

7600 61.914 284.179 240.269 202.878 275.711

7800 61.733 292.544 241.356 203.850 284.076

8000 41.520 300.870 242.410 206.801 292.402

r-OR ,_

_*(Tyr

J/mol_

1NFINZTE

133.286

130.681

130.682

131.819

133.975

136.394

158.823

141.173

143.413

145.538

147.551

149,461

151.275

153.004

154.653

156.231

157.744

159.197

160.596

161.943

163.244

164.502

165.719

166.899

168.044

169.156

170.236

171.288

172.313

173.311

174.285

175.235

176.166

177.071

177.959

178.827

179.678

180.511

181.327

182.128

182.913

183.684

186.440

185.184

185.914

186.632

187.338

288.032

188.715

189.388

190.050

190.702

191.345

191.978

192.601

193.217

193.823

196.421

195.012

195,596

196.756

197.849

190.935

199.994

201.028

202.059

203.026

203.992

204.936

205.860

TK0

200

298.15

300

40O

500

6O0

700

800

900

1000

1100

1200

1300

1_00

1500

1600

1700

1800

1900

2000

2100

2200

Z300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

5800

3900

4000

6100

4200

4300

4400

6500

4600

4700

4800

4900

5000

5100

5200

5300

5600

5500

5600

5700

5800

5900

6000

6200

6600

6600

6800

7000

7200

7400

7600

7800

8000

166 NASA/TP-3287/REVl
T

K

8200

8400

B600

8800

9000

9200

9400

960O

98O0

10000

10500

llOO0

11500

12000

12500

13000

13500

1_000

1_500

15000

15500

16000

16500

17000

17500

18000

38500

19000

19500

20000

C °

j/moPl.K

_1.279

41.011

40.721

40.411

40.08<i

39.743

39.390

39. 026

38.656

38.280

37. 326

36.372

35,437

34.533

33.669

32.855

32.086

31.369

30.703

30.084

29.511

28.979

28.487_

28.030

27.605

27.211

26.845

26.507

26. 197

25.915

"fABLEIX21. - Conc;uded.

H°_)'H°{_ S°@) _GO(T_.HO(0))_ Ho(.r) .GO{T)n T

kJ/mol J?moI-K _mot-K kJImoi _moI-K K

309.150 243.432 205.731 300.682 206.764 8200

317.380 244.424 206.6_1 308.912 207.6_9 8400

325.555 245.385 207.530 317.085 208.515 8600

333.667 246.318 208.401 325.199 209.36_ 8800

341.717 247,223 209.254 333.249 210.195 9000

349.700 248.100 210.089 341.232 211.010 9200

357.613 248.951 210.907 349.145 211.808 9_00

365.455 249.776 211.708 356.987 212.590 9600

373.223 250.577 212.493 364.755 213.357 9800

380.917 251.354 213.263 372.449 21_.110 10000

399.819 253.199 215.121 391.351 215.928 10500

418.243 254.913 216,891 409.775 217.661 11000

436.194 256.510 218,580 427.726 219.316 11500

_53.685 257.998 220.191 4_5.217 220.897 12000

470.734 259.591 221.732 462.266 222.409 12500

487.362 260.695 223.206 478.894 223.857 13000

503.595 261.920 224.617 495.126 225.244 13500

519.456 263.074 225.970 510.988 226.575 14000

534.972 264.163 227.268 526.504 227.853 14500

550.167 265.193 228.516 541.699 229.080 15000

565.063 266.170 229.715 556,595 230.261 15500

579.684 267,099 230,869 571.216 231.398 16000

59_.049 267.983 231.980 585.581 232.493 16500

608.177 268.826 233.051 599.709 233.549 17000

622.084 269.633 234.085 613.616 234.569 17500

635.787 270.405 235.083 627.319 235.554 18000

649.300 271.145 236.048 640.832 236.506 18500

662.657 271.857 236.981 654.169 237.427 19000

675.812 272.541 237.884 667.344 238.318 19500

688.838 273.201 238.759 680.370 239.182 20000

NASA/TP-3287/REV 1

167
TABLE IX.22.. THERMODYNAMIC FUNC_ONS FROM COEFFICIENTS FOR He

T C o HO(.T).Ho(O) SO(T) .{Go(.r).Ho_)}_ H°(T)

K Jhn_l-K kJ/mot Jhnoi-K JlmoI-K kJhn_

0 0.000 0.000 0.000 0.000 -6. 197

200 20.786 4.157 II7.854 97.068 -2.040

298.15 20.786 6.197 126.154 ]05.367 0.000

300 20.786 6.236 126.282 105.496 0.038

400 20.786 8.315 132.262 111.476 2.117

500 20.786 ]0.393 156.900 116.114 4.196

600 20.786 12.472 140.690 119.904 6.274

700 20.786 14.550 143.894 123.108 8.353

800 20.786 16.629 146.670 125.884 10.432

900 20.786 18.708 149.118 128.332 12.510

1000 20.766 20.786 151.308 130.522 14.589

llO0 20.786 22.865 153.290 132,503 16.667

1200 20.786 24.944 155.098 134.312 18.746

1300 20.786 27.022 156.762 135.976 20.825

1400 20.786 29.101 158.302 137.516 22.903

1500 20.786 31.179 159.736 138,950 24.982

1600 20.786 33.258 161.078 140.292 27.061

1700 20.786 35.357 162.338 141.552 29.139

1800 20.786 37.415 163.526 142.740 31.218

1900 20.786 39.494 164.650 143.864 33.296

2000 20.786 41.573 165.716 144.930 35.375

2100 20.786 43,651 166.730 145.944 37.454

2200 20.786 45.730 167.697 146.911 39.532

2300 20.786 47.808 168.621 147.835 41.611

2400 20.786 49,887 169.506 148.720 43.690

2500 20.786 51.966 170.355 149.568 45.768

2600 20.786 54.044 171.170 150.384 47.847

2700 20.786 56.123 171,954 151.168 49.926

2800 20.786 58.202 172.710 151.924 52.004

2900 20.786 60.280 173.440 152.653 54.083

3000 20.786 62.359 174,144 153.358 56.161

3100 20.786 66.437 174.826 ]54.040 58.240

5200 20.786 66.516 175.486 ]54.700 60.319

3300 20.786 68.595 176.126 155,359 62.397

3400 20.786 70.673 176.766 155.960 64.476

3500 20.786 72.752 177.349 156.562 66.555

3600 20.786 74,831 177.934 157.168 68.633

3700 20.786 76.909 178.506 157.717 70.712

3800 20.786 78.988 179.058 158.272 72.790

5900 20.786 81.066 179.598 158.812 74.869

4000 20.786 83.145 180.124 159.338 76.948

_i00 20,786 85.224 180.638 159,851 79.026

4200 20.786 87.302 181.138 160.352 81.105

4300 20.786 89.381 181.628 160.861 83.184

4400 20.786 91.460 182.105 161.319 85.262

4500 20.786 93.538 182.573 161.786 87.341

6600 20.786 95.617 183.029 162.265 89,419

4700 20.786 97.695 183.476 162.690 91.498

4800 20.786 99.776 183.914 163.128 93.577

4900 20.786 101.853 186.345 163.556 95.655

5000 20.786 103.931 184.763 163.976 97.754

5100 20.786 106.010 185.176 164.388 99.815

5200 20,786 108.089 185.578 166.792 101.891

5500 20.786 110.167 185,974 165.188 103.970

5600 20.786 112.246 186.362 165.576 106.048

5500 20.786 114.325 186.744 165.957 108.127

5600 20.786 116.403 187.118 166.332 110.206

5700 20.786 118.482 187.486 166.700 112.284

5800 20,786 120.560 187.848 167.061 ]14.363

5900 20.786 122.659 188.203 167.617 116.442

6000 20.786 124,718 188.552 167.766 118.520

6200 20.786 128.875 189.234 168.448 122.677

6400 20.786 133.032 189.894 169.108 126.855

6600 20.786 137.189 190.533 169.747 130.992

6800 20.786 141.346 191.154 170.368 135.149

7000 20.786 145.504 191.757 170.970 139.306

7200 20.786 149.661 192.342 171.556 163.463

7400 20.786 153.818 192.912 172.125 167.621

7600 20.786 157,975 193.466 172.680 151.778

7800 20.786 162.133 194.006 173.220 ]55.955

8000 20.787 166.290 194.532 , 173.746 160.092

_mot-K

INFINITE

128.055

126.154

126.154

126.969

128.509

130.233

131.962

133.631

135.218

136.720

138.137

139.476

i_0.7_3

141.963

163.082

144.165

165.197

166.183

167.126

148.029

]48.895

]49.728

150,530

151.302

152.0_7

152.767

153.463

154.137

154.791

155.424

156.039

156.636

157.217

157.783

158.333

158.869

159.392

159.903

160.601

160.887

161.363

161.828

162.283

162.728

163.163

163.590

164.009

166.619

166.821

165.216

165.603

165.983

166.357

166.724

167.084

167.439

167.787

168.130

168.467

]68.799

169.467

170.076

170.686

171.279

171.856

172.417

172.963

173.495

174.014

174.521

T

K

0

2O0

298.15

3OO

400

500

600

7O0

800

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

Z000

2100

22OO

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

6200

4300

4400

4500

6600

4700

6800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

168 NASA/TP-3287/REV 1
TABLE IX.22. - Conoluded.

T C_ _(-0.H_) So_) _GP_)-NQ(_)n _(T) _°_)n

K JlmoI-K _nol JhnoI-K J/moI-K kJ/m_ JlmoI-K K

8200 20.787 170.447 195.045 174.259 164.250 175,015 8200

8400 20.787 174.604 195.546 174,760 168.407 175.498 8_00

8600 20.786 178.762 196.035 175.249 172.564 175.970 8600

8800 20.786 182.919 196.513 175.727 176,722 176,431 8800

9000 26.786 L87.076 196.980 176.194 180.879 176.883 9000

9200 20.786 191.234 197.437 176.651 185.036 177.325 9200

9400 20.786 195.391 197.884 177.098 189.193 177.757 9400

9600 20,786 199.548 198.322 177.536 193.351 178.181 9600

9800 20,786 203.705 198.751 177.964 197.508 178.597 9800

10000 20,786 207,862 199.171 178.384 201.665 179.004 10000

10500 20.786 218,255 200.185 179.398 212.058 179.989 10500

11000 20.786 228.648 201,152 180.365 222.451 180.929 11000

11500 20.786 239.041 202.076 181.289 232.843 181.828 11500

12000 20,786 249.454 202.960 182.174 243.236 182.690 12000

12500 20.786 259.827 203.809 183,023 253.629 183.518 12500

13000 20.787 270.220 204.624 183.838 264.022 184.315 13000

13500 20.788 280.613 205.408 184.622 274.416 185.081 13500

14000 20.789 291.007 '206.169 185.378 284.810 185,821 14000

14500 20.791 301.402 206.894 186.108 295.205 186.535 14500

15000 20.793 311.798 207.599 186.812 305.601 187.226 15000

15500 20.796 322,195 208.281 187._94 315.998 187.894 15500

16000 20.801 332,595 208.941 188.154 526,397 188.5_1 16000

16500 20.806 342.996 209.581 $88.794 336.799 189.169 16500

17000 20.813 353._01 210.202 189.414 347.203 189.779 17000

17500 20.822 365.810 210.806 190.017 357,612 190.371 17500

18000 20.833 374.223 211.393 190.602 368.026 190.947 18000

18500 20.847 384.643 211.964 191.172 378.445 191.507 18500

19000 20.865 395.070 212,520 191.727 388.873 192.053 19000

19500 20.883 405.507 213.062 192.267 399.309 192.585 19500

20000 20.907 415.95_ 213.591 192,793 q09.757 193.103 20000

NASA/TP-3287/REV 1

169
TABLE IX.23. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Hg(cr.I)

T C o Ho('I')'H°(O) S°(I-) "{G°(T)'H°(O))/T H°(l') "GO0")/T T

K J/moPI-K kJ/rood JlmoI-K J/mol-K kJ/mol Jlmot-K K

0 0. 000 0.000 0. 000 0. 000 -9,5_3 INFINITE 0

200 27.275 4.291 55.022 33. 568 -5. 052 80,285 200

cr 234.29 28,485 5.246 59.428 37.037 -4.097 76.915 234.29

t 234.29 28.476 7.541 69.225 57.037 -1.802 7"6.915 254.29

298.15 27.975 9.364 76.050 64.691 0.001 76.028 298.15 300

400

500

600

700

800

900

I000

IIO0

1200

1300

i_00

1500

1600

1700

1800

1900

2000

27.961 9,595 76.203 44.885 0.052 76.028 300

27.412 12.161 84.163 53.760 2.818 77,118 400

27.I76 1_.888 90.250 60._73 5.545 79.159 500

27.]39 17.602 95.198 65.861 8.259 81.432 600

27.292 20.322 99.390 70.359 10.979 83.706 700

27.580 23.065 103.052 74.221 13.722 85.900 800

27.895 25.838 I06.319 77.609 16._95 87.990 900

28.211 28.644 109.274 80.630 19.301 89.973 I000

28.524 31.481 111.978 83.359 22.138 91.852 II00

28.836 34.349 Ii_.473 85.849 25.006 93.655 1200

29.149 37.248 116.793 88.141 27.905 95.328 1300

29.464 q0.179 118.965 90.266 30.836 96.940 1400

29.779 43.141 121,009 92,248 33.798 98.477 1500

30.095 _6.134 122,940 94.107 36.791 99.946 ]600

30,407 49.159 124.774 95.857 39.816 101.353 1700

30,719 52.216 126.521 97.512 _2.873 102.703 1800

31.031 55.303 128.190 99.084 45.960 104.001 1900

31.348 58.422 129.790 100.579 49.079 105.251 2000

170 NASA/TP-3287/REV 1
TABLE IX.24. - THERMODYNAM_ FUNCTIONS FROM COEFFICIENTS FOR _(or.

T C o H°('I')'PP(_ $°C1") _GO(T).HO(O)}K HO(T) _o(-r)_ T

K J_-K _o} JlmoI-K J_ol-K _ JlmoI-K K

0 0.000 0.000 0.000 0.000 -13.196 INFINITE 0

200 51.560 7.979 94.950 55.055 -5.217 121.035 200

298.15 54.440 13.196 116.139 71.879 0.0000.101 116.139116.140 298.15300

300 54.511 13.297 116.476 72,153

CP 386.75 61.519 18.284 151.041 83.764 5.088 117.884 586.75

...................... ;7........ ...... ...... .....;[;7;;; ....... , 3s6 75 79.555 _ _? ,_'._ _ 716 2_.808 119.706 _9_

- 600 79.555 _'_ _'9_ 106"059 29.763 132.451 _UU

500 79.555 _L._v _ •

600 79.555 50.915 206._82 121.624 57.719 143.618

700 79.555 58.570 218.745 134.6_5 45.674 153.497

800 79,555 66.826 229.368 145.836 53.6_0 162._31

900 79.555 74.781 258.739 155.649 61.585 170.311

1000 79.555 82,737 247.121 164.384 69.541 177.580

Ii00 79.555 90.692 254.703 172.256 77.496 184.252

1200 79.555 98.648 261.625 179.619 85.452 190.416

1300 79.555 106.603 267.993 185.991 93._07 196.141

1600 79.555 114.559 273.889 192.061 I01.363 201.687

1500 79.555 122.516 279.377 197.701 109.318 206.699

1600 79.555 130.470 284.512 202.968 117.274 211.216

1700 79.555 138.425 289.335 207.908 125.229 215.671

1800 79.555 146.381 293.882 212.559 133.185 219.891

1900 79.555 156.336 298.183 216.954 141.140 223.899

2000 79.555 162.292 302.264 221.118 149.096 227.716

2100 79.555 170.247 306.145 225.075 157.051 231.359

2200 79.555 178.203 309.846 228.845 165.007 234.843

2300 79.555 186.158 313.383 232.644 172.962 238.182

2600 79.555 194.11_ 316.769 235.888 180.918 241.386

2500 79.555 202.069 320.016 239.189 158.873 244.467

Z600 79.555 210.025 323.136 2_2.358 196.829 2_7.433

2700 79.555 217.980 326.139 Z45.405 204.78_ 250.293

2800 79.555 225.936 329.032 248.3_i 212,740 255.054

2900 79.555 233.891 331.824 251.172 220.695 255.722

3000 79.555 241.8_7 334.521 253.905 228.651 258.304

3100 79.555 249.802 337.129 256.568 236.606 260.805

3200 79.555 257.758 359.655 259.106 244.562 263.230

3300 79.555 265.713 3_2.103 261.584 252.517 265.583

5600 79.555 273.669 366.478 263.987 260.473 267.869

3500 79.555 281.62_ 346.784 266.320 268.428 270.090

3600 79.555 289.580 349.025 268.587 276.38_ 272.252

3700 79.555 297.535 351.205 270.790 284.339 276.357

3800 79.555 305.491 353.327 272.934 292.295 276.407

3900 79.555 313.446 355.393 275.022 300.250 278.406

6000 79.555 321.402 357.407 277.057 308.206 280.356

4100 79.555 329,357 359.372 279.041 316.161 282.259

6200 79.555 337.313 361.289 280.976 324.117 284.118

4300 79.555 345.268 363,161 282.866 332.072 285.935

4_00 79.555 353.22_ 366.990 284.712 340.028 287.711

4500 79.555 361.179 366.778 286.515 347.983 289.448

4600 79.555 369.135 368,526 288.279 355.939 291.1_8

_700 79.555 377.090 370.237 290.005 363.894 292.813

6800 79.555 385.046 371.912 291.694 371.850 294.443

6900 79.555 393.001 573.552 293.348 379.805 296.041

5000 79.555 400.957 375.159 294.968 387.761 297.607

5100 79.555 408.912 376.735 296,556 395.716 299,143

5200 79,555 416.868 378.280 298.113 603.672 300.651

5300 79.555 624.823 379.795 299.640 411.627 302.130

5600 79.555 432.779 381.282 301.138 419.583 303.552

5500 79.555 440.73_ 382.762 302.608 4Z7.538 305.008

5600 79.555 _48,690 384.175 30_.05Z 635.494 306.409

5700 79.555 456.645 385.583 305.470 _43.449 307.785

5800 79.555 464.601 386.967 306.863 451.405 309.139

5900 79.555 472.556 388.327 308.253 459.360 510.469

6000 79.555 480.512 389.664 309.579 467.316 311.778

600

700

800

900

I000

II00

1200

1300

1400

1500

1600

I700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

_300

6_00

6500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV 1

171
TABLE IX_5. • THERMODYNAMIC FUNCTIONS FROM COEFRCIENTS FOR _,

T C o NO(T)'H*_) S=(T) _G°('r)'H*_)} _ H°("T) _°03rr T

K J/m_.K IcJ/mol J/m_-K JhnoI.K _/moJ J_ol-K K

0 0.000 0.000 0.000 0.000 -7,088 INFINITE 0

200 26.820 4.324 53,469 31.847 -2.764 67,287 200

298.15 29.600 7.088 64.680 40.907 0.000 64.680 298.15

500 29.688 7,1_3 64.863 41.054 0.055 64.681 300

cr 336.86 32,129 8.278 68.429 43.855 1.190 64.897 336.86

...... ;;7;;;...... ;77777...... ;77777....... 7777i...... ;;S;; ....... 1 7777

400 31.544 12.609 80.790 49.268 5,521 66,988 400 5O0

6O0

7OO

8O0

900

1000

1100

12o0

1300

i_00

1500

1600

1700

1800

1900

2000

2100

2200

30.733

30.154

29.848

29.836

30.128

30.729

31.642

32.868

34.410

36.267

38.440

_0.929

43.734

_6.856

50.294

54.050

58.122

62.512

15.721 87.738 56.296 8.633

18.763 93.286 62.014 11.675

21.761 97.908 66,821 14.673

24.743 101.889 70.961 17.655

27.738 105._17 74.597 20.650

30.779 108.620 77.841 23.691

33.895 111.589 80.776 26.807

37.118 114.395 83.461 30.030

_0.479 117.082 85.945 33.391

_4.010 119.698 88.263 36.922

47.743 122.273 90._44 40.655

51.709 124.831 92.514 4q.621

55.939 127.395 94.490 48.851

60,_66 129.982 96.390 53.378

65.32l 132.606 98.227 58.233

70.535 135.280 100.012 63,447

76.141 138.014 101.756 69.053

82,170 140.818 103.468 75.082

70.472 500

73.827 600

76.9_6 700

79.821 800

82._72 900

84.929 1000

87.219 II00

89.368 1200

91.397 1300

93.325 1400

95.170 1500

96.944 1600

98.659 1700

100.328 1800

101.957 1900

103.556 2000

105.132 2100

106.690 2200

172 NASA/TP-3287/REV 1
TABLEtX.26. -THERMODYNAMIC FUNCTIONS FROMCOEFF_.AENTS FORKr

T C ° H°(T)'H°(0) S°(T) _G°(T)'H°_)}K H°(T) _°(T)K

K J_ kJ_m_ J/moI-K Jlmo|-K _lm_ ._mol-K

0 0.000 0,000 0.000 0.000 -6.197 INFINITE

200 20.786 4.157 155.787 135.001 -2.040 165.988

298.15 20.786 6.197 164.086 145.300 0.000 164.086

300 20.786 6.236 164.215 143.429 0.038 164.087

400 20.786 8.315 170.195 149.409 2.117 164.902

500 20,786 10.393 174.833 154.047 4.196 166.442

600 20.786 12.472 178.625 157.837 6.274 168.166

700 20.786 14.550 181.827 161.041 8.355 169.894

BOO 20.786 16.629 184.605 163.817 10.432 171.563

900 20.786 18.708 187.051 166.265 12.510 173.151

i000 20.786 20.786 189.241 168.455 14.589 174.652

1100 20.786 22.865 191.222 170.436 16.667 176.070

1200 20.786 24.944 195.031 172.245 18.746 177,409

1500 20.786 27.022 194.695 175.908 20.825 178.676

1400 20.786 29.101 196.235 175.449 22.903 179.876

1500 20,786 51.179 197.669 176.885 24.982 181.015

1600 20.786 33.258 199.011 178.224 27.061 182.098

1700 20.786 35.357 200.271 179.485 29.139 183.130

IS00 20.786 37.415 201.459 180.673 31.218 184.116

1900 20.786 39,494 202.585 181.797 33.296 185.058

2000 20.786 41.575 205.649 182.863 35.375 185.962

2100 20.786 _3.651 204.665 183.877 37.454 186.828

2200 20.786 45.730 205.630 184.844 39.532 187.661

2300 20.786 47,808 206.554 185.768 41.611 188.462

2_00 20.786 49.887 207.459 186.653 43,690 189.235

2500 20.786 51.966 208.287 187.501 45.768 189.980

2600 20.786 54,044 209.103 188.316 47.847 190.700

2700 20.786 56.123 Z09,887 189.101 49.926 191.396

2800 20.786 98.202 210.643 189.857 52.004 192.070

2900 20.786 60.280 211,372 190.586 54.083 192.723

3000 Z0.786 62.359 212.077 191.291 56.161 193.357

3100 20,786 64.457 212.759 191.972 58.240 193.972

3200 20.786 66,516 213.419 192.632 60.319 194,569

3300 20.786 68,595 214.058 193.272 62.397 195.150

3400 20,786 70.673 214,679 193.893 64.476 195.715

3500 20.786 72.752 215.281 194.495 66.555 196.266

3600 20.786 74.831 215.867 195.081 68.633 196.802

3700 20.786 76.909 216.436 195.650 70,712 197.325

3800 20.786 78.988 216.991 196.205 72.790 197.835

3900 20.786 81.066 217.531 196.744 74.869 198.334

4000 20.786 83.145 218.057 197.271 76.948 198.820

4100 20.786 85,224 218,570 197.784 79,026 199.296

4200 20.786 87.302 219.071 198.285 81.105 199.760

4300 20.786, 89.381 219,560 198.774 83.184 200.215

4400 20.786' 91,460 220.038 199,252 85.262 200.660

4500 20.786 93.538 220.505 199.719 87,341 201.096

4600 20.786 95.617 220.962 200.176 89.419 201.523

4700 20.786 97.695 221.409 200.623 91.498 201.942

4800 20.786 99.774 221.847 201.061 93.577 202.352

4900 20.786 101.853 222.275 Z01.489 95.655 202.754

5000 20.786 105.931 222.695 201.909 97.734 205.149

5100 20.786 106.010 223.107 ZOZ.3Z1 99.813 203.536

5200 20.1786 108.089 223.511 202.724 101.891 203.916

5300 20.786 110.167 223.907 203.120 103.970 204,290

5400 20.786 112.246 224,295 203,509 106.048 204.656

5500 20.786 114.325 224.676 205.896 I08,127 205.017

5600 20.786 116.605 225.051 204.265 110.206 205.371

5700 20.786 118._82 225.419 204.633 112.284 205.720

5800 20.786 120.560 225.780 Z04.994 114.363 206.065

5900 20.786 122.639 226.136 205.349 116.442 206.400

6000 20.786 124,718 226.485 205.699 118.520 206.732

6200 20.913 128.890 227.169 206.380 122,692 207.380

6400 20.940 133.076 227.834 207.041 126.879 208.009

6600 20.909 137.262 228.478 207.680 131.064 208.619

6800 20.850 141.438 229.101 208.301 135.241 209.213

7000 20.782 145.601 229.70_ 208.904 139.404 209.790

7200 20.719 149.751 230.289 209.490 1_5.554 210,351

7400 20.667 153.890 230.856 210.060 147.692 210.898

7600 20.632 158.019 231._07 210.615 151.822 211.430

7800 20.614 162.144 231.942 211.155 155.946 211.949

8000 20.613 166.266 232.464 211.681 160,068 212.456

T

K

0

200

298.15

3O0

400

500

600

700

800

900

I000

1100

1200

1500

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

5300

3_00

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

_500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV 1

173
TABLE IX,26, - Concluded.

T Cp° HoF).HO(0) SO(t_) _G°(T)'H°(0)} K

K Jlmot-K kJ/mo_ Jlmoi-K JlmoI-K

8200 20.628 170,390 232.973 212,194

8400 20.658 174.518 233.471 212.695

8600 20.701 178.654 233.957 213.]84

8800 20.753 182.799 234.434 213.661

9000 20.813 186.956 254.901 214.128

9200 20.880 191.125 235.359 21_.584

9400 20.952 195.308 235.809 215.031

9600 21.028 199.506 236.251 215._69

9800 21.107 203.720 236.685 215.897

i0000 21.189 207.949 237.112 216.317

10500 21.411 218.598 238.151 217.333

II000 21.667 229.366 239.153 218.302

11500 21.982 240.275 240.123 219.230

12000 22.390 251.363 241.067 220.120

12500 22.927 262,686 241.991 220.976

13000 23.631 274.318 242.903 221.802

13500 24.538 286.351 243.812 222.600

14000 25.676 298.894 244.724 223.374

14500 27.067 312.069 245.648 224.126

15000 28.720 326.005 246.593 224.859

15500 30.634 340.833 247.565 225.576

16000 32.790 356.679 248,571 226.279

16500 35.156 373.658 249.616 226.970

17000 37.680 391,862 250.703 227,652

17500 40,293 411.353 251.833 228.327

18000 42.905 452.155 253.004 228.996

18500 45.407 454.240 254.214 229,661

19000 47.666 477.521 255.456 230.323

19500 49.531 501.840 256.719 230.984

20000 50.825 526.957 257.991 231.643

H*(T)

kJ/rnol

164.192

168.321

172.457

176.602

180.758

184.928

189.111

193.309

197.522

201.752

212.401

223.168

234.077

245.166

256.489

268.121

280.154

292.697

305.872

319.807

334.635

350.482

367.461

385.665

405.156

425.957

448.042

471.324

495.6_3

520.760

-Go('r)K

JlmoI-K

212,950

213.432

213.904

214.365

21_.817

215.258

215.691

216.114

216.530

216.937

217.925

218.865

219.768

220.636

221._72

222.279

223.059

223.817

22_.554

225.273

225.976

226.666

227.3_6

228.017

228.681

229.340

229.996

230.650

231.302

231,953

T

K

8200

8_00

8600

8800

9000

9200

9_00

9600

9800

1000o

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

ZOO00

! 74 NASA/TP-3287/REV l
TABLE IX.27. - THERMODYNAMIC FUNCTIONS FROM COEFRCIENTS FOR U(_,0

T C o HO(T).Ho(O) SO(T) _GO(T).Ho(O)}K HO(T) _o(I')K T

K JIm_l-K _lmol _moI-K JlmoI.K _ol J/mol_ K

0 0.000 0,000 0,000 0.000 -6.63Z INFINITE 0

200 21.552 2.343 19.853 8.136 -2.289 31.296 200

298,15 26.860 6.632 29,120 13.586 0.000 29.120 298.15

300 26.881 6,678 29,276 13 '680 0.046 29.120 300 600

.586 7 280 36 742 18 541 2.648 3_.121

600 27 " ' ' 6 87 31 119 453 69

cr 653.69 29.769 8.819 40.367 20.910 .I .... _............. ___

....................................................................... 653.69

# 453.69 30.375 11.819 66.960 20.910 7 187 31.119

500 50.071 13.Z1B 69.897 23.661 8 586 32.725 500

600 29.584 16.199 55.336 28._35 II 567 36.055 600

700 29.268 19.160 59.867 52.525 16 508 39.142 700

800 29.017 22.052 63.757 56.191 17 620 61.981 800

900 28,870 26.946 67.165 39.447 20,316 66.594 900

i000 28.795 27.829 70,202 42.374 23.197 47.006 1000

1100 28.785 30.707 72.946 45.030 26.075 49.241 1100

1200 28.836 33.588 75.452 47.462 28.956 51.522 1200

1300 28.945 36.476 77.766 69,706 31.866 55.269 1500

1600 29.111 59.379 79,915 51.787 36.747 55.096 1600

1500 29.354 42.300 81.93i 53.730 37.668 56.818 1500

1600 29.611 65.267 83.832 55.553 40.615 58.468 1600

1700 29.962 48.224 85.637 57.270 45.592 59.995 1700

1800 30.328 51.237 87.359 58.89_ 46.605 61.667 1800

1900 30.767 56,292 89.011 60.636 49.660 62.874 1900

2000 31.260 57.393 90.601 61.905 52.761 66.221 2000

2100 31.806 60.566 92.139 63.508 55.914 65.514 2100

2200 32.606 63.756 93.633 64.653 59,126 66.75g 2200

2300 53.058 67.0Z8 95.087 65.946 62.596 67.95B 23_0

2600 33.764 70.369 96.509 67.188 65.737 69.118 2600

2500 56.522 73.785 97.902 68.389 69.151 70.242 2500

2600 35.336 77.275 99.272 69.551 72.665 71.532 2600

2700 36,198 80.851 100.622 70.677 76.219 72.592 2700

2800 37.115 86,517 101,954 71.770 79.885 73,424 2800

2900 38.086 88.276 103.276 72.834 83.664 74.431 2900

3000 39.107 92.135 104.582 73.870 87.503 75.414 3000

175

NASA/TP-3287/REV 1
TABLE IX.28. - THERMODYNAMIC FUNCTIONS FROM COEFRCIENTS FOR Mg(cr, f)

T C ° H°(T)'H°(_ 8°C1") _G°(T)-H°_)}K H°(1") _°(T)K T

K J/m_-K kJh_ol _moI-K _moI-K _/mol J/moI-K K

0 0.000 0.000 0.000 0,000 -4.979 INFINITE 0

ZOO 22.649 2.639 23.041 9.848 -2.341 34.744 200

298.15 24.775 4.979 32.535 15.835 0.000 32.535 298.15

300 24.862 5.025 32.689 15.938 0.046 32.536 300

400 26.234 7.586 40.047 21.082 2.607 33.530 400

500 27.218 10.260 46.009 25.489 5.281 35.448 500

600 28,192 13.030 51.057 29.340 8.051 37.639 600

700 29.284 15.902 55.483 32.765 10.923 39.878 700

800 30.548 18.892 59.473 35.858 13.913 42.082 800

900 32.010 22.018 63.154 38.689 17.039 44.221 900

cr 923 32.376 22.759 63.966 39.308 17.780 44.703 923

t 923 34.300 31.159 73.067 39.308 26.180 44.703 923

1000 34.300 33.800 75.815 42.015 28.821 46.994 1000

1100 34.300 37.230 79.084 45.239 32.251 _9.765 1100

1200 34.300 40.660 82.069 48.185 35.681 52.335 1200

1300 34.300 44.090 84.814 50.899 39.111 54.729 1300

1400 34.300 47.520 87.356 53.413 42.541 56.970 1400

1500 34.300 50.950 89.723 55.756 45.971 59.075 1500

1600 34.300 54.380 91.936 57.949 49.401 61.061 1600

1700 34.300 57.810 94.016 60.010 52.831 62.939 1700

1800 34.300 61,240 95.976 61.954 56.261 64.720 1800

1900 34.300 64.670 97.831 63.794 59.691 66.414 1900

2000 34.300 68.100 99.590 65.540 63.121 68.030 2000

2100 34.300 71.530 101.264 67.202 66.551 69.573 2100

2200 34.300 74.960 102.859 68.786 69.981 71.050 2200

2300 34.300 78.390 104.384 70.301 73.411 72.466 2300

2400 34.300 81.820 105.844 71.752 76.841 73.827 2400

2500 34.300 85.250 107.244 73.144 80,271 75.136 2500

2600 34.300 88.680 108,589 74.481 83.701 76.396 2600

1700 34.300 92,110 109.884 75.769 87.131 77.613 2700

2800 34.300 95.540 111.131 77.010 90.561 78.788 2800

2900 34.300 98.970 112.335 78.207 93.991 79.924 2900

3000 34.300 102.400 113.497 79.364 97.421 81.024 3000

3100 34.300 105.830 114.622 80.483 100.851 82.090 3100

3200 34.300 109.260 115.711 81.567 104.281 83.123 3200

3300 34.300 112.690 116.767 82,618 107.711 84.127 3300

3400 34.300 116.120 117.791 83,638 111.141 85.102 3400

3500 34.300 119.550 118.785 84.628 114.571 86.050 3500

3600 34.300 122.980 119.751 85.590 118.001 86.973 3600

3700 34.300 126.410 120.691 86.526 121.431 87.872 3700

3800 34.300 129.840 121.606 87.437 124.861 88.747 3800

3900 34.300 133.270 " 122.497 88.325 128.291 89.601 3900

4000 34.300 136.700 123.365 89.190 131.721 90.435 4000

4100 34.300 140.130 124.212 90.034 135.151 91.248 4100

4200 34.300 143.560 125.038 90.858 138.581 92.043 4200

4300 34.300 146.990 125.846 91.662 142.011 92.820 4300

4400 34.300 150.420 126.634 92.448 145.441 93.579 4400

4500 34.300 153.850 127.405 93,216 148.871 94.323 4500

4600 34.300 157.280 128.159 93.967 152.301 95.050 4600

4700 34.300 160.710 128.896 94.703 155.731 95,762 4700

4800 34.300 164.140 129.619 95.423 159.161 96.460 4800

4900 34.300 167.570 130.326 96.128 162.591 97.144 4900

5000 34.300 171.000 131.019 96.819 166.021 97.815 5000

5100 34,300 174.430 131.698 97,496 169.451 98.472 5100

5200 34,300 177.860 132.364 98.160 172.881 99.118 5200

5300 34.300 181.290 133.017 98.812 176.311 99.751 5300

5400 34.300 184.720 133.659 99.451 179.741 100.373 5400

5500 34.300 188.150 134.288 100.079 183.171 100.984 5500

5600 34.300 191.580 134.906 100.695 186.601 101.584 5600

5700 34.300 195.010 135.513 101.301 190,031 102.174 5700

5800 34.300 198.440 136.110 101.896 193.461 102,754 5800

5900 34.300 201.870 136.696 102.481 196.891 103.325 5900

6000 34.300 205.300 137.272 103.056 200.321 103.886 6000

176 NASA/TP-3287/REV l
TABLE IX.20. - THERMODY/'C_M/C:FUNCTIONS FROM COEFFICIENTS FOR Mn(a,,_,,./,6,/)

T C o Ho(-T).Ho(o_ So(T) _GO(T).Ho(O}y'r HoG) _o('r)rr 7

K _m_l-K _/mol JknoI-K J/moFK k,J/mol J_oI-K K

0 0.000 0.000 0.000 0.000 -4.996 INFINITE 0

200 25.048 2.557 22.140 9.554 -2.457 36.324 Z00

298.15 26.299 4.994 32.010 15.260 0.000 52.010 298.15

300 26.346 5.043 32.173 15.364 0.049 32,011 300

400 28.550 7,792 40.068 20.587 2.798 33.072 400

500 30.354 10.760 46.637 25.158 5.746 35.146 500

600 31.959 13.856 52.315 29.221 8.862 37.5_5 600

700 33.458 17.128 57.355 32.887 12.134 40.021 700

800 34.911 20.547 61.918 36.235 15.553 42.677 800

900 36.368 24.110 66.114 39.325 19.116 44.874 900

980 57.566 27,067 69.261 41.661 22.075 46.737 980

980 57.572 29,295 71.532 41.641 24.299 46,737 980

1000 37.699 30.046 72.293 42,247 25.052 47.241 1000

1100 38.142 33.840 75.908 45.165 28.846 49.685 1100

1200 38.533 37.673 79.243 47.849 32.679 52.011 1200

1300 38.965 ql.548 82.345 50.385 36.554 54.226 1300

1361 39.202 43.932 84.137 51.858 38.938 55.527 1361

7 1361 43.095 46.054 85.696 51.858 41.060 55.327 1361

1600 43.433 _7.742 86.919 52.817 42.748 56.384 1400

1412 _3.513 43.264 87.290 5_.109 43.270 56.645 1412

............................................................................................

1412 65.229 50.143 88.620 53.109 45.149 56.645 1412

1500 65,988 54.159 91.380 55.274 49,165 58.603 1500

6 1519 46.105 55.03_ 91.959 55.729 50.040 59.016 1519

1519

1600

1700

1300

1900

2000

2100

2200

2300

2600

2500

2600

2700

2800

2900

3000

5100

3200

3300

3_00

3500

3600

3700

3800

3900

6000

4100

4200

_300

4500

_600

6700

4B00

6900

5000

5100

5200

5300

5400

5500

56_0

5700

5800

5900

6000

46 024

46 024

46 024

46 024

46 024

46 024

46.024

46.026

46.024

46.024

46.024

46.024

66.024

_6.024

46.024

46.024

46.024

46,024

46.024

46.024

66,024

46,024

_6.024

46.024

_6.024

46.026

46.024

46.024

46.024

46.024

66,024

46.024

46,024

46,026

46.024

46.024

46.026

46.024

46.026

46.026

46.024

46.026

66.026

66.024

46.024

46.024

67.092 99.897 55.729 62.098 59.016 1519

70.820 102.288 58.026 65.826 61.147 1600

75.422 105.078 60.712 70.428 63.650 1700

80.025 107.709 63.251 75.031 66.025 1800

84.627 IID.198 65.657 79.633 68.2_5 IgO0

89.229 112.558 67.964 86.235 70.441 2000

93.832 114.804 70,122 88.838 72.500 2100

98.434 116.965 72.202 93.440 74.472 2200

103.037 118.991 74.192 98.043 76.363 2300

107.639 120.949 76.100 102.645 78.181 2400

112.241 122.828 77.932 107.247 79.929 2500

116.844 124.633 79.693 111.850 81.614 2600

121.446 126.370 81.390 116.452 83.240 2700

126.049 128.044 83.027 121.055 8_.810 2800

130.651 129.659 84.607 125.657 86.329 2900

135.253 131.219 86.135 130.259 87.B00 3000

139,856 132.729 87.614 134.862 89.225 3100

144.458 136.190 89.046 139.664 90.607 3200

149.061 135.606 90.436 164.067 91.949 3300

153.663 136.980 91.785 148.669 93.25_ 3400

158.265 138.314 93.095 153,271 94.522 3500

162.868 139.611 94.369 157.874 95.757 3600

167.470 140.872 95.609 162.476 96.959 3700

172.073 142.099 96.817 167.079 98.131 3800

176.675 163.296 97.993 171.681 99.274 3900

181.277 166.460 99.140 176.283 100.389 4000

185.880 145.596 100.260 180.886 101.478 4100

190.482 146.705 101.352 185.488 102.541 4200

195.085 147.788 102.420 190.091 103.581 4300

199.687 148.846 103.463 194.693 104.598 4400

204.289 149.881 104.483 199.295 105.593 4500

208.892 150.892 103.481 203.898 106.566 4600

213.494 151.882 106.658 208.500 107.520 4700

218.097 152.851 107.416 213.103 108.454 4800

222.699 153.800 108.351 217.705 109.370 _900

227.301 154.730 109.269 222.307 110.268 5000

231.904 155.641 110.170 226.910 111.149 5100

236.506 156.535 111.053 231.512 112.013 5200

241.109 157.411 111.919 236.115 112.861 5300

245.711 158.272 112.770 240.717 113.694 5400

250.313 159.116 113.605 245.319 114.513 5500

256.916 159.9_5 I14,425 2q9.922 115.317 56_0

259,518 160.760 I15.231 25_,524 116.107 5700

264.121 161.561 116.022 259.127 116.883 5800

268.723 162.347 116.801 263.729 117.647 5900

273.325 163.121 117.567 268.331 118.399 6000

NASA/TP-3287/REV l 177
T C °

K JIm_-K

0 0.000

200 21.507

298.15 23.935

300 23.960

600 25.076

500 25.852

600 26.463

700 26.975

800 27._38

900 27.892

1000 28.369

1100 28.900

1200 29.487

1300 30.141

1400 30.861

1500 31.647

1600 32.500

1700 33.422

1800 34.417

1900 35.491

2000 36.650

2100 37.899

2200 39.240

2300 _0.674

2400 42.171

2500 43.883

2600 65.934

2700 48.426

TABLE IX.30. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR

H°(T)-H°(_ S°(T) _G°(T).H°_)}_ H°(T)

_/mol J/mol-K J/moI-K _hn_

0.000 0.000 0.000 -4.585

2.333 19.476 7.810 -2.252

4.585 28,605 13.227 0.000

4.629 28.755 13.322 O.OG4

7,085 35.812 18.098 2.500

9,634 41.494 22.227 5.049

12.251 46.264 25.846 7.666

14,923 50,382 29.064 10.338

17.644 54.015 31.960 13.059

20.410 57.273 34.595 15.825

23.223 60.236 37,015 18.638

26.086 62.964 39.250 21.501

29,005 65.504 41.333 24.620

31.986 67.889 63.285 27.401

35.035 70.149 45.124 30.450

38.i60 72.305 46.864 33.575

41.367 74.374 48.520 36.782

64.663 76.372 50.099 40.078

48.054 78.310 51.613 43.669

51.549 80.199 53.068 46.966

55.155 82.048 54.671 50.570

58.882 83.867 55.828 56.297

62.738 85.660 57.143 58.153

66.734 87.436 58.421 62.149

70.875 89.198 59.667 66.290

75.175 90.954 60.884 70.590

79.663 92.715 62.074 75.078

84.377 94.492 63.242 79.792

Mo(cr,_

_O(T)/T T

J/moI-K K

INFINITE 0

30,735 200

28.605 298.15

28.605 300

29.560 400

31.397 500

33.688 600

35.616 700

37.691 800

39.689 900

61.598 1000

43.418 I100

45.154 1200

66.812 1500

68.399 1600

_9.921 1500

51.385 1600

52.796 1700

56.160 1800

55,_81 !900

56.764 2000

58.011 2100

59.227 2200

60.415 2300

61,578 2400

62.718 2500

63.857 2600

64.940 2700

2800 51.460 89.565 96.306 60.390 84.780 66.027 2800

cr2896 54.890 96.465 98.096 65.477 89.880 67.061 2896

...........................................................................................

2896 37.656 130.447 110.521 65.477 125.862 67.061 2896

2900 37.656 130.597 110.573 65.540 126.012 67.121 2900

3000 37.656

3100 37.656

3200 37.656

3300 37.656

3400 37.656

3500 37.656

3600 37,656

3700 37.656

5800 37.656

3900 37.656

4000 37.656

4100 37.656

4200 37.656

4300 _7.656

6400 37.656

4500 37.656

4600 37.656

4700 37.656

6800 37.656

4900 37.656

SO00 37.656

5100 37.656

5200 37.656

5300 37.656

5400 37.656

5500 37.656

5600 37.656

5700 37.656

5800 37.656

5900 37.656

6000 37.656

134.365 111.850 67.062 129.778 68.590 3000

138.128 113.084 68.527 133.543 70.006 3100

141.894 116.280 69.938 137.309 71.371 3200

145.660 115.439 71.299 141.075 72.689 3300

149.425 116.563 72.614 146.840 73.963 3400

153.191 117.654 73.886 148.606 75.196 3500

156.956 118.715 75.116 152.371 76.390 3600

160.722 119.747 76.309 156.157 77.548 5700

166.488 120.751 77.465 159.903 78.672 3800

168,253 121.729 78.587 163.668 79.765 3900

172.019 122.683 79,678 167.434 80.824 4000

175.784 123.612 80.738 171,199 81.857 4100

179,550 126.520 81.770 174.965 82.862 4200

183.316 125.606 82.774 178.731 83.841 4300

187.081 126.272 83.753 182.496 84.795 4400

190.847 127.118 84.707 186.262 85.726 4500

194.612 127.946 85.638 190,027 86.635 4600

198.378 128.755 86.5_7 193.793 87.523 4700

202.164 129.548 87.435 197.559 88.390 4800

205.909 130.325 88.302 201,324 89.238 4900

209.675 131.085 89.150 205.090 90.067 5000

213.440 131.831 89.980 208.855 90.879 5100

217.206 132.562 90,792 212.621 91.676 5200

220.972 135.280 91.587 216.387 92.452 5300

226.737 135.985 92.365 220.152 93.214 5600

228.503 136.674 95.128 223.918 93,962 5500

252.268 135.555 93.876 227,683 94.695 5600

236.034 136.019 96.610 231.449 95.414 5700

239.800 136.674 95.329 235.215 96.120 5800

263.565 137.318 96.036 238.980 96.813 5900

247.331 137.951 96.729 242.746 97.495 6000

178 NASA/TP-3287/REV l
TABLE IX,31. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR N2

T C_ HO(T_HO(_ SO(T) qG°(T).HO(O)}K Ho0] _°(Drr

K J_ol-K _hn_ J_oI-K JlmoI-K kJ/m_ J_oI-K

0 0.000 0.000 0.000 0,000 -8.670 INFINITE

200 29.107 5.813 179.986 150.922 -2.857 ]94.273

250 29,110 7.268 186.481 157.409 -1.402 ]92.089

298.15 29.124 8.670 191.610 162.530 0.000 191.610

300 29.125 8.724 191.790 162.710 0.054 191.610

550 29.165 10.181 196.282 167.193 1.511 191.965

400 29.249 11.641 200.181 171.078 2.971 192.754

500 29-582 14.581 206.740 177.578 5,911 194.918

600 30.I09 17.564 212.177 182.904 8.894 197.354

700 30.754 20.607 216.866 187.428 11.937 199.814

800 51.434 23.716 221.017 191.37_ 15.046 202.210

900 32.090 26.893 224.758 194,877 18.223 204.511

lO00 32.696 30.152 228,171 198.038 21.462 206,708

llO0 33.242 33.430 231.313 200.922 24.760 208.804

i200 33.724 36.779 234.227 203.578 28.109 210.803

1300 34.147 40.173 236.943 206.041 31.505 212,718

1400 34.518 43.606 259.488 208.340 34.956 214.533

1500 34.842 47.075 241.880 210.497 38.405 216,277

1600 35.127 50.573 244.]38 212.550 41.903 217,949

1700 35.377 54.099 246.276 214.453 45.429 219,553

1800 35.599 57.648 248.304 216.277 48,978 221.094

1900 35.795 61.218 250.234 218.019 52.548 222,577

2000 35.970 64.806 252.075 219.672 56.136 224.007

2100 56.127 68.411 253.834 221.257 59.741 225.385

2200 56.267 72.031 255.517 222.776 63.361 226.717

2300 36.395 75.664 257.132 224.235 66.994 228.005

2400 36.510 79.310 258.684 225.638 70.639 229.251

2500 36.615 82.966 260.176 226.990 74.296 250.458

2600 36.711 86.632 261.614 228.294 77,962 231,629

2700 36.800 90.308 263,002 229.554 81,638 232,765

2800 36.881 93.992 264.341 230.773 85.322 233.869

2900 36.957 97.684 265.637 231.953 89.014 234.943

3000 37.027 101,385 266.891 235,097 92.713 235,987

3100 57.093 105.089 268.106 234.206 96.419 237,003

3200 37.155 108.802 269.285 235.284 100.151 237.994

3300 37.213 112.520 270.429 236.532 103.850 238.959

3400 37.265 116.244 271.541 237.351 107.574 239.901

5500 37.320 119.974 272.622 238.344 111.503 240.821

3600 37.370 125.708 275.674 239.511 115.058 241.719

3700 37.417 127.447 274.698 240.253 118.777 242.597

3800 37.46Z 131,191 275.697 241.173 122.521 243.454

3900 37.506 134.940 276.671 242.071 126.270 244.294

4000 37.548 158.692 277.621 242.948 130.022 245.115

4100 37.589 142.449 278.548 245.805 133.779 245.919

4200 37.629 146,210 279.455 244.643 137.540 246.707

_300 37.667 149.975 280.340 245.463 141.305 247.479

4400 37.706 153,744 281.207 246.265 145.074 248.236

4500 37,743 157.516 282,055 247.051 148,846 248,978

4600 37.781 161.292 282.885 247.821 152.622 249.706

4700 37.818 165.072 283.698 248.576 156,402 250.420

4800 37.856 168.856 Z84.494 249.316 160.186 251.122

4900 37,893 172.645 285.275 250.042 163.973 251,811

5000 37.932 176.435 286.041 250.754 167.764 252.488

5100 37.971 180.250 286.793 251.453 171.560 255.153

5200 38.011 184.029 287.530 252.140 175.359 253.807

5300 58.053 187.852 288.255 252.815 179.162 254.451

5400 38.096 191.639 288,966 253.478 182.969 255.083

5500 38,141 195.451 289.666 254.129 186.781 255.706

5600 38.189 199,268 290.354 254.770 190,598 256.318

5700 38.238 203,089 291,030 255.400 194.419 256.921

5800 38.291 206.916 291.695 256.020 198.245 257.515

5900 38.547 210,747 292.350 256.630 202.077 258,100

6000 38.406 214.585 292.995 257.231 205.915 258.676

6200 38.560 222.282 294.257 258.405 213.612 259.804

6400 38.719 230.009 295.484 259.545 221.339 260.900

6600 38.887 237.770 296.678 260.652 229.100 261.966

6800 39.069 245.565 297.841 261.729 236.895 263.004

7000 59.270 253.399 298.977 262.777 2_4.729 264.016

7200 39.497 261.275 300.086 263.798 252.605 265.002

7400 39.755 269.199 S01.172 264,794 260.529 265.965

7600 40,044 277.178 302.236 265.765 268.508 266.906

7800 40.372 285.219 305.280 266.713 276.549 267.825

8000 40,741 293.330 304,307 267.640 284.660 268,724

T

K

o

200

250

298.15

300

350

400

50O

600

70O

800

900

I000

1100

1200

1500

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

$400

3500

3600

3700

3800

3900

4000

_10o

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV 1 179
TABLE IX,31. • Concluded,

T ¢o H°(T)'H°(O) S°(T) "(G°(r)-H°(O))n H°(r) _°(r)R

K _m_l-K kJ/mol d/moI-K J_oI-K _ J_oI-K

8200 41.153 301.519 305.318 268.547 292.849 269.604

8400 41.608 309.794 306.315 269.435 301.124 270.467

8600 42.108 318,165 307,300 270.304 309.495 271,312

8800 42.652 326.640 308.27_ 271.156 317.970 272.141

9000 43.240 335.229 309.239 271.991 326.559 272.955

9200 43.871 343.939 310.196 272.811 335.269 273.754

9400 44.543 352.780 311.147 273.617 344.110 274.539

9600 45.253 361.759 312.092 274.409 353.089 275.312

9800 46.000 370.884 313.033 275.187 362.213 276.072

10000 46.779 380.161 313.970 275.954 371.491 276.821

10500 48.851 404.062 316.301 277.819 595.392 278.6_5

11000 51.051 429.034 318,624 279.621 420,363 280.410

11500 53.315 455.124 320.944 281.368 446.454 282.122

12000 55.576 482,348 323.261 283.065 473.678 283.787

12500 57.769 510.688 325.574 284.719 502.018 285,413

13000 59.830 540.095 327.880 286.555 531.425 287.002

13500 61.702 570.487 330.174 287.916 561.817 288.558

14000 63.334 601.757 332.449 289.466 593.087 290.085

14500 64.683 633.773 334.695 290.987 625.103 291.585

15000 65.717 666.387 336.907 292.481 657.717 293.059

15500 66.415 699.434 339.074 293.949 690.764 294.508

16000 66.767 732.744 341.189 295.392 7Z4.074 295.934

16500 66.778 766.144 343.244 296.811 757.474 297.337

17000 66.462 799.467 345.234 298.206 790.797 298.717

17500 65.851 832.557 347.152 299.578 823.887 300.073

18000 64.991 865.277 3_8.996 300.925 856.607 301.407

18500 63.940 897.516 350.763 302.248 888.846 302.717

19000 62.773 929.197 352.452 303.547 920.527 304.004

19500 61.582 960.285 354.068 304.822 951.615 305.267

20000 60.473 990.793 355.612 306.073 982.123 306.506

T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

II0O0

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

180 NASA/rP-3287/REVl
TABLE IX.32. - THERMODYNAMIC FUNGI'IONS FROM COEFFICIENTS FOR Na(cr,

T C o HO(T).HO(_ SO(T) _Go(-r).l.lO(0)y.r HO(T) _O(T)/T T

K Jhn_-K _/mol J_oI-K J/moI-K _/mol _moI-K K

0 0.000 0.000 0.000 0.000 -6.460 INFINITE 0

200 25.998 3.803 40.519 21.50_ -2.657 53.804 200

298.15 28.230 6.460 51.300 29.653 0.000 51.300 298.15

6.512 51,475 29.767 0.052 51.301 300

.... ;-;7;Z---i;5;; ...... ;;_;;;...... ;;778;- 3_536 _761 51.9_8 _7101 _0 31511 12.159 87.161 36.815 5.679 s2965 400

500 30.626

600 29.900

700 29.342

800 28.966

900 28.781

1000 28.793

Ii0O 29.006

1200 29.421

1300 30.040

I_00 30.863

1500 51.889

1600 33.119

1700 34.553

I_00 36.190

1900 38.031

2000 q0.076

2100 _2.327

2200 4_.782

2300 47.445

15.244 74.095 43.607 8.784 56.527 500

18.269 79.612 49.16_ 11.809 59.950 600

21.230 84.177 53.849 1_.770 65.077 700

24.1_3 88,068 57.889 17.683 65.964 800

27.029 91.667 61.435 20.569 68.613 900

29,906 94._99 64.593 23.466 71,053 1000

52.794 97.251 67.458 26.334 73,311 II00

35.714 99.792 70.030 29.254 75.413 1200

38.685 102.170 72._11 52.225 77.381 1300

41.729 I04._25 74.618 35.269 79.233 1400

_4.865 106.588 76.678 38.405 80.985 1500

48.114 I08.684 78.613 41.654 82.651 1600

51.495 110.73_ 80.442 45.035 84.242 1700

55.051 I12.75_ 82.181 48.571 85.770 1800

58.7_0 114.759 85.843 52.280 87.2_3 1900

62.64_ 116.761 85.439 56.184 88.669 2000

66.762 118.770 86.979 60.302 90.055 2100

71.116 120.795 88.470 64,656 91.406 2200

75.726 122.844 89.919 69.266 92.728 2300

NASA/TP-3287/REV 1 181
T C °

K JI_L-K

0 0.000

200 23.091

298.15 24.694

30O 24.710

600 25.390

500 25.898

600 26.367

700 26.769

600 27.182

900 27.596

1000 27.999

II00 28.405

1200 28.797

1300 29.179

1400 29.590

1500 30.061

1600 50.605

1700 31.222

1800 31.903

1900 32.639

2000 35.430

2100 34.269

2200 35.195

2300 36.193

2600 37.510

2500 38.650

2600 40.252

2700 42.263

cr 2750 45.432

TABLE IX.33. -THERMODYNAMIC FUNCTIONS FROM COEFRCIENT8 FOR NtXcr, t)

H°(T)-H°(O)

0 000

2 879

5 241

5 287

7 794

10 359

12.972

15.628

18.325

21.066

23.844

26.664

29,524

32.423

35.361

38.343

41.376

44.467

47.622

50.849

56.152

57.536

61.009

64.577

68.251

72.046

75.987

80,109

82,251

S°( T) "(G°(T)'H°(O))K H°(T) _°('I')K T

J_-K _m_ _lmol J_oI-K K

0.000 0.000 -5.241 INFINITE 0

26.878 12.480 -2.362 38.685 200

36.464 18.886 0.000 36.464 298.15

36.617 18.996 0.046 36.464 300

43,826 24,360 2.555 37.443 400

49.548 28.829 5.118 39.511 500

56,310 32.690 7.731 qi.425 600

56.403 36.076 10.387 45.565 700

62.005 39.098 13,084 45.649 800

65.230 41.825 15.823 47.669 900

68.158 44.314 18.603 49.555 I000

70.846 46.606 21.423 51.370 1100

73,354 48.731 24.283 53.098 1200

75.654 50.716 27,182 5q,745 1300

77.832 52,574 30.120 56,317 1400

79.889 54.327 33.I02 57.821 1500

81.846 55.986 36.135 59.261 1600

83.719 57,563 39.226 60.645 1700

85.523 59.066 42.381 61.978 1800

87,267 60,505 45.608 63.263 1900

88.961 61.885 48.911 64.506 2000

90.612 63.214 52.295 65.710 2100

92.228 64.496 55.768 66.879 2200

93.814 65.737 59.336 68.015 2300

95.377 66.939 65.010 69.123 2400

96.926 68.108 66.805 70.204 2500

98.472 69.246 70.746 71.262 2600

100.027 70.357 74.868 72.298 2700

100.813 70.906 77.010 72,809 2750

t 2750 33.472 109.154 110.596 70.904 103.913 72.809 2750

2800 33._72 110.828 111.199 71.618 105.587 73.490 2800

2900 33.472 114.175 112.374 73.003 108.934 74.810 2900

3000 33.472 117.522 i13_508 70.33_ 112.281 76.081 3000

5100 33.472 120.869 114.606 75.616 115.628 77.307 3100

3200 33.472 126.217 115.669 76.851 I18,976 78.489 3200

3300 33.472 127.566 116.699 78.043 122.323 79,631 3300

3400 55.472 150.911 117.698 79.195 125,670 80.736 3400

3500 33.472 134.258 118.668 80.309 129,017 81.806 3500

3600 33.472 137.605 I19,611 81.387 132.364 82.845 3600

3700 33.672 140.953 120.528 82.433 I35.712 83.849 3700

3800 33.672 144.300 121.#21 83.447 139.059 84.826 3800

3900 33.472 147.6Q7 122.290 84.432 142.606 85.776 3900

4000 33.472 150.994 125.138 85.389 145.753 86.699 4000

4100 33.472 156.541 123.964 86.520 149.100 87.598 4100

4200 33.472 157.689 124.771 87.226 152.448 88.474 4Pon

4300 35.472 161.036 125.558 88.108 155.795 89,327 4300

4600 35.672 166.383 126.328 88.968 159.142 90.159 6400

6500 33.472 167.730 127.080 89.807 162.489 90.971 6500

6600 33.472 171.077 127.816 90.625 165,836 91,766 4600

4700 33.672 174.425 128.536 91.424 169.184 92.539 4700

4800 33.472 177.772 129.240 92.205 172.531 93.296 4800

_900 33.472 181.119 129.951 92.968 175.878 96.037 4900

5000 35.472 184.466 130.607 93.714 179.225 96.762 5000

5100 33.472 187,813 131.270 96.443 182.572 95.471 5100

5200 33.672 191.161 131.920 95,158 185.920 96.166 5200

5300 33.672 194.508 152.557 95.858 189.267 96.846 5300

5400 33.472 197.855 133.183 96.543 192.616 97.514 5400

5500 35.472 201.202 133.797 97.215 195.961 98.168 5500

5600 33.472 206.549 134.400 97.873 199.508 98.809 5600

5700 33.472 207.897 136.993 98.519 202.656 99.459 5700

5800 33.472 211.244 135,575 99.155 206.003 100.057 5800

5900 53.472 216.591 136.147 99.776 209.550 100.66_ 5900

6000 33._72 217.958 156.709 100.586 212.697 101.260 6000

182 NASA/TP-3287/REV 1
TABLE IX,34. • THERMODYNAMIC; FUNCTIONS FROM COEFFICIENTS FOR Nle

T C o HQ(T).HO_) SO(T) _G°(T)-H°(0)}K Ha("T) "G°CI')K

K J/m_l-K kJ/mol J/moI-K NmoI-K kJ1mol JlmoI-K

0 0.000 O. 000 0. 000 O. 000 -6. 197 INFINITE

200 20.786 4.157 158.030 117.244 -2.060 Iq8.231

298.15 20.786 6.197 166,330 125.543 0.000 146.330

300 20.786 6.236 146.458 125.672 0.038 146.330

400 20.786 8.315 152.458 131.652 2.117 147.145

500 20.786 10.393 157.076 136.290 4.196 148.685

600 20.786 12.672 160.866 140.080 6.274 150.409

700 20.786 14.550 166.070 165.284 8.353 152.138

800 20.786 16.629 166.846 146.060 10.432 153.807

900 20.786 18.708 169.294 148.508 12.510 155.394

I000 20.786 28.786 171.484 150.698 16.589 156.896

II00 20.786 22.865 173.666 152.679 16.667 158.315

1200 20.786 24.944 175.274 154,488 18.746 159.652

1300 20.786 27.022 176.938 156.152 20.825 160.919

]400 20.786 29.101 178.478 157.692 22.903 162.119

1500 20.786 31.179 179.912 159.126 24.982 163.258

1600 20,786 35.258 181.256 160.668 27,061 164,341

1700 20.786 35.337 182.514 161.728 29.139 165.373

1800 20.786 37.415 183.702 162.916 31.218 166,359

1900 20.786 39.694 184.826 166.040 33.296 167.302

ZOO0 20.786 61.573 185.892 165.106 35.375 168.205

2100 20.786 43.651 186.906 166.120 37.454 169.071

2200 20,786 45.730 187,873 167.087 39,532 169.904

2300 20.786 67.808 188.797 168.011 41.611 17D.706

2400 20.786 49.887 189,682 168.896 43.690 171.478

2500 20.786 51.966 ]90.531 169,744 45.768 172.223

2600 20.786 54,064 191.346 170.560 67.847 172.963

2700 20.786 56.125 192.130 171.344 49.926 173.639

2800 20.786 58.202 192,886 172.100 52,004 174.313

2900 20,786 60.280 193.616 172.829 54.083 174.967

3000 20,786 62.359 194.320 173.554 56.161 175.600

3100 20.786 66.437 195,002 174.216 58,240 176,215

3200 20.786 66.516 195,662 174.876 60.319 176.812

3300 20,786 68.595 196.302 175.515 62.597 177.393

5400 20.786 70.673 196.922 176.136 64.476 177.959

3500 20.786 72.752 197.525 176.738 66.555 178.509

3600 20.786 74.831 198.110 177.326 68,653 179.045

3700 20.786 76.909 198,680 177.893 70.712 179.568

5800 20.786 78.988 199.234 178.648 72.790 180.079

5900 20.786 81,066 199,776 178.988 76.869 180.577

4000 20.786 83.165 200.300 179.516 76.948 181.063

4100 20.786 85.224 200.814 180.027 79.026 181.539

6200 20.786 87.302 201.314 180.528 81.105 182.006

6300 20.786 89.381 201.804 181.017 83.184 182.459

6400 20.786 91,460 202,281 181.495 85,262 182.904

4500 20.786 93,538 202.749 181.962 87.541 183.339

4600 20.786 95.617 203.205 182.419 89.419 183.766

4700 20.786 97.695 203.652 182.866 91.698 186.185

4800 20.786 99.776 204,090 183.304 93.577 184.595

6900 20.786 101.855 206.519 183.732 95.655 184.997

5000 20.786 103.931 204,939 184.152 97.756 185.392

5100 20.786 106.010 205.350 184.564 99.813 185.779

5200 20.786 108.089 205.754 186.968 101.891 186.159

5300 20.786 110,167 206.150 185.364 103.970 186.533

5400 20.786 i12.2_6 206,538 185.752 106,068 186,900

5500 20.786 114.325 206.920 186.133 108,127 187.260

5600 20.786 116.603 207.296 186.508 I10,206 187,615

5700 20.786 i18,482 207.662 186.876 112.284 187.963

5800 20.786 120.560 208,024 187.237 116.363 188.306

5900 20.786 122.639 208.379 187.593 116.442 188.663

6000 20,786 126.718 208.728 187.942 118.520 188.975

6200 20.781 128.874 209.610 188.624 122.677 189.623

6600 20.780 133.030 210.070 189.284 126.853 190.252

6600 20.780 157.186 210.709 189.923 130.989 190.862

6800 20.781 161.562 211.329 190.54_ 135.145 191.455

7000 20.783 145.499 211.932 191.146 139.301 192.032

7200 20.785 169.656 212.517 191.732 143.658 192.593

7400 20.787 153.813 213,087 192.301 147.615 193.139

7600 20.788 157.970 213.641 192.856 151.773 193.671

7800 20.789 162.128 214.181 193,396 155,931 194.190

8000 20.790 166.286 216,708 193.922 160.089 196.696

T

K

0

200

298.15

300

600

500

600

700

800

900

I000

1100

1200

1300

1400

1500

1600

1700

1600

1900

2000

2100

2200

2300

2600

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

6000

4100

6200

630O

6600

4500

4600

6700

4800

6900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

183

NASA/TP-3287/REV 1
T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

I0000

10500

Ii000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

TABLE IX,3,4. • Conclgded.

C° H°0")'H°_) s°cr) "{G°('r)'H°(o))_ H°_) -G°(T)_ T

_m_l-K _.,_ot J_-K J_oI-K kJ_ol JIm_-K K

20.790 170.4_4 215.221 19_.435 164.247 195.191 8200

20,790 17q.602 215.722 194.936 168.405 195.674 8400

20.789 178.760 216.211 195._25 172.562 196.146 8600

20.788 182.918 216.689 195.903 176.720 196.607 8800

20.787 187.075 217.156 196.370 180.878 197.059 9000

20.786 191.232 217.613 196.827 185.035 197.501 9200

20.784 195.389 218.060 197.274 189.192 197.933 9400

20.783 199.546 218.498 197.712 193.348 198.357 9600

20.782 203.702 218.926 198.140 197.505 198.773 9800

20.780 207.859 219.346 198.560 201.661 199,180 10000

20.778 218.248 220.360 199.574 212,051 200.164 10500

20.778 228.637 221.326 200.541 222.440 201.105 11000

20.780 239.027 222.250 201._65 232.829 202.004 11500

20.785 249.418 223.154 202.350 2_3.220 202.866 12000

20.795 259.812 223.983 203.198 253.615 205.694 12500

20.805 270.212 224.799 204.013 26_.014 204.490 13000

20.822 280,618 225.584 20_.798 27_._21 205.257 13500

20.845 291.05_ 226.542 205.554 28_.837 205.996 i_000

20.870 501.462 227.074 206.285 295.265 206.711 14500

20.905 311,906 227.782 Z06.988 305.708 207.401 15000

20.948 522.568 228._68 207.670 316.171 208.070 15500

21.002 352.855 229.154 Z08.330 526.658 208.718 16000

21.069 3_3.373 229.781 208.971 337.175 209.346 16500

21.155 553.927 250.411 209.592 3_7.730 209.957 17000

21.255 364.528 231.026 210.196 358.331 210.550 17500

21.580 375.186 231.626 210.783 368.988 211.127 18000

21.532 385.913 232.214 211.35_ 379,715 211.689 18500

21.715 396.725 232.791 211.911 390.525 212.257 19000

21.936 q07.63_ 233.358 212.453 _01._37 212.771 19500

22.199 _18.666 233.916 212.983 412.468 213.293 20000

184 NASA/TP-3287/REV 1
TABLE 1X.35. -THERMODYNAMIC FUNCTIONS FROM COEFFiCiENTS FOR Nl(cr,I)

T C ° HoCr).Ha(_ _(T) _GOC_._o(O))n HOcr) _oF3K T

K J/m_FK kJ/mol J_oI-K _moI-K _/mo! J_ol-K K

0 0.000 0.000 0.000 0.000 -4.786 INFINITE 0

200 22.468 2.398 20.202 8.212 -2.388 32.142 200

298.15 25.987 4.786 29.870 13.818 0.0O0 29.870 298.15

300 26.041 4.834 30.031 13.917 0.048 29.870 300

400 28.493 7.562 37.863 18.957 2.776 30.922 400

500 31.047 10.539 44.497 23.420 5.753 32.992 500

600 34.855 13.814 50.459 27.436 9.028 35.413 600

700 30.573 17.275 55.810 31.132 12.489 37.969 700

800 30.909 20.326 59.883 34.476 15.540 40.458 800

900 31.451 23.447 63.558 37.507 18.661 42.824 900

1000 32.194 26.625 66.907 40.281 21.639 45.067 1000

1100 32.882 29.88' 70.012 42.845 25.098 47.196 1100

1200 33.677 33.198 72.895 45.230 28.41Z _9.219 1200

1300 34.427 36.601 75.619 47.464 31.815 51.146 1300

1_00 35.342 40.089 78.Z03 49.568 35.303 52.987 1400

1500 36.291 43.670 80.67_ 51.560 38.884 54.751 1500

1600 37.251 47.347 83.0,6 38 254 51 122 85.334 5. • •

_ 7_'¢cn R_'1q7 85 962 55.755 47.411 58.525 1728

............ ...... ...... ...... 755 6 566 8525 1728 1728 .... 67368 60o51 18oo

1900 35.911 76.045 99.582 59.558 71.259 62.077

2000 38.911 79.936 101.577 61.609 75.150 64.002

2100 38.911 83.827 103.476 63.558 79.041 65.837

2200 38.911 87.718 105.286 65.414 82.932 67.590

2300 38.911 91.609 I07.016 67.186 86.823 69.266

2400 38.911 95.500 108.672 68.880 90.714 70.874

2500 38.911 99.391 110.260 70.504 94.605 72.418

2600 38.911 103.283 111.786 72.062 98.497 73.903

2700 38.911 107.174 113.255 73.561 102.388 75.333

2800 35.911 111.065 114.670 75.00_ 106.279 76.713

2900 38.911 114.956 116.035 76.395 I10,170 78.0,6

3000 38.911 118.847 117.355 77.739 11_.061 79.33,

3100 38.911 122.738 118,630 79.037 117.952 80.581

3200 38.911 126.629 119.866 80.294 121.843 81.790

3300 38.911 130.520 121.063 81.512 125.734 82.962

3400 38.911 134,411 122.225 82.692 129.625 84.100

3500 38.911 138.302 123.353 83.838 133.516 85.205

3600 38.911 142.19_ 124.449 84.951 137.408 86.280

3700 38.911 146.085 125.515 86.033 141.299 87.326

3800 38.911 149.976 126.553 87.085 145.190 88.345

3900 38.911 153.867 127.563 88.110 149.081 89.337

4000 35.911 157.753 128.549 89.109 152.972 90.306

4100 38.911 161.649 129.509 90.083 156.863 91.250

4200 38.911 165.5,0 130.447 91.033 160.754 92.172

,300 38.911 169.431 131.363 91.960 164.645 93.073

4400 38.911 173.322 132.257 92.866 168.536 93.953

4500 38.911 177.213 133.132 93.751 172.427 94.814

4600 38.911 181.105 133.987 9q.616 176.319 95.657

4700 38.911 184.996 134.824 95.463 180.210 96.481

_&O0 38.911 188.887 135.643 96.291 184.101 97.288

4900 38.911 192.778 136.,05 97.103 187.992 98.079

5000 38.911 196.669 137.231 97.897 191.883 98.855

5100 38.911 200.560 138.002 98.676 195.774 99.615

5200 38.911 20_._51 138.757 99.440 199.665 100.360

5300 38.911 208.342 139.499 100.189 203.556 101.092

5,00 38.911 212.233 140.226 100.923 207._47 101.810

5500 38.911 216.124 1,0.940 101.644 211.338 102.515

5600 38.911 220.016 141.641 102.352 215.230 103.207

5700 38.911 223.907 142.330 103.048 219.121 103.887

5800 38.911 227.798 143.006 103.731 223.012 104.556

5900 38.911 231.689 143.672 104.402 226.903 105.213

6000 38.911 235.580 144.326 105.062 230.794 105.860

1900

2000

2100

2200

2300

2900

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

,300

0400

_500

4600

0700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV l 185
TABLE IX.36. • THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR O2

T C ° H°t'rH.t°_) S°t'D _GO(T)-HO(0))_

K J/m_l-K _Ntml J/mol-K J_oI-K

0 0.000 0.000 0.000 0.000

200 29.126 5.812 193.484 164,425

298.15 29.378 8.680 205.1Q9 176.036

300 29,388 8.734 205.331 176.216

400 30.115 11.706 213.875 184.610

500 31.092 14.766 220.698 191.167

600 32.090 17.925 226.456 196.581

700 32.990 21.180 231.472 201.214

800 33.745 24.518 235.928 205.280

900 34.361 27.925 239.939 Z08.912

1000 34.883 31.387 243.587 212.200

IIO0 35.333 34.899 246.934 215.208

1200 35.695 38,451 250.024 217.982

1300 36.006 42.036 252.894 220.558

1400 36.288 45.651 255.573 222.965

1500 36.553 49.293 258.086 225.223

1600 36.808 52.961 260.453 227.352

1700 37,057 56.655 262.692 229.365

1800 37.302 60.373 264.817 231.276

1900 37.545 64.115 266,840 233.095

2000 37.784 67.882 268.772 234.831

2100 38.020 71,672 270.621 236.492

2200 38.254 75.486 272.395 238.084

2300 38.484 79.322 274.101 139.613

2400 38.710 83.182 275.744 241.084

2500 38.933 87.064 277.328 242.503

2600 39.152 90.969 278.860 243.872

2700 39.366 94.895 280.341 245.195

2800 39.575 98.842 281.777 246.476

2900 39.780 102.810 283.169 247.717

3000 39.980 106.798 284.521 248.922

3100 _0.175 110.805 285.835 250.091

3200 40.365 114.832 287.114 251.229

3ZD0 40.549 118.878 288.359 252.335

3400 _0.729 122.942 289.572 253.412

3500 40.904 127.024 290.755 254.462

3600 41.074 131.123 291.910 255.487

3700 41.239 135,238 293.037 256,486

3800 41.400 139.370 294.139 257.463

3900 41.556 143.518 295.217 258.417

4000 41.707 147.681 296.271 259.350

4100 41.854 151.860 297.302 260.263

4200 41.997 156.052 298.313 261.]57

4300 42.135 160.259 299.302 262.033

4400 42.269 164.479 300.273 262.891

4500 42.400 168.712 301.224 263.732

4600 42.526 172.959 302.157 264.558

4700 42.649 177,218 303.073 265.367

4800 42.769 181.489 303.972 266.162

4900 42.884 185.771 304.855 266.943

5000 42.997 190.065 305.723 267.710

5100 43.106 194.370 306.576 268.464

5200 43.212 198.686 307.414 269.205

5300 43.315 203.013 308.238 269.933

5400 43.414 207.349 309.048 270.650

5500 43.511 211.696 309.846 271.356

5600 43.605 216.051 310.631 272.050

5700 43,695 220.416 311.403 272.734

5800 43.783 224.790 312.164 273.407

5900 43.868 229.173 312.913 274.070

6000 43.950 233.564 313.651 274.724

6200 44.059 242.365 315.094 276.003

6400 44.161 251.187 316.494 277.246

6600 44.246 260.018 317.855 278,456

6800 44.306 268.884 319,177 279.635

7000 44.338 277.749 320.461 280.783

7200 44.339 286.617 321.711 281.903

7400 44,308 295.482 322.925 282.995

7600 44.244 304.338 324.106 284.061

7800 44.149 313.178 325.254 285.103

8000 44.023 321,995 326.370 286.121

H*03

_lmol

-8 680

-2 868

0 000

0 05_

3 026

6 086

9.245

12.500

15.838

19.244

22.707

26.219

29.771

33.356

36.971

40.613

44.281

47.975

51.693

55.435

59.202

62.992

66.805

70.642

74.502

78.384

82.289

86.215

90.162

94.129

98.117

102.125

106.152

110.198

114.262

118.344

122.443

126,558

130.690

134.838

139.001

143.179

147.372

151.579

155.799

160.032

164.279

168,537

172.808

177.091

181.385

185.690

190.006

194.333

198.669

203.015

207.371

211.736

216.110

220.493

224.884

253.685

242.507

251.348

260.204

269.069

277.937

286.802

295.658

304.498

313.315

J/mol_

INFINITE

207.826

205.149

205.150

206.310

208,527

211.048

213.615

216.130

218,557

220.880

223,099

225.215

227.235

229.165

231.010

232.777

234.471

236.099

237.66_

239.171

240.625

242.029

243.387

244.701

245.975

247.210

248.410

249.576

250.711

251.815

252.892

253.941

254.965

255.965

256.942

257.898

258.832

259.747

260.643

261.520

262.381

263.224

264.052

264.864

265.661

266.445

267.214

267,971

268.714

269.446

270.166

270.874

271.571

272.258

272.934

273.600

274.256

274.904

275.541

276.170

277.403

278.605

279.772

280.911

282.023

283.108

284.168

285.204

286.216

287.206

T

K

0

200

298.15

300

400

500

600

700

800

900

I000

II00

1200

1300

1400

k500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

5700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

186 NASA/TP-3287/REV 1
T

K

8200

8400

8600

8800

9000

9200

9000

9600

9800

10000

10500

11000

11500

12000

L2500

13000

13500

lq000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

C °

J/moPI-K

43.868

43.685

43.477

43.245

42.992

42.720

42._,30

62.125

41.807

41.477

q0.613

59.713

38.796

37.881

36.979

36. 102

35. 257

34.449

33.683

32.960

32.281

31.644

31.049

30.494

29.975

29.491

29. 037

28,611

28.210

27.830

TABLE IX.36. -Concluded.

H°(T)'H°(0) SO(T) _GO(T).HO(0)}K HO@) _o_)n T

_ol JlmoI-K J_oI-K _d JlmoI-K K

330.785 327.455 287.116 322.105 288.174 8200

339.541 328.510 288.089 330.861 289.122 8400

348.257 329,536 289.041 339.577 290.050 8600

356,930 330.533 289.973 348,Z50 290.959 8800

365.554 331.502 290.885 356.B74 291.849 9000

374.125 332.444 291.778 365.445 292.721 9200

382.640 333.359 292.653 373.960 293.576 9400

391.096 334.250 293.510 382.416 294.415 9600

399,490 355.115 294,351 390.809 295,236 9800

407.818 335.956 295.174 599.138 296.042 10000

428.343 337.959 297.165 419.663 297.991 I0500

_48.426 339.828 299.062 439.765 299.851 11000

468.053 341.573 300.873 459.373 301.627 11500

487.222 343.205 302.603 478.542 303.326 12000

505,936 344.733 304.258 497,256 304.952 12500

524.205 346.166 305.842 515.525 306.510 13000

542.043 347.512 307.361 533.363 308.006 13500

559.668 348.780 308.818 550.788 309.438 14000

576.499 349.975 310.217 567.819 310.815 14500

593.159 351.105 311.561 584.479 312.140 15000

609.667 352.174 312.856 600.787 315._14 15500

625.647 353.189 314.099 616.767 316.641 16000

641.118 356.154 315.298 632.638 315.824 16500

656.503 355.072 316.455 647.823 316.965 17000

671.619 355.949 317.570 662.938 318.067 17500

686.484 356.786 318.648 677.806 319.131 18000

701.114 357.588 319.690 692.434 320.159 18500

715.525 358.357 320.697 706.845 321.154 19000

729.750 359,095 321.673 721,050 322.118 19500

743.739 359.804 322.617 735.059 323.051 20000

187

NASA/TP-3287/REV l
TABLE IX,37. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR P(cr.whRe,f)

T C_ H°(T)'H°( 0) S°(T) "{G°(T)-He(O)}/T H°m -G°(T)IT T

K J/mohK k,J/mol J/moi-K J/moI-K k,J/mol JJmol-K K

0 0. 000 0. 000 0. 000 0. 000 -5. 360 INFINITE 0

20D 21,086 3. 151 32. 139 16. 385 -2.209 43. 185 200

298.15 23.824 5.360 41.090 23.112 0,000 41.090 298,15

300 23 o869 5. 604 41.238 23.22_, O. 064 41. 090 300

or 317.30 2_.267 5.821 42.587 24.2(*3 0.(+61 41.136 317.30

! 317.30 26,120 6.480 44.664 2<i ,243 1,120 41.136 317,30

400 26.120 8.640 50.714 29.115 3.280 42.515 400

500 26,120 11.252 56.542 34.039 5.892 44.759 500

600 26.120 13.864 61.305 38.198 8.504 47,132 600

700 26.120 16.476 65.331 41.794 11,116 49.451 700

800 26.120 19.088 68.819 44.959 13.728 51.659 800

900 26.120 21,700 71.895 47.785 16.340 53,740 900

1000 26.120 24,312 74,647 50.336 18.952 55.696 1000

1100 26.120 26.924 77.137 52.661 21.564 57.533 1100

1200 26.120 29.536 79.410 54,796 24.176 59.263 1200

1300 26.120 32.148 81.500 56.771 26.788 60.894 1300

1400 26.120 36.760 83.436 58.608 29.400 62.436 1400

1500 26,120 37.372 85.238 60.324 32.012 63.897 1500

1600 26.120 39.986 86.924 61.934 34.629 65.284 1600

1700 26.120 42,596 88.507 63.451 37.236 66.604 1700

1800 26.120 65.208 90.000 64.885 39,868 67.863 1800

1900 26.120 47.820 91.613 66.246 42.460 69.065 1900

2000 26.120 50,432 92.752 67.536 45.072 70.216 2000

2100 26,120 53.066 94.027 68.768 47,684 71.320 2100

2200 26,120 55.656 95,242 69.944 50.296 72.380 2200

2300 26.120 58.268 96.403 71.069 52.908 73,400 2300

2400 26.120 60.880 97,515 72.168 55.520 76.381 2400

2500 26.120 63.492 98.581 73.184 58,132 75.328 2500

2600 26.120 66.104 99.605 74.181 60.764 76.242 2600

2700 26.120 68.716 100.591 75.141 65.356 77.126 2700

2800 26.120 71.328 101.541 76.067 65.968 77.981 2800

2900 26.120 73.940 102.458 76.961 68.580 78.809 2900

3000 26.120 76.552 103.343 77.826 71.192 79.612 3000

3100 26.120 79,164 104.200 78.663 73.606 80.392 3100

3200 26.120 8].776 105.029 79,474 76.416 81.149 3200

3300 26.120 86.388 105.833 80.261 79.028 81.885 3300

3600 26.120 87.000 106.612 81.024 81.660 82.601 3400

3500 26,120 89.612 107.369 81.766 84.252 85.298 3500

3600 26.120 92,224 108.105 82._88 86.864 83.976 3600

3700 26.120 94.836 108.821 83.190 89.476 84.638 3700

3800 26.120 97.448 109.518 83.873 92.088 85.284 3600

3900 26.120 100.060 110.196 84.540 94.700 85.914 3900

4000 26.120 102.672 110.857 85.189 97.312 86.529 4000

4100 26.120 105.284 111.502 85.823 99.924 87.131 4100

4200 26.120 107.896 112.132 86.442 102,536 87,718 4200

4300 26.120 110.508 112.746 87.047 105.148 88.293 4300

4400 26.120 113.120 113.367 87.638 107.760 88.856 4400

4500 26.120 115.732 113.934 88.216 110.372 89.407 4500

4600 26.120 118.344 114.508 88.781 112.984 89.946 4600

4700 26.120 120.956 115.070 89.334 115.596 90.475 4700

4800 26,120 123.568 I15.620 89.876 118.208 90.993 4800

_900 26.120 126.180 116.158 90.407 120.820 91.501 4900

5000 26.120 128.792 116.686 90.927 123.432 91.999 5000

5100 26.120 131.404 117.203 91,438 126.046 92.489 5100

5200 26.120 134.016 117.710 91.938 128.656 92.969 5200

5300 26,120 136.628 I18,208 92.429 131.268 93.440 5300

5400 26,120 139.240 118.696 92.911 133.880 93.904 5400

5500 26.120 141.852 119.175 93.384 136.492 94.359 5500

5600 26,120 144.46_ I19.6_6 93.849 139.104 94.806 5600

5700 26,120 147.076 120.108 94.306 141.716 95.246 5700

5800 26.120 149,688 120.563 94.754 144.328 95.678 5800

5900 26,120 152.300 121.009 95.196 146.940 96.104 5900

6000 26.120 154.912 121.448 95.629 149.552 96.523 6000

188 NASA/TP-3287/REV 1
TABLE 1X.38. -THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Pb(cr,I)

T C ° HOfD._p(_ So(-D _G=(T).HO(O)}rr H=(-D _=(T)K T

K Nm_I-K _/mol Nmol-K J/moI-K kJ/mol J_oI-K K

6 0.000 0,000 0.000 0.O00 -6.870 INFIIIITE 0

200 25.771 4,295 54,328 32,861 -2.577 67.211 200

298.15 26.650 6,870 64,800 41.758 0,000 64.800 298.15

500 26.670 6,919 6Q.965 41.901 0.049 64.801 300

350 27.242 8.267 69,118 45,499 1.397 65.127 350

400 27,801 9.643 72.793 48.685 2.773 65.860 400

450 28.298 11.046 76.097 51.550 4.176 66.817 450

500 28.776 12,473 79.103 54.158 5.603 67.898 500

550 29.271 13.924 81.B69 56.553 7.054 69.044 550

600 29,736 15.399 84,436 58,771 8,529 70,221 600

cr 600.65 29,741 15,419 84.468 58,798 8,549 70.236 600.65

.........................................................................

; 60 65- 30.627 z0231 92 480 5879; .... 7 236 - ; 0 65

700 0. 13 23.2 8 97.145 63.919 16.388 73.733 700

800 29.979

900 29.660

i000 29.369

1100 29.116

1200 28.903

1300 28.731

1400 28.602

1500 28.513

1600 28.465

1700 28.451

1800 28.475

1900 28.532

Z000 28,620

2100 28.737

2200 28.881

2300 29.048

2400 29.238

2500 29.446

260O 29.671

2700 29.909

2800 30.160

2900 30.419

3000 30.684

3100 30.953

3200 31.223

3500 31.492

3_00 31.757

3500 32.015

3600 32.264

26.273 101.171 68.330 19,403 76.917 800

29.255 I09.683 72,178 22.385 79.811 900

32.206 107.793 75.587 25.336 82,457 1000

35.130 110.580 78,644 28.260 84.889 I100

38.030 113.104 81.412 31.160 87.187 1200

40.912 115.410 83.940 34.042 89.224 1300

43.778 117.534 86.264 36.908 91.172 1400

46.653 119.504 88,415 39.763 92,995 1500

49.482 121.343 90.417 42.612 94.710 1600

52.327 123.068 92.287 45.457 96.328 1700

55.173 124.694 94.043 48,303 97.859 1800

58.023 126.235 95,697 51,153 99,313 1900

60.881 127.701 97.261 54.011 100.696 2000

63.748 129,100 98.744 56.878 102.015 2100

66.629 130.440 100.154 59.759 103.277 2200

69.525 131.728 101.499 62.655 104.486 2300

72._59 132.968 102.785 65.569 105.647 2400

75.373 134.165 104.016 68.503 106.764 2500

78.329 135,325 105,198 71._59 107.840 2600

81.308 136.449 106.335 74.438 108.879 2700

84.311 137.541 107.430 77.441 109.884 2800

87.340 138.604 108.487 80,_70 110.856 2900

90.395 139.640 109.508 83.525 111.798 3000

93.477 140.650 110.496 86.607 112.712 3100

96.586 141.637 111.454 89.716 113.601 3200

99.722 142.602 112.383 92.852 I14._65 3300

102.884 143.546 113.286 96.014 115.307 3400

106.075 144.470 114.164 99.203 116,127 3500

109.287 145.376 115.018 102.417 116.927 3600

NASA/TP-3287/REV 1 189
TABLE IX.39. - THERMODYNAME, FUNCTIONS FROM COEFFICIENTS FOR Rb(cr, _)

T C o H°(l')'H°( 0 ) S°( T ) "{G°(T)'H°(O)}K HOt'r) -G°(T)/T T

K J/moPI-K WJImol JlmoI.K Jlmol-K kJ/rnol JlmoI.K K

0 0.000 O. 000 O. 000 O. 000 -7.489 INFINITE 0

200 27.446 4. 657 65. 302 62. 018 -2.832 79 . 463 200

298,15 31.060 7.489 76.78D 51.662 0,000 76.780 298.15

300 31. 209 7.5q7 76. 973 51,817 0. 058 76.781 300

cr 312.47 32.385 7.943 78.266 52.847 0.454 76.814 312.47

Q 312.47 31.801 10.135 85.281 52.847 2.6_6 76.814 312.47

400 30. 824 12.868 92. 998 6 D.828 5. 379 79. 550 400

500 50._84 15.950 99.831 67.972 8.441 82.950 500

600 30.440 18.974 105.382 73.758 11.485 86.240 600

700 50.525 22.022 110.080 78.620 14.533 89.319 700

800 30.709 25,082 114.166 82,813 17,593 92,175 800

900 5i.OIZ 28,167 117.800 86,502 20.678 94.824 900

1000 51.476 31.290 121.089 89,799 23.801 97.288 I000

Ii00 32.151 34.470 124.119 92.783 26,981 99.591 ii00

1200 33.094 37.729 126.955 95.514 30,240 101.755 1200

1300 34.366 41.099 129.652 98.037 33.610 103.798 1300

1400 36.027 _4.616 132.257 100.388 37.127 105.738 1400

1500 38.140 48.320 134.B12 102.598 40.831 107.591 1500

1600 40.768 52.261 137.354 104.691 44.772 109.372 1600

1700 43.976 56.493 139.919 106.688 _9.004 111.093 1700

1800 _7,828 61.077 142.538 108.606 53.588 112.767 1800

1900 52,387 66.082 145.243 110.463 58.593 i14,40_ 1900

2000 57.719 71.581 148.062 112.272 64.092 116,016 2000

2108 63.887 77.654 151.024 114.046 70.165 117.612 2100

190 NASA/TP-3287/REV 1
TABLE IX.40. -THERMODYNAM_ FUNCTION8 FROM COEFFICIENTS FOR S(u._,_

T C o HO(T).Ho_) SO(T) _GO(T-).Ho(O)}K HO(T) _ O('T)/T T

K _m_l-K kJ/tool J/moI-K _moI-K _lmol J/moI-K K

0 0ii000 0.000 0.000 0.000 -4.412 INFINITE 0

200 19.360 2.333 23.655 11.992 -2.079 34,052 200

298.15 22.690 4.412 32.070 17.272 0.000 32.070 298.15

300 22.737 4.454 52.211 17,364 0.042 32.070 300

368.30 26.237 6.061 37.031 Z0,574 1.649 32.554 368,30

............................................................................................

368.30 24.773 6.462 38.119 20.574 2.050 32.554 368.30

B 388.36 25.180 696! 39.444_ 1515 2.551 _ 3 :87 ....

400 32.369 9.058 44.824 22.180 4.646 33.210 400

428.15 36.595

432.25 48.833

453,15 42.472

500 38.026

550 35.614

600 34.371

650 33.493

700 32.451

717 31,992

800 32.000

900 32,000

1000 32.000

110o 32.000

1200 32.000

1300 32.000

1400 32.000

1500 32.000

1600 32.000

1700 32.000

1800 32.000

1900 32.000

2000 32.000

2100 32.000

2200 32.000

2300 32.000

2400 32.000

2500 32.000

2600 32.000

2700 32.000

2800 32,000

2900 32.000

3000 32.000

3100 32.000

3200 32.000

3300 32.000

3400 32.000

3500 32.000

3600 32.000

3700 32.000

3800 32.000

3900 32.000

4000 32.000

4100 32.000

4Z00 32.000

4300 32.000

4400 32,000

4500 32.000

4600 32.000

4700 32,000

4800 32.000

4900 32.000

5000 32.000

5100 32.000

5200 32.000

5300 32.000

5400 32.000

5500 32.000

5600 32.000

5700 32.000

5800 32.000

5900 32.000

6000 32.000

10.002 _7.104 23.743 5.590 34.048

10.173 47.502 23.966 5.761 34.173

ii.I18 49.638 25.103 6,706 5_.839

12,993 53,578 27.593 8.581 36.417

14.827 57.076 30.118 10.415 38.140

16.573 60.116 32.494 12.161 39.847

18.270 62.832 34,725 13.858 41.513

19,920 65.279 36.822 ]5.508 43.124

20.468 66.052 37,505 16.056 43.659

23.124 69.557 40.652 18.712 46.267

26.324 73.326 44.077 21.912 48.980

29.524 76.698 47.174 25.112 51.586

32.724 79.748 49.999 28.312 54.010

35.92_ 82.532 52,595 31.512 56.272

39.124 85.093 54.998 34.712 58.392

42.324 87.465 57.233 37.912 60.385

45.524 89.672 59.323 41.112 62,265

48.724 91.738 61.285 44.312 64.043

51.924 93.678 63.134 47.512 65.730

55.124 95.507 64.882 50.712 67.334

58.324 97.237 66.540 53.912 68.862

61.524 98.878 68.116 57.112 70.322

64.724 i00.4_0 69.619 60.312 71.720

67.924 101,928 71.054 63.512 73.059

71.124 103.351 72.427 66.712 74.346

74.324 104,713 73.744 69.912 75.583

77.524 106.019 75.009 73.112 76.774

80.724 107.274 76.226 76.312 77.923

83.924 108.482 77.399 79.512 79.033

87.12_ 109.645 78,530 82.712 80.106

90.32_ 110.768 79.622 85,912 81.14_

93.524 111.853 80.679 89.112 82.149

96,724 112,902 81.701 92.312 83.124

99.924 113.918 82.692 95.512 84,071

103.124 114.903 83.654 98,712 84.990

106.324 115.858 84.587 101.912 85.884

109.524 116.786 85.494 105.112 86.754

112.724 117.687 86.375 108.312 87.601

115.924 118.564 87.234 111.512 88.426

I19.124 i19,418 88.069 114.712 89.230

122.324 120.249 88.884 117.912 90.015

125.524 121,059 89.678 121.112 90.781

128.724 121.849 90.453 124.312 91.529

131.924 122,620 91,210 127.512 92.260

135.124 123,373 91.949 130.712 92.975

138.324 124,109 92.672 133.912 93.674

141.524 124.828 93.378 157.112 94.359

144.724 125.531 94.070 140.312 95.029

147.924 126.220 94.746 143.512 95.685

151.124 126.893 95.409 146.712 96.328

154,324 127.553 96.058 149.912 96.959

157.524 128.200 96.695 153.112 97.577

160.724 128,833 97,319 156.312 98.184

163.924 129.455 97.931 159.512 98.779

167.124 130.064 98.531 162.712 99.364

170.324 130,662 99.121 165,912 99.938

173.524 131.250 99.700 169.112 100.502

176.724 131.826 100.268 172.312 101.056

179.924 132.393 100.827 175.512 101.601

183.124 132.949 101.376 178.712 102.137

186.32_ 133.496 101.916 181.912 102.66_

189.524 134,034 102.447 185.112 103.182

428.15

432.25

453.15

500

550

600

650

700

717

800

9O0

1000

I100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

NASA/TP-3287/REV l 191
TABLE IXA1. oTHERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Si(cr,(i)

T C o H°('T')"HO{_ S°(T) _G°(T')-H°(_)_ H°('l") _°('T')ff T

K _m_l-K kJ/m_ J/moI-K J/mol_ I_l/mol J/moI-K K

0 0.000 0.000 0.000 0.000 -3.217 INFINITE 0

200 15.656 1.452 11.683 4.422 -1.765 20.509 200

298.15 19,789 3.217 18.810 8.019 0.000 18.810 298.15

300 19.855 3.254 18.933 8.085 0.037 18.810 300

400 22.301 5.377 25.023 11,580 2.160 19.624 _00

500 23.610 7.678 30.152 14.796 4.461 21.231 500

600 24.472 10.085 34.537 17.730 6.867 23.092 600

700 25.123 12.566 38.361 20.410 9.348 25.006 700

800 25.662 15.106 41.752 22.870 11.888 26.891 800

900 26.135 17.696 44.802 25.140 14.478 28.715 900

1000 26.568 20.331 47.578 27.247 17.114 30.464 1000

1100 26.974 23.009 50.130 29.213 19.791 32.138 1100

1200 27.362 25.725 52.493 31.056 22.508 33.737 1200

1300 27.737 28.480 54.698 32.790 25.263 35.265 1300

1400 28.103 31.273 56.767 34.430 28.055 36.728 1400

1500 28.462 34.101 58.719 35.985 30.883 38.130 1500

1600 28.816 36.965 60.567 37.464 33.747 39.475 1600

cr 1690 29.131 39.572 62.152 38.737 36.355 40.640 1690

Q 1690 27.200 89.782 91.862 58.757 86.565 40.640 1690

1700 27.200 90.054 92.023 39.050 86.837 40.942 1700

1800 27.200 92.774 93.578 42.036 89.557 43.824 1800

1900 27.200 95.494 95.048 44.788 92.277 46.481 1900

2000 27.200 98.214 96.443 47.336 94.997 48.945 2000

2100 27,200 100.934 97.770 49.706 97.717 51.239 2100

2200 27.200 103,654 99.036 51.920 100.437 53.383 2200

2300 27.200 106.374 100.245 53.995 103.157 55.394 2300

2_00 27.200 109.094 101.402 55.946 105.877 57.287 2400

2500 27.200 111.814 102.513 57.787 108.597 59.074 2500

2600 27.200 114.534 103.580 59.528 111.517 60.765 2600

2700 27.200 117.254 104.606 61.179 114.037 62.370 2700

2800 27.200 119.974 105.595 62.747 116.757 63.896 2800

2900 27.200 122.694 106.550 64.241 119.477 65.351 2900

3000 27.200 125.414 107.472 65.667 122.197 66.740 3000

5100 27.200 128.134 108.364 67.030 124.917 68.068 3100

3200 27.200 130.854 109.227 68.335 127.637 69.341 3200

3300 27.200 133.574 110,064 69.587 130.357 70.562 3300

3400 27.200 136.294 110.876 70,790 133.077 71.736 3400

3500 27.200 139.014 111.665 71.946 135.797 72.866 3500

3600 27.200 141.734 112.431 73,060 138.517 73.954 3600

3700 27.200 144.454 113.176 74.135 141.237 75.004 3700

5800 27.200 147.174 113.902 75.172 143.957 76,018 3800

5900 27.200 149.894 114.608 76.174 146.677 76.999 3900

4000 27.200 152.614 115.297 77.143 149.397 77.948 qO00

6100 27.200 155,334 115.969 78.082 152.117 78.867 4100

4200 27.200 158.054 116.624 78.992 15_.837 79.758 4200

_300 27,200 160.774 117.264 79.875 157,557 80.623 4300

4_00 27.200 163.494 117.889 80.732 160.277 81.463 4400

_500 27.200 166.214 118.501 81,564 162.997 82.279 4500

_600 27.200 168.934 119.098 82.374 165.717 83.073 4600

6700 27.200 171.654 119.683 83.161 168.437 83.846 4700

4800 27.200 174.374 120.256 83.928 171.157 84.598 4800

4900 27.200 177.094 120.817 84.675 173.877 85.332 4900

5000 27.200 179.814 121.366 85.404 176.597 86.047 5000

5100 27.200 182.534 121.905 86.11_ 179.317 86.745 5100

5200 27.200 185.254 122.433 86.807 182,037 87.426 5200

5300 27.200 187.974 122.951 87.484 184.757 88.092 5300

5400 27.200 190.694 123.460 88.146 187.477 88.742 5400

5500 27.200 193.414 123,959 88.793 190.197 89.378 5500

5600 27.200 196.134 124.449 89.425 192.917 90.000 5600

5700 27.200 198.854 124.930 90.044 195.637 90.608 5700

5800 27.200 201.574 125.403 90.649 198,357 91.204 5800

5900 27,200 204.294 125.868 91.242 201.077 91.788 5900

6000 27.200 207.014 126,326 91.823 203.797 92.359 6000

192 NASA/TP-3287/REV 1
T

K

0 0.000

200 25.500

298.15 27.112

300 27.144

350 28.026

_00 28.90_

450 29.887

TABLE IX.42. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR 8n(cr,I)

C o H=_'H_W) sO(T) _GO_.Ho_)}K Ho_ _ocr)K T

_m_-K _lmol J_oI-K JlmoI-K kJ/m_ _moI-K K

0.000 0.000 0.000 -6,323 INFINITE 0

3.738 40.683 21.994 -2.585 53.609 200

6.323 51.180 29.973 0.000 51.180 298.15

6.373 51.348 30.104 0.050 _1.181 300

7.752 55.598 33.448 1.429 51.514 350

9.176 59,398 36.459 2.853 52.266 400

10.645 62.857 39.202 4.322 53.254 450

500 31.036 12.167 66.065 41.730 5.844 54.376 500

cr 505.12 31.158 12.326 66.381 41.978 6.003 54.496 505.12

.......................... ; ......;; ;;; ;1-;;; ;;7i;; ;;496.... ;;;;;

, 505.12 29.415 1 59.036 600 600 28.663 22.273 85.620 48.498 35.9S0

700 28.249 25.116 90.003 54.123 18.793 63.156 700

800 28.043 27.930 93.760 58.848 21.607 66.752 800

900 27.957

I000 27.945

II00 27.979

1200 28.044

1300 28.130

1400 28.229

1500 28.339

1600 28.455

1700 28.575

180D 28.698

1900 28.822

2000 28.947

2100 29.071

2200 29.195

2300 29,318

2400 29.439

2500 29.559

2600 29.676

2700 29.792

280D 29.909

2900 30,015

3000 30.123

3100 30,228

3200 30.331

3300 30.431

3400 30,528

3500 30.622

3600 30.713

3700 30.801

3800 30,886

3900 30.968

4000 31.0_7

4100 31.123

_200 31.196

4300 31.266

4400 31.333

_500 31.396

4600 31.457

4700 31.514

30.729 97.057 62.914 24._06

33.52_ 100.002 66.478 27.201

36.319 102.667 69.649 29.996

39.120 105.104 72,503 32.797

_1.929 107.352 75.099 35.606

44.747 109._40 77.478 38,424

47,575 111.391 79.674 41.252

50.415 113.224 81,715 44.092

53.266 114.952 83.619 46.943

56.130 116.589 85.406 49.807

59.006 118.144 87.088 52.683

61.894 119.626 88.679 55.571

64.795 121.041 90.186 58.472

67.708 122.396 91.620 61.385

70.634 123.697 92.986 64.311

73.572 124.947 94.292 67.249

76.522 126.151 95.543 70.199

79.48_ 127.313 96.742 73.161

82.457 128.435 97.895 76.134

85.442 129,521 99.006 79.119

88.438 130.572 100.076 82,I15

91,445 131.591 101.110 85.122

94.462 132.581 102.109 88.159

97.490 133.542 103.076 91.167

100,528 134.477 104.014 94.205

103.576 135.387 104.923 97.253

106.634 136.273 105.806 100.311

109.701 137.137 106.665 103.378

112.776 137.980 107.500 106.453

115.861 138.802 108.313 109.538

116.953 139.606 109.105 112,630

12Z.054 1_0.391 109.877 115.731

125.165 141.158 110.631 118.840

128.279 141.909 111,367 121.956

131.402 142.644 112.085 125.079

134,532 143.364 112.788 128.209

137.668 144.068 113.475 131.345

140.811 144.759 114.148 134.488

143.959 145._36 114.807 137.636

69.940

72.801

75.397

77.773

79.963

81.994

83.890

85.666

87.339

88.919

90.416

91.840

93.197

94.494

95.735

96,927

98,072

99.174

100.237

101,264

102.256

103,217

104.149

105.052

105.930

106.783

107.613

108.421

109.209

109.977

110.726

111.458

112.173

112.872

113.556

114.225

Iiq.881

115.523

116.152

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

270D

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

4600

4700

NASA/TP-3287/REV 1

193
T C °

K J/m_-K

0 0.000

200 25.777

298.15 26.830

300 26.850

400 27.847

500 28.664

600 29.386

700 30.059

TABLE fX.43. - THERMODYNAMIC FUNCTIONS FROM COEFRCIENT8 FOR Sr(Q,_,_)

H°('l')-H°(0) S°(T) _GO(T)-Ho(O)}K HO('TJ

k.J/m_ J/moI.K J/m_-K _ol

0.000 0.000 0.000 -6,558

3.978 44.516 24.626 -2,580

6.558 54.999 33.003 0.000

6.608 55,165 33.139 0.050

9.344 63.031 39.670 2.786

12.171 69.335 44.993 5.613

15.074 74.626 49.502 8,516

18.046 79.205 53.426 11,_88

_%r)JT

J/moFK

INFINITE

57.417

54.999

55.000

56.065

58.109

60.433

62.795

T

K

0

200

298.15

30o

4o0

500

600

70o

800 30.634 21.080 83.256 56.906 14.522 65.104 800

= 820 30.749 21.694 84.014 57.558 15.135 65.556 820

...... ;;T;;; ...... ...... ;;S;; ...... ...... ;;T;;; ...... ....... ;;;---

900 30,146 24,943 87,841 60,117 18,384 67,414 900

1000 30.548 27.977 91.038 63.061 21.419 69.619 1000

fl 1041 30.713 29.233 92.269 64.187 22.675 70.487 1041

1100 37.000 39.416 101.994 66.161 32.858 72.125 1100 IZ00 37.000

1300 37.000

1400 37.000

1500 37.000

1600 57.000

1700 37.000

1800 37.000

1900 37.000

2000 37.000

2100 37.000

2200 37.000

2300 37.000

2400 37.000

2500 37.000

2600 37,000

2700 37.000

2800 37.000

2900 37.000

3000 37.000

3100 57.000

3200 37.000

3300 37,000

3400 37.000

3500 37.000

3600 37.000

3700 37.000

3800 37.000

3900 37.000

4000 37.000

4100 37.000

4200 37.000

4300 37.000

4400 37.000

4500 37.000

4600 37.000

4700 37.000

4800 37.000

_900 37.000

5000 57.000

5100 37.000

5200 37.000

5300 37.000

5400 37.000

5500 37.000

5600 57.000

5700 37,000

5800 37.000

5900 37.000

6000 37.000

43.116 105.213 69.283

46.816 108.175 72.162

50.516 110.917 74.834

5_.216 113.470 77.326

57,916 115.858 79.660

61.616 118.101 81.856

65.316 120.215 83.929

69.016 122.216 85.892

72.716 124.114 87.756

76.416 125.919 89.530

80.116 127.640 91.224

83.816 129.285 92.843

87.516 130.860 94.395

91.216 132.570 95.884

94,916 133,821 97,315

98.616 135,218 98.693

102.316 136.563 100.022

106.016 137,862 101.304

109.716 139.116 102.544

113._16 140.329 103.743

117.116 141.504 104.905

120.816 142.642 106.032

124.516 143.747 107.125

128.216 144.820 108,186

131.916 " 145.862 109.219

135.616 146.876 110,223

139.316 147.862 111.200

143.016 148.824 112.153

146.716 149.760 113.081

150.416 150.674 113.987

154.116 151.565 114.871

157.816 152.436 115.735

161.516 153.287 116.579

165.216 154.118 117.404

168.916 154.931 118.211

172.616 155.727 119.000

176.316 156.506 119.774

180.016 157.269 120.531

183.716 158.017 121.273

187.416 158.749 122.001

191.116 159.468 122.715

194.816 160.173 123.415

198.516 160.864 124.102

202.216 161.543 124.776

205.916 162.210 125.439

209.616 162.865 126.090

213.316 163.508 126,729

217.016 164.141 127.358

220.716 16_.762 127,976

36.558 74.748 1200

40.258 77.207 1300

43.958 79.518 1400

47.658 81.698 1500

51.358 83.759 1600

55.058 85.714 1700

58.758 87.572 1800

62.458 89.343 1900

66.158 91.035 2000

69.858 92.655 2100

73.558 94.205 2200

77.256 95.695 2300

80.958 97.127 2400

84,658 98.507 2500

88.358 99.838 2600

92.058 101.122 2700

95.758 102.364 2800

99.458 103.566 2900

103.158 104.730 3000

106.858 105.859 3100

110.558 106.955 3200

114.258 108.019 3300

117.958 109.054 3400

121.658 110.060 3500

125.358 111.040 3600

129.058 111.995 3700

132.758 112.926 3800

136.458 113.834 3900

1_0.158 114.721 _000

143.858 115,587 4100

147.558 116.433 4200

151.258 117.260 4300

154.958 118.069 4400

158.658 118.861 4500

162.358 119.656 4600

166.058 120.396 4700

169.758 121.140 4800

173.458 121.870 4900

177.158 122.585 5000

180.858 123.287 5100

184.558 125.976 5200

188.258 124.652 5300

191.958 125.516 5400

195.658 125.969 5500

199.358 126.610 5600

203.058 127.240 5700

206.758 127.860 5800

210.458 128.470 5900

214.158 129.070 6000

194 NASA/TP-3287/REV 1
TABLE IX.44. - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Ta(cr,I)

T C o H°(l')'H°(_ 8o(T) _GO(T).Ho(O)}K He(T) _oCD K T

K J_I-K _/mol J/moI-K J/mol-K _/m_ J/mol-K K

0 0.000 0.000 0.000 0,000 -5.681 INFINITE 0

200 24,082 3.246 31.582 I5.351 -2.435 43.756 200

298.15 25.295 5.681 41,471 22.417 0.000 41.471 298.15

300 25.308 5,728 41.628 22.535 0.047 41.471 300

400 25.850 8.287 48.986 28.269 2,606 42.471 400

500 26,347 10.897 54.808 33.014 5.216 44.376 500

600 26.830 13.556 59.655 37.061 7.875 46.530 600

700 27.219 16.260 65.822 40.594 10.579 48.709 700

800 27._74 18.995 67.474 43.730 13.314 50.831 800

900 27.653 21.752 70.721 46.552 16.071 52.864 900

1000 27,937 24.529 73.647 49.118 18.848 54.799 1000

1100 28.280 27.340 76.325 51._71 21.659 56.636 1100

1200 28.664 30.187 78.802 53.647 24.506 58.38I 1200

1300 28,991 33.070 81.110 55.671 27.389 60.041 1300

1400 29.198 35.981 83.267 57.566 30.500 61.624 1400

1500 29.317 38.907 85.286 59.348 33.226 63.135 1500

1600 29.445 41.845 87.182 61.029 36.164 64.579 1600

1700 29.691 44.800 88.973 62.620 39.119 65.962 1700

1800 30.113 _7.789 90.682 64.132 42.108 67.288 1800

t900 30.673 50.827 92.324 65.573 45.146 68.565 1900

2000 51.189 53.922 93.912 66.950 48.241 69.791 2000

2100 31.712 57.067 95.446 68.271 51.386 70.976 2100

2200 32.252 60.265 96.954 69.540 54.584 72.123 2200

2300 32.827 63.519 98,380 70.763 57.838 73.233 2300

2400 33.459 66.832 99.790 71.943 61.151 74.310 2400

2500 34.167 70.215 101.170 73,085 64.532 75.357 2500

2600 34.970 73.669 102.525 74.191 67.988 76.376 2600

2700 35.890 77.211 105,862 75.265 71.530 77.369 2700

2800 36,946 80.851 105.186 76.310 75.170 78.339 2800

2900 38.158 84.605 106.505 77.329 78.924 79.288 2900

3000 39.546 88.489 107.819 78,323 82.808 80.217 5000

• O 92 521 109 141 79 296 86 840 81.128 3100 3100 41 13 • • • " 4 82 025 3200 30 96 722 I10 475 80.249 91.0 1 • 8

3200 42.9 - " " 4 93 564 82.538 525

_. _258 _.080 V9.245 Ili.256 80.79 • ...........................

ZL_ZZ ........................................................... 8

. 13_ 813 122 480 80 794 130 132 82.538 525 e 3258 _ _ ,.-'_ _23"o16 81"528 i31_889 83.o5_ _R

3300 _l._u _J_ .... ;_'oL_ o_'=_7 _36 073 84.24_ _u_

3_o0 _18_o !9_ _;_ _;_ 140"257 85.405 35oo

3500 _1.8_0 _.v_o A_ ..........

3600 41.8_0 150.122 126.657 84.956 144.441 86.534 3600

3700 61.8G0 154.306 127.803 86.099 148.625 87.654 5700

3800 _1.840 158.490 128.919 87.211 152.809 88.706 3800

3900 _l 8_0 162.674 130.006 88.294 156.993 89.751 3900

_000 _.8_0 166.858 131.065 89.350 I61.177 90.771 4000

_lO0 _1 8;0 171.042 132.098 90.381 165.361 91.766 4100

_200 N_._0 175.226 133,106 91.386 169.545 92.759 4200

_300 *l 8_0 179.410 134.091 92.368 173,729 93.689 4300

_00 wl _0 183.59_ 135.053 93.327 177.913 9_.618 4_00

4500 _1 _q0 1_7.778 135.993 9_.265 182.097 95.527 4500

_600 _l 8_0 191.962 136.913 95.182 186.281 96.417 4600

4700 *_ _0 196.146 137,813 96.079 190.465 97.288 4700

480C _1 8_0 200,330 138.693 96.958 194.609 98.141 4800

_900 _1.8_0 204.514 139,556 97.818 198.833 98.978 4900

5000 _1.8_0 208.698 140.401 98.662 203.017 99.798 5000

5100 _1.8_0 212.882 141.230 99.488 207.201 100.602 5100

5200 _1._0 217.066 142.042 100.299 211.385 101.391 5200

5300 _1.8_0 221.250 142.839 101.094 215.569 102.166 5300

5400 _1.8_0 225.43_ 143.621 10_.87_ 219.753 102.926 5400

5500 _1.840 229.618 144.389 102.640 223.937 103.673 5500

5600 _1.840 233.802 145,143 103.593 228.121 104.407 5600

5700 _1.840 237.986 145.884 104.132 232.305 105.128 5700

5600 41.840 242.170 146.611 104.858 236.489 105.837 5800

5900 _1.840 246.354 147.327 105.572 240.673 106.534 5900

6000 41.840 250.538 148.030 106.273 244,857 107,220 6000

195

NASA/TP-3287/REV l
TABLE 1X.48. • THERMODYNAMIC FUNGTION$ FROM COEFFICIENTS FOR Th(=,_,

T C o H°O')'H°(_ S°O') _G°(T)'H°_))_ H°(r) _°('r}_ T

K J_-K kJ/mol J/mol-K NmoI-K _lmol NmoI-K K

0 0.000 0.000 0,000 0.000 -6.350 INFINITE 0

200 25.261 3.820 41.569 22.651 -2.530 56.201 200

298.15 26.230 6.350 51.830 30.532 0.000 "51.830 298.15

300 26,246 6.399 51.992 30.664 0.069 51.831 300

400 27.087 9.065 59,658 36.995 2.715 52.870 400

500 27.949 11.817 65.794 42.161 5.667 54.861 500

600 28.831 14.656 70.968 46.542 8.306 57.125 600

700 29.720 17.585 75.679 50,360 11.235 59.451 700

800 30.611 20.600 79.505 53,756 14,250 6].695 800

900 31.501 23.705 85.162 56.823 17.355 65.879 900

1000 32.392 26.900 86.527 59.627 20.550 65,977 1000

II00 33.285 50.184 89.656 62.217 23.834 67.989 II00

1200 34.175 35.556 92.590 66.627 27.206 69.918 1200

1500 55.069 37.019 95.361 66.885 30.669 71.770 1300

1400 35.964 40.570 97,993 69.016 34,220 73.550 1600

1500 36,860 66.211 100.505 71.050 37.861 75.266 1500

1600 37.752 47.942 102.912 72.968 61.592 76.917 1600

a 1650 38.196 49.861 104.081 75.874 43.491 77.722 1650

...... ;;7;;; ...... ..... ...... ;37;;; ...... ;;7;;; ...... ;;S;: ......

1700 36.017 55.127 107.268 74,861 48.777 78.576 1700

1800 57.212 58.788 109.360 76.700 52,438 80.228 1800

1900 38.407 62,569 111.604 78.675 56.219 81.815 ]900

2000 39.602 66.470 113.405 80.170 60,120 85.345 2000

B 2023 59.877 67.584 113.859 80.551 61.036 83.689 2023

...... ...... ;E:;; ..... ...... ;:7;;;...... ;;7;;; ...... ......

2100 66.000 8_.726 122,399 82.056 78.376 65.077 2100 2200 66.000

2300 66.000

2400 46.000

2500 46.000

2600 46.000

2700 66.000

2800 46.000

2900 46.000

3000 46.000

5100 66.000

3200 _6.000

3300 66.000

3400 66.000

3500 66.000

3600 46.000

3700 46.000

5800 46.000

3900 66.000

4000 46.000

6100 46.000

6200 66.000

6300 46.000

4400 46.000

6500 46.000

4600 46.000

4700 46.000

_800 46.000

4900 46.000

5000 46.000

5100 66.000

5200 46.000

5300 46,000

5600 _6,000

5500 66.000

5600 46.000

5700 46.000

5800 46.000

5900 46.000

6000 46.000

89.326 124.539 83.937

93.926 126.584 85.767

98.526 128.542 87.489

103.126 130.420 89.169

107.726 132.224 90.791

112,526 133.960 92.558

116.926 135,635 93.873

121.526 157.267 95.341

126.126 158.806 96.766

150.726 140.315 98.165

135.326 161.775 99,486

139.926 I_3.191 100.789

I_4.526 144,56_ 102.056

169.126 145.897 103.290

153.726 147.193 10_.692

158.326 148.654 105.663

162.926 149.680 106.805

167.526 150.875 107.920

172.126 152.060 109.008

176.726 153.176 110.072

181.326 154.28_ 111.111

185.926 155,367 112.128

190.526 156.626 115.125

195.126 157.658 116.097

199.726 158.469 115.050

204.326 159,658 115,985

208.926 160.427 116.900

213.526 161.375 117.798

218.126 162.504 118.679

222.726 163.215 119.544

227.326 164.109 120.592

231.926 164.985 121.225

236.526 165.845 122.044

261.126 166.689 122.848

245.726 167.518 123.638

250.326 168.332 124.615

254.926 169.132 125.179

259,526 169.918 125.931

266.126 170.691 126.670

82.976 86.823 2200

87,576 88.508 2300

92.176 90.135 2400

96.776 91.709 2500

101.576 95.255 2600

105.976 94.709 2700

110,576 96.141 2800

115.176 97.531 2900

119.776 98.881 3000

124.376 100.193 3100

128.976 101.470 3200

133.576 102.713 3300

138.176 103.924 3400

162.776 105.106 3500

167.376 106.255 3600

151.976 107.379 3700

156.576 108.476 3800

161.176 109.568 3900

165.776 110.596 6000

170.376 111.621 6100

17_.976 112.623 6200

179.576 113.605 4300

184.176 114.566 6600

188.776 115.508 6500

193.576 116.431 4600

197.976 117.336 4700

202.576 118.225 6800

207.176 119.096 _900

211,776 119,949 5000

216.376 120.789 5100

220.976 121.613 5200

225.576 122.623 5300

230.176 125.219 5600

234.776 126.002 5500

239.376 126.772 5600

243.976 125.529 5700

248.576 126.276 5800

253.176 127.007 5900

257.776 127.729 6000

196 NASA/TP-3287/REV 1
TABLE IX.46, - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR "1"l(0c,_, I0

T C o HoCI-).HO(_ _('r) _GO(-I').Ho(_}_ I._(T) _°(T) _ T

K J_ IcJ#.ol J/moI-K _moI-K _ J_oI-K K

0 0,000 0.000 0,000 0,000 -_.824 INFIt_ITE 0

200 22.303 2.479 21,217 8.822 -2.345 32.942 200

298.15 25,060 4.824 30.720 14,540 0.000 30,720 298.15

530 25.092 4.870 30.875 14.640 0.046 30.720 300

400 26.373 7,449 38.285 19.662 2.625 31.722 400

500 27.363 10.136 44.277 24.005 5.312 33.653 500

600 28.412 12.924 49.357 27.817 8.100 35.857 600

700 29.506 15.820 53.819 31.219 10.996 38.110 700

800 30.461 18.821 57,825 34.299 13.997 40.329 800

900 31.001 21,899 61.449 37.1,17 17,075 42.477 900

1000 32,682 25.045 64.763 39.718 20.221 44.542 1000

ii00 39.222 28.597 68.144 42.146 23,773 46.531 1100

1156 45.189 30.953 70.231 43.455 26.129 47.628 1156

-; - 34.753 73.51; "

1200 28_566 35.997 74.574 44.577 31.17_ 48.597 1200

1300 29.953 38.922 76.915 46.975 34.098 50.686 1300

1400 31._03 41.990 79.187 49.195 37.166 52.641 1400

1500 32.916 45.205 81._05 51.269 40.381 54.485 1500

1600 34._9_ 48.575 83.580 53.220 43.751 56.235 1600

1700 36.136 52.106 85.720 55.069 47.282 57.907 1700

1800 37.842 55.804 87,833 56.831 50.980 59.511 1800

1900 39.611 59.676 89.926 58.518 54.852 61.057 1900

1944 40.409 61.437 90.842 59.259 56.613 61.720 1944

............. ...... ...... ...... ...... ...... 6[ 72;......

1944 • " " 62 765 2000

200D 46.800 78.657 99.682 60.353 73.835 .

2100 46.800 83.337 101.965 62.280 78.513 64.578 2100

2200 46.800 88.017 104.142 64.134 85.193 66.327 2200

2300 46.800 92.697 106.222 65.919 87.873 65.017 2300

2400 46.800 97.377 108.214 67.640 92.553 69.650 2400

2500 46.800 102.057 110.125 69.302 97.233 71.231 2500

2600 46.800 106.757 111.960 70.907 101.913 72.763 2600

2700 46.800 111,417 113.726 72.461 106.593 74.247 2700

2800 46.800 116.097 115.429 73.965 111.273 75.688 2800

2900 46.800 120.777 117.071 75.425 115.955 77.087 2900

3000 _6.800 125.457 118.657 76.838 120.633 78._46 3000

3100 46.800 130.1_7 120.192 78.212 125.513 79.768 3100

3Z00 46.800 134.817 121.678 79.547 129.993 81.055 3200

3300 46.800 139.497 123.118 80.846 134.673 82,308 5300

3_00 46.800 14_,177 124.515 82,110 139,353 83.529 3400

3500 46.800 148.857 125.872 83.341 144,033 84.719 3500

3600 46.800 153.537 127.190 84.5_1 148.713 85.881 3600

3700 46.800 158.217 128.472 85.711 153.393 87.015 3700

380D 46.800 162.897 129.720 86.853 158.075 88,122 3800

3900 46.800 167.577 130.936 87.967 162.753 89.204 3900

4000 46.800 172.257 132.121 89.057 167.433 90.263 4000

4100 46.800 176.937 133.277 90.121 172.113 91.298 4100

_200 46.800 181.617 134,404 91.162 176.793 92.311 _200

4300 46.800 186.297 135.505 92.181 181.473 93.302 4300

4400 46.800 190.977 136.581 93.177 186,153 94.27_ 4400

4500 _6.800 195.657 137.633 94.154 190.833 95.226 4500

4600 46.800 200.337 130.662 95.110 195.51_ 96.159 4600

4700 46.800 205.017 139.668 96.048 200.193 97.074 4700

4800 46.800 209.697 140.654 96.967 204.873 97.972 4800

_900 46.800 214.377 141.619 97.868 209.553 98.853 4900

5000 46.800 219.057 142.56_ 98.753 214.233 99.717 5000

5100 46.800 223.737 143,491 99.621 218.913 100.567 5100

5200 46_800 228.417 144,400 100.473 223,593 101._01 5200

5300 46.800 233,097 145.291 101.310 228.273 102.221 5300

5400 46.800 237.777 146.166 102,133 232.953 103.026 5400

5500 46.800 242.457 147.025 102.9_1 237.633 103,818 5500

5600 46.800 247.137 147.868 103.736 242.313 104.598 5600

5700 46.800 251.817 148.696 104.518 246.993 105.364 5700

5800 46.800 256.497 I_9.510 105.286 251.673 106.118 5800

5900 46.800 261.177 150.310 106.043 256,353 106,860 5900

6000 46.800 265.857 151.097 106.787 261,033 107.591 6000

197

NASA/TP-3287/REV l
TABLE IX.47. • THERMODYNAMIC FUNCTIONS FROM COEFF CENTS FOR U(a,l_,'v,_)

T G o Ha(.T).HO(0) SO(T )

K Jlm_t-K _lmol JlmoI-K

0 0.000 0,000 0.000

200 25.835 3.738 39,542

298.15 27.665 6.364 50.200

300 27.700 6.415 50.371

400 29.688 9.283 58.607

500 31.968 ]2.362 65.470

600 34.659 ]5.690 71.529

700 37.857 19.311 77.105

800 41.614 23.280 82.399

_GO(T')'H°(0)) K H°('l') _°('T)_ T

J/moi-K kJ/m_ JlmoI-K K

O. 000 -6.364 INFINITE 0

20.851 -2.626 52.671 200

28,855 0,000 50,200 298

26.967 0.051 50.201 300

35.400 2.919 51.310 400

40.745 5.998 53.473 500

45.379 9.326 55.986 600

49,517 12,947 58.609 700

53.299 16.916 61.254 800

,I5

900 45.924 27.653 87.544 56.819 21.289 63.890 900

942 47,884 29.622 B9.683 58.237 23.258 64.992 942

............................................................................................

942 42.400 32.402 92.634 58.237 26.038 64.992 942

1000 42.400 34.861 95,167 60.306 28,497 66,670 1000

1049 42.400 36.939 97.196 61.982 30.575 68.049 1049

............................................................................................

7 1049 38.300 41.669 101.705 61.982 35.305 68.049 1049

1100 38.300 43.622 103.523 63.866 37.258 69.652 1100

1200 38.500 47.452 106.855 67.312 41.088 72.615 1200

1300 38.300 51.282 109,921 70.473 44.918 75.368 1300

1400 38.300 55.112 112.759 73.393 48.748 77.939 1400

7 1408 58.300 55.419 112.978 75.618 49.055 78.158 1408

............................................................................................

1408 47.739 64.139 119.171 73.618 57.775 78.138 1408

1500 47.914 68.559 122.198 76.505 62.175 80.748 1500

1600 48.126 73.340 125.297 79.459 66.976 83.436 1600

1700 48.357 78.164 128.221 82.242 71.800 85.986 1700

1800 48.602 83.012 130.992 84.874 76.648 88.410 ]800

1900 48.859 87.885 133.627 87.371 81.521 90.721 1900

2000 49.126 92.785 136.140 89.747 86.421 92.929 2000

2100 49.401 97.711 138.543 92.014 91.347 95.045 2100

2200 _9.683 10Z.665 140.848 94.182 96.301 97.075 2200

2300 49.969 ]07.648 143.063 96.259 101.284 99.026 2300

2400 50.261 112.659 145.195 98.254 106.295 100.906 2400

2500 50.556 117.700 147.253 100.173 111.336 102.719 2500

2600 50.854 122.770 149.242 102.022 116.406 104.470 2600

2700 51.155 127.871 151.167 103.807 121.507 106.164 2700

2800 51.458 133.001 153.032 105.532 126,637 107.805 2800

2900 51.763 138.162 154.843 107.201 131.798 109.396 2900

3000 52.070 143.354 156,60_ 108.819 136.990 110.940 3000

3100 52.379 148.577 158.316 110.388 142.213 112.441 3100

3200 52.689 153.830 159.984 111.912 147,466 113.901 3200

3300 53.000 159.114 161.610 113.393 152.750 115.322 3300

3400 53.312 164.430 163.197 114.835 158,066 116.707 3400

3500 53.625 169.777 164.747 116.239 163.413 118.057 3500

3600 53.939 175.155 166.262 117.607 168.791 119.375 3600

5700 5_.254 180.565 167.744 118.943 174.201 120.663 3700

3800 54.569 186.006 169,195 120.246 179.642 121,921 3800

3900 54.855 191.479 170.616 121.519 185.115 123.151 3900

4000 55.201 196.983 172.010 122.76q 190.619 124.$55 4000

198 NASA/TP-3287/REV 1
TABLE IX.48, - THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR V(or,l)

T C° HO(T)._(_ _(T) tGO(T).Ho(_)K PP(T) _°(13n T

K J_-K _hnol J_oI-K Nmot-K IcI/mot J/moI-K K

0 0.000 0.000 0.000 0.000 -_.640 INFINITE 0

200 21.677 2.326 19.563 7.933 -2.314 31.133 200

298.15 24.896 4.640 28.936 13.373 0.000 28.936 298.15

300 24.931 4.686 29.090 13.470 0.046 28.936 300

400 26.216 7.251 56.461 18.355 2.611 29.933 400

500 26.942 9,912 42.595 22.571 5,272 31.851 500

600 27.489 12.655 47.356 26.300 7.993 34.053 600

700 28.028 15.408 51.631 29.620 10,768 36.249 700

800 28.672 18.242 55.415 32.612 15.602 38.412 800

900 29.555 21.145 58.831 35.339 16.505 40.494 900

i000 30.088 24.115 61.961 37,846 19.475 42.486 I000

I100 30.892 27.163 64.866 40.172 22.525 44.590 1100

1200 31.778 50.296 67.591 42.345 25.656 46.211 1200

1300 32.750 33.522 70.175 44.387 28.882 47,956 1300

1400 35.805 36.849 72.658 ,46.317 32.209 49.632 1400

1500 54.809 40.279 75.004 48,152 35.659 51.245 1500

1600 35.867 43.812 77.284 49.902 59.172 52.802 1600

1700 37.005 47.455 79.692 51.578 42.815 54,307 1700

1800 38.226 51.216 81.642 53.188 66.576 55.766 1800

1900 59.526 55.105 83.745 54.741 50.463 57.183 1900

2000 40.918 59.124 85.805 56.243 54.484 58.565 2000

0 42 472 65 292 87.838 57.699 58.652 59.909 ZlO0

_._ _'16n A7"187 89.654 58.975 62.547 61.094 2190

................... ..... 58975 85392 61094 2190 , 2190 .... 85854 61272 2200 2200 46204 90.494 100.296 59.165 • •

2300 66.204 95.114 102.350 60.996 90.474 63.013 2300

2400 06.204 99.755 104.517 62.7&0 95.095 64,694 2400

2500 46.204 104.355 106.205 64.461 99,715 66,517 2500

2600 46.204 108.976 108.015 66.101 104.336 67,886 2600

2700 46.204 113.596 109.759 67.686 108.956 69,405 2700

2800 46.204 118.216 IiI._39 69.219 113.576 70.876 2800

2900 46.204 122.837 113.060 70.703 118.197 72.303 2900

3000 46.204 127.457 114.627 72.161 122.817 73.688 5000

3100 66.204 132.078 116,1_2 73.536 127.438 75.033 3100

3200 46.204 136.698 117.609 74.890 152.058 76.340 3200

5300 46.204 141.318 119.030 76.207 136.678 77.613 5_00

3400 46.204 145.939 120.410 77.487 141.299 78.851 3400

3500 46.20_ 150.559 121.749 78.752 145.919 80.058 5500

3600 46.204 155.180 123.051 79.945 150.5_0 81.234 5600

3700 66.204 159.800 124.517 81.127 155.160 82.381 5700

3800 46.204 164.620 125.569 82.280 159.780 83.501 5800

5900 66.204 169.041 126.749 83.405 164.401 8_,595 3900

6000 46.204 173.661 127.919 84.505 169.021 85.663 6000

4100 46.20_ 178.282 129.060 85.576 173.642 86.708 4100

4200 46.204 182.902 130.173 86.625 178.262 87.730 _Z00

4300 66.204 187.522 131.260 87.650 182.882 88.729 4300

4400 46,204 192.143 132.522 88.654 187.503 89.708 4400

4500 46.204 196.765 135.561 89.636 192.123 90.667 6500

4600 46.204 201.386 134.576 90.597 196.744 91.606 4600

4700 46.204 206.00_ 135.370 91.539 201.364 92.527 6700

4800 66.204 210.624 136.343 92.465 205.984 93.429 4800

4900 46.204 215.245 137.295 95.568 210.605 94.315 4900

5000 46.204 219.865 138.229 94.256 215.225 95.184 5000

5100 46.204 224.486 139.164 95.127 219,846 96.057 5100

5200 46.204 229.106 140.061 95.982 224.466 96.874 5200

5500 46.204 253.726 160.921 96.822 229.086 97.697 5300

5400 46.204 238.367 141.785 97.646 233.707 98.506 5400

5500 46.204 242.967 142.633 98.057 238.327 99.500 5500

5600 46.204 247.588 1_3.465 99.253 242.948 100.082 5600

5700 46.204 252.208 144.283 100.056 247.568 100.850 5700

5800 46.204 256.828 145.086 100.806 252.188 101.606 5800

5900 46.204 261.449 145.876 101.563 256.809 102.349 5900

6000 46.204 266.069 146.653 102.308 261.429 105.081 6000

NASA/rP-3287/REV 1 199
TABLE _.4,g. - THERMODYNAMIC FUNCTION8 FROM COEFFICIENTS FOR W(_,_

T C o H°(T)'H°(_ S°(T) _G°(T)'Ho(O)}_ H°(T) _°(T)ff T

K J/rn_bK kJJmol JtmoI.K J_oI-K _ol _moI-K K

0 01000 0.000 0.000 0.000 -4.973 INFINITE 0

200 22._84 2,656 23.265 9.976 -2.315 34.841 ZOO

298.15 24.295 _.973 32,660 15.980 0.000 32.660 298.15

300 24.312 5.018 32.810 16.084 0.045 52.660 300

400 24.923 7.483 59.898 21.190 2.510 33.623 400

500 25.352 9.997 65.506 25,512 5.026 35.458 500

600 25.785 12.554 50.167 29.263 7.581 37.532 600

700 26.233 15.155 56.175 32.525 i0.182 39.630 700

800 26.673 17.800 57.707 35.656 12.827 _1.673 800

900 27.105 20.489 60.873 38.108 15.516 63.633 900

1000 27.566 23.222 63.75Z 60.530 18.249 65.503 1000

1100 28.013 26.001 66.400 42.763 21.028 67.284 1100

1200 28.669 28.825 68.857 46.837 23.852 68.981 1200

1300 28.929 31.695 71.154 46.776 26.722 50.599 1300

1400 29.393 36.611 73.315 48.595 29.638 52.145 1400

1500 29.860 37.574 75.359 50,310 32.601 53.625 1500

1600 30.331 40.583 77.301 51,937 35.610 55.045 1600

1700 30.805 43.640 79.154 53.484 38.667 56.409 1700

1800 31.28_ 66.764 80.929 5_.959 41.771 57.722 1800

1900 31.767 69.897 81.633 56.371 64.926 58.989 1900

2000 32.253 53,098 84,275 57.726 48.125 60.212 2000

2100 32.743 56.348 85.860 59.028 51.375 61.396 2100

2200 33.237 59.647 87.395 60.283 54.674 62.543 2200

2300 33.736 62.995 88.883 61.694 58.022 63.656 2300

2400 34.236 66.393 90.329 62.665 61.420 64.738 2600

2500 34.737 69.842 91.737 63.800 64.869 65.789 2500

2600 35.245 73.341 93.109 66.901 68.368 66.814 2600

2700 36.180 76.908 96.455 65.971 71,935 67.813 2700

2800 37.678 80.589 95.796 67.01Z 75,616 68.788 2800

2900 39.073 84.416 97.136 68.028 79.441 69.743 2900

3000 41,042 88.416 98.493 69.021 83.443 70.678 3000

3100 43.413 92.635 99.876 69.994 87,662 71.598 3100

3200 46.027 97.107 101.295 70.969 92.134 72.503 3200

3300 48.966 101.857 102.757 71.891 96.884 73.398 3300

3400 52.270 106.913 104.266 72.821 101.940 74,284 3600

3500 56.515 112.343 105.840 73.742 107.370 75.162 3500

3600 61.696 11B,2_8 107.503 7_.656 113.275 76.037 3600

cr 3680 66.154 123,361 108.907 75.385 118.388 76,737 3680

3680 35.564 158.758 118,526 75,385 153,785 76.737 3680

3700 35.564 159.470 118,719 75.619 154.497 76.963 3700

3800 35.566 163.026 119.667 76.766 158.053 78.074 3800

3900 35.564 166.583 120.591 77.878 161.610 79,153 3900

4000 35.564 170.139 121.492 78.957 165.166 80.200 4000

4100 35.566 173.695 122.370 80.005 168,722 81.218 4100

4200 35.56_ 177.252 123.227 81.024 172.279 82.208 4200

4300 35.564 180.808 124.064 82.015 175.835 83.172 4300

4400 35.566 184.365 124.881 82.980 179.392 86.110 4400

4500 35.564 187.921 125.680 83.920 182.968 85.025 6500

4600 35.566 191.477 126.662 84.837 186.504 85.918 4600

6700 35.566 195.034 127.227 85.730 190.061 86.788 4700

4800 35.566 198.590 127.976 86.603 193.617 87.639 4800

4900 35.566 202.167 128.709 87.455 197.174 88.469 4900

5000 35.564 205.703 129.427 88.287 200.730 89.281 5000

5100 35.566 209.259 130.L32 89.100 20_.286 90.076 5100

5200 35.564 212.816 130.822 89.896 207.843 90.853 5200

5300 35.564 216.372 131.500 90.675 211.399 91.613 5300

5400 35.564 219.929 132.16_ 91.437 214.956 92.358 5400

5500 35.564 223.485 132.817 92,183 218.512 95.088 5500

5600 35.564 227,041 133.458 92.915 222.068 93.803 5600

5700 35.56_ 230.598 136.087 93.632 225.625 94.504 5700

5800 35.564 234.154 13_.706 9_.336 229.181 95.192 5800

5900 35,564 237.711 135.314 95.024 232.738 95.867 5900

6000 35.564 261.267 135.912 95.700 236.294 96.529 6000

200 NASA/TP-3287/REV 1
TABLE IX.50. - THERMODYNAMIC FUNCTION8 FROM COEFFICIENTS FOR Xe

T C_ H°(T)'H°_) S°(T) "(G°_'PP_))ff H°(T) _°CqK

K JIm_l-K kJ/mol J_oFK NmoI-K _hnol _moI-K

0 0.000 0.000 0.000 0.000 -6.197 INFINITE

200 20.786 4.157 161.586 140.600 -2.040 171.587

298,15 20.786 6.197 169.686 1_8,900 0.000 169.686

300 20.786 6.256 169.815 149.028 0.038 169.686

400 20.786 6.315 175.794 155.008 2.117 170.502

500 20.786 10,393 180.433 159.646 4.196 172.041

600 20,786 12.472 184.222 163.436 6,274 173.765

700 20.786 14.550 187.427 166.640 8.353 175.494

800 20.786 16.629 190.202 169.416 10.432 177,163

900 20.786 18.708 192.651 171.864 12.510 178.750

1000 20.786 20.786 194.841 174.054 14.589 180.252

1100 20.786 22.865 196,822 176,036 16.667 181.670

1200 20,786 24.944 198.630 177.844 18.746 183.009

1300 20.786 27,022 200,294 179.508 20,825 184.275

1_00 20.786 29.101 201.835 181.048 22.903 185.475

1500 20.786 31.179 203.269 182.482 24.982 186.614

1600 20.786 33.258 204,610 183.824 27.061 187.697

1700 20,786 35.337 205.870 185.084 29.139 188.730

1800 20,786 37.415 207.059 186.272 31.218 189.715

1900 20.786 39.494 208.182 187.396 33.296 190.658

2000 20.786 41,573 209.249 188.462 35.375 191.561

2100 20.786 43,651 210.263 189.476 37.454 192.428

2200 20.786 45.730 211.230 190.443 39.532 193.260

2300 20.786 47.808 212.154 191.367 41,611 194.062

2400 20,786 49.887 213.038 192.252 43.690 194.834

2500 20.786 51.966 213.887 193.101 45.768 195,580

2600 20.786 54.044 214.702 193.916 47.847 196.300

2700 20.786 56.123 215.487 194.700 49.926 196.996

2800 20.786 58.202 216.243 195.456 52.004 197.670

2900 20.786 60.280 216.972 196.186 54.083 198.323

3000 20.786 62,359 217.677 196.890 56.161 198.956

3100 20.786 64.437 218.358 197.572 58.240 199,571

3200 20.786 66.516 219.018 198.232 60.319 200,169

3300 20.786 68.595 219.658 198.872 62.597 200.750

3400 20.786 70.673 220.278 199.492 64.476 201.315

3500 20.786 72.752 220.881 200.095 66.555 201.865

3600 20.786 74.831 221.466 200.680 68.633 202.402

3700 20.786 76.909 222.036 201.250 70.712 202.925

3800 20.786 78.988 222.590 201.804 72.790 203.435

3900 20.786 81.066 223.130 202.344 74.869 203.933

4000 20.786 83.145 223.657 202.870 76,948 204.420

4100 20.786 85.224 224.170 203.384 79.026 204.895

4200 20.786 87.302 224.671 203.884 81.105 205.360

4300 20.786 89.381 225.160 204.374 83.184 205.815

4400 20.786 91.460 225.638 204.851 85.262 206.260

4500 20.786 93.538 226.105 205.319 87.341 206,696

4600 20.786 95.617 226.562 205.775 89.419 207.123

4700 20.786 97.695 227.009 206.222 91._98 207.541

4800 20.786 99.774 227.446 206.660 93.577 207.951

4900 20.786 101.&53 227.875 207.089 95.655 208.353

5000 20.786 103.931 228.295 207,509 97,734 208.748

5100 20,786 106.010 228.706 207.920 99.813 209.135

5200 20.786 108.089 229.110 208.324 101.891 209.516

5_00 20.786 110.167 229.506 208.720 103.970 209.889

5400 20,786 112.246 229.895 209.108 106.048 210,256

5500 20.786 114.325 230.276 209.490 108.127 210.617

5600 20.787 116.403 230.651 209.864 110.206 210.971

5700 20,787 118.482 251.018 210.232 112.284 211.319

5800 20.787 120.561 231.380 210.594 114.363 211.662

5900 20.787 122.639 231.735 210.949 116.442 211.999

6000 20.787 124.718 232.085 211.298 118.520 212.331

6200 20.589 128.853 232.763 211.980 122.655 212.979

6400 20.525 132.962 233._15 212.640 126.765 213.608

6600 20.547 137.069 234.047 213.279 130.871 214.218

6800 20.619 141.185 234.661 213.899 134.987 214.810

7000 20,714 145.318 235.260 214.500 139.120 215.386

7200 20.815 149.471 235.845 215.085 143,273 215.946

7400 20.909 153.643 236.417 215.654 147._46 216.492

7600 20.989 157.833 236.975 216.208 151.636 217.023

7800 21.051 162.037 237.521 216.747 155.840 217.542

8000 21.097 166.253 238,055 217.273 160,055 218.048

T

K

0

200

298.15

300

400

500

6O0

700

80O

900

1000

1100

1200

1300

1400

1500

1600

1700

1800

1900

2000

2100

2200

2300

2400

2500

2600

2700

2800

2900

3000

3100

3200

3300

3400

3500

3600

3700

3800

3900

4000

4100

4200

4300

4400

4500

_600

4700

4800

4900

5000

5100

5200

5300

5400

5500

5600

5700

5800

5900

6000

6200

6400

6600

6800

7000

7200

7400

7600

7800

8000

NASA/TP-3287/REV l 201
T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

II000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

170O0

17500

18000

18500

19000

19500

20000

C o

J_K

21. 127

21.147

21.161

21.176

21.200

Z1 .ZqO

21.305

21.402

21. 540

21.727

22.457

23.652

25.402

27.779

30.827

34.565

38.983

44. 043

49.678

55.792

62,260

68.927

75.608

82.091

88,132

93.461

97.774

1o0.743

102.007

101.178

TABLE I)(.50. - Conduded.

H°(T)-H°(0} S°(T) -(G°(T)oH°(0)}_ H°('l") -G°(T)_

KJ/mol J_oI-K _mol-K k.J/m_ J/moI-K

170.475 238.576 217.787 164.278 218.543

174.703 239.086 218.288 168.505 219.026

178.933 239.584 218.777 172.736 219.498

183.167 240.070 219.256 176.970 219.960

187.405 240.5_6 219.724 181.207 220.412

191.648 241.013 220.1B1 185.451 220.855

195.902 241.470 220.629 189.705 221.289

200.172 241.920 221.068 193,975 221,714

204.466 242.362 221.498 198.268 222.131

208.792 242.799 221.920 202.594 222.540

219.821 243.875 222.940 213.623 223.530

231.326 244.946 223.916 225.129 224,479

243.565 246.033 224.854 237.368 225.393

256.833 247.162 225.760 250.636 226.276

271.456 248.356 226.639 265.259 227.135

287.776 249.635 227.499 281.578 227.976

306.135 251.021 228.344 299.937 228.803

326,866 252.528 229.180 320.668 229.623

350.274 254.170 230.013 344.077 230.441

376.624 255.956 230.848 370.427 231.261

406.125 257.890 231.689 399.928 232.089

438.917 259.972 232.540 432.720 232.927

475.055 262.195 233.404 468.857 233.780

514.493 264.550 234.285 508.295 234.650

557.072 267.018 Z35.185 550.875 235.539

602,506 269.577 236.105 596.309 236.449

650.364 272.200 237.045 644.167 237.380

700.056 274.850 238.005 693.859 238.331

750.823 277.487 238.983 744.625 239.301

801.715 280.064 239.978 795.517 240.288

T

K

8200

8400

8600

8800

9000

9200

9400

9600

9800

10000

10500

11000

11500

12000

12500

13000

13500

14000

14500

15000

15500

16000

16500

17000

17500

18000

18500

19000

19500

20000

202 NASA/TP-3287/REV 1
TABLE IX.51. • THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Zn(¢r,0

T C o HO(T).HO(O) SO(T) _GO(.I-).Ho(O))/T HO(T) _O(T)/T T

K Nm_I-K _/rr_ J_oI-K NmoI-K _/mol J/moI-K K

0 0.000 0.000 0,000 0.000 -5.657 INFINITE 0

200 24.050 3.233 31.790 15.623 -2.424 43.908 200

296,15 25.390 5.657 41.630 22.656 0.000 41.630 298.15

300 25.411 5.704 41.787 22.774 0.047 41.630 300

400 26.224 8.288 49.217 28,496 2.631 42.638 400

500 27.220 10.956 55.165 33.253 5.299 44.567 500

.820 13 753 60 260 37 339 8 096 46.767 600 600 28 ' ' " "86 48 863 692.73

_ (.qp 7_ 30 975 16.519 64.543 _0.697 10. 2 • _ ..........

:___:_+_--:_.... __"............................................... -........... _.....

,, i .3 0 73

800 31,400 27.187 79.602 45.618 21.530 52.689 800

900 31.400 30.327 83.300 49.603 24.670 55.889 900

1000 31.400 33.467 86.609 53.141 27.810 58.798 1000

1100 31.400 36.607 89.601 56,322 30.950 61.465 I100

1200 31.400 39.747 92.334 59.211 34.090 63.925 ]200

1300 31._00 42.887 94.847 61.857 37.230 66.208 1300

1400 31.400 46.027 97.174 6_.297 40.370 68.338 1_00

1500 31,400 49.167 99.340 66.562 43.510 70.333 1500

1600 31.400 52.307 101.367 68.675 46.650 72.210 1600

1700 31.400 55.447 103.270 70.654 49.790 73.982 1700

1800 31.400 58.587 105.065 72.517 52.930 75.659 1800

1900 31.400 61.727 106.763 74.275 56.070 77.252 1900

2000 31.400 64.867 108.373 75.940 59.210 78.768 2000

2100 31.400 68.007 109.905 77.521 62.350 80.215 2100

2200 31.400 71.147 111.366 79.027 65.490 81.598 2200

2300 31.400 74.287 112.762 80.463 68.630 82.923 2300

2400 31.400 77.427 114.098 81.837 71.770 84.194 2400

2500 31.400 80.567 115.380 83.153 74.910 85.416 2500

2600 31.400 83.707 116.612 84.417 78.050 86.592 2600

2700 31.400 86.847 117.797 85.631 81.190 87.726 2700

2800 31.400 89.987 118.939 86.800 84.330 88.821 2800

7900 31.400 93.127 120.041 87.928 87.470 89.878 2900

3000 31.400 96.267 121.105 89.016 90.610 90.902 3000

3100 31.400 99.407 122.135 90.068 93.750 91.893 3100

3200 31.400 102.547 123.132 91.086 96.890 92.853 3200

3300 31.400 105.687 124.098 92.071 100.030 93.786 3300

3400 31.400 108.827 125.035 93.027 103.170 9_.691 5400

3500 31,400 111.967 125.945 93.955 106.310 95.571 3500

3600 31.400 115.107 126.830 94.856 109.450 96.427 3600

3700 31.400 118.247 127.690 95.732 112.590 97.260 3700

3800 31.400 121.387 128,528 96.584 115.730 98.072 3800

3900 31.400 124.527 129.343 97.413 118.870 98.864 3900

_000 31.400 127.667 130.138 98.221 122.010 99.636 4000

GIO0 31.400 130.807 130.914 99.009 125.150 100.389 4100

4200 31._00 133.947 131.670 99.778 128.290 101.125 4200

_300 31.400 137.087 132.409 100.528 131.430 101.844 4300

4400 31._00 140.227 133.131 101.261 13_.570 102.547 4400

4500 31.400 143.367 133.837 101.977 137.710 103.234 4500

4600 31.400 146.507 134.527 102.677 140.850 103.907 4600

_700 31.400 149.647 135.202 103.362 143.990 104.566 4700

_800 31.400 152.787 135,863 104.033 147,130 105.211 4800

4900 31.q00 155,927 136,511 104.689 150.270 105.843 4900

5000 31._00 159.067 137.145 105.332 153.q10 106.463 5000

5100 31.400 162.207 137.767 105.961 156.550 107.071 5100

5200 31._00 165.347 138.377 106.579 159.690 107.667 5200

5300 31.400 168.467 158.975 107.185 162.850 108.252 5300

5400 31.400 171.627 139.562 107.779 165.970 108.826 5400

5500 31.400 174.767 lq0.138 108.362 169.110 109,390 5500

5600 31.400 177.907 140.704 108.934 172.250 109,945 5600

5700 31.400 181.047 141.259 109.497 175.390 110.489 5700

5800 31.400 184.187 141.805 110.049 178.530 111.024 5800

5900 31.400 187.327 142.342 110.592 181.670 111.551 5900

6000 31.400 190.467 142.870 111.125 184.810 112.068 6000

203

NASA/TP-3287/REV I
TABLE 1X.52.- THERMODYNAMIC FUNCTIONS FROM COEFFICIENTS FOR Zr(a,lS,0

T C = H%f')-I-_(O) S°(T) _G°O')'Ho(O)}K H°(T) _°(T')K T

K J/m_FK _ol Jlmol_ J/moI.K _ J/moI-K K

0 0.000 0.000 0.000 0.000 -5.497 INFINITE 0

200 23.871 3.079 29.048 13.655 -2,418 41.1_0 200

298.15 25.202 5.697 38.869 20.432 0.000 38.869 298.15

300 25.218 5.544 39.025 20.546 0.047 38.869 300

400 25.937 8.103 46.384 26.125 2.606 39.868 400

500 26.572 10.729 52.239 30.782 5.232 41.776 500

600 27.262 13.420 57.144 34.778 7.923 43,939 600

700 28.058 16.185 61.404 38.283 10.688 46.136 700

800 28.973 19.035 65.209 41.415 13.538 48.287 800

900 30.002 21.983 68.680 44,255 16.486 50.362 900

1000 31.125 25.039 71,099 46.860 19.542 52.357 1000

1100 32.306 28.210 74.920 49.275 22.713 54,272 1100

e 1135 32.725 29.548 75.939 50.081 23.851 54.925 1135

1135 28.329 33.365 79.478 50.081 27.868 54.925 1135

1200 28.511 35.212 81.060 51.717 29.715 56.298 1200

1300 28.879 38.081 83.356 54.063 32.584 58.292 1300

1400 29.353 40.991 85.513 56.234 35.494 60.160 1400

1500 29.934 43.955 87.558 58.254 38.458 61.919 1500

1600 30.621 46.982 89.511 60.147 41.485 63,583 1600

1700 31.414 50.083 91.390 61.930 44.586 65.164 1700

1800 32.314 53.268 95.211 65.618 _7.771 66.671 1800

1900 33.320 56.549 94.985 65.222 51.052 68.115 1900

2000 34._33 59.936 96.722 66.75_ 54.439 69.502 2000

2100 35,651 63.439 98,431 68.221 57,942 70.839 2100

# 2125 35.973 64,334 98.854 68,579 58,837 71.166 2125

t 2125 41.8_0 85.254 108.699 68.579 79.757 71.166 2125

2200 41.840 88.592 110.150 69.972 82.895 72.471 2200

2300 41.840 92.576 112.010 71.760 87.079 74.150 2300

2400 41.840 96.760 113.791 73.474 91.263 75.764 2400

2500 _1,840 100.944 115._99 75.121 95.447 77.320 2500

2600 4[.840 105.128 117.140 76.706 99.631 78,820 2600

2700 41.840 109.312 118.719 78.233 103.815 80.269 2700

2800 41.840 113,496 120.241 79.706 107.999 81.669 2800

2900 41,840 117.680 121.709 81.129 112.183 83.025 2900

3000 _1.840 121.864 123.127 82.506 116.367 84.338 3000

3100 _1,840 126.048 124.499 83.838 120.551 85.612 3100

3200 _1.840 130.232 125.828 85.130 124.735 86.848 3200

3300 41.840 134.416 127.115 86.383 128.919 88.049 3300

3400 41.840 138.600 128.364 87.599 133.103 89.216 3400

3500 41.840 142.784 129.577 88.781 137.287 90.352 3500

3600 41.840 146.968 130,756 89.931 141.471 91.458 3600

3700 41.840 151.152 131.902 91.050 145.655 92.536 3700

3800 41.840 155.336 133.018 92.140 149.839 93.586 3800

3900 41,840 159.520 134.105 93.202 154.023 94.611 3900

4000 41.840 163.704 135.164 94.238 158.207 95.612 4000

4100 41.840 167.888 136.197 95.249 162.391 96.589 4100

_200 41.840 172.072 137.205 96.236 166.575 97.544 4200

4300 41,840 176.256 138.190 97.200 170.759 98.478 4300

4400 41.840 180.440 139.152 98.142 174.943 99.392 4400

4500 41.840 18_.62_ 1_0.092 99.064 179.127 100.286 4500

4600 41.840 188.808 141.011 99.966 183.311 101.161 4600

4700 41.840 192.992 141.911 100.849 187.495 102.019 4700

4800 41.840 197.176 142.792 101.714 191.679 102.859 4800

4900 41.840 201.360 143.655 102.561 195.863 103.683 4900

5000 41.840 205.544 144.500 103.391 200.047 104.491 5000

5100 41.840 209.728 145.329 ]04.205 204.231 105.283 5100

5200 41.840 213.912 146.141 105.004 208.615 106.061 5200

5300 41.840 218.096 146.938 105.788 212.599 I06.825 5300

5_00 41.840 222.280 147.720 106.557 216.783 107,575 5400

5500 41.8_0 226._64 148.488 107.313 220.967 108.312 5500

5600 41.840 230.648 149.242 108.055 225.151 109.036 5600

5700 41,840 234.832 149.982 108.784 229.335 109.748 5700

5800 41.840 239.016 150.710 109.500 233.519 110.448 5800

5900 41.840 2_3.200 151.425 110.205 237,703 111.137 5900

6000 41.840 247.384 152.128 110.898 241.887 111,814 6000

204 NASA/TP-3287/REV 1
TABLE X. - LEAST-SQUARES FITTING DIFFERENCES WITH THE 9-CONSTANT FUNCTIONAL FORM

Ag(cr) Silver Cubic Crystal. CODATA, 1989, p228.

MAX REL ERR CP/R = 0.009759 TEMP = 400. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.003021 TENP = 200, AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.001515 TEHP = 200. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000100 TEHP = 500. AVER REL ERR GH/R_ =

HAX ERR CP/R = 0.602353 TEHP = 400. AVER ERR CP/R =

MAX ERR HH/RT = 0.006010 TEMP = 200. AVER ERR HH/RT =

MAX ERR S/R = 0.005952 TEHP = 200. AVER ERR S/R :

MAX ERR GH/RT = 0.000506 TEHP = 800. AVER ERR GH/RT =

Al(cr) Aluminum Cubic Crystal, CDDATA

HAX REL ERR CP/R = 0.000047 TEMP = 400.

MAX REL ERR HHtRT = 0.000809 TEMP = 200.

MAX REL ERR S/R = 0.000637 TEMP = 200.

HAX REL ERR GH/RT = 0.002762 TEMP = 200.

MAX ERR CP/R = 0.000163 TEHP = 900.

MAX ERR HH/RT = 0.001098 TEHP = 200.

MAX ERR S/R = 0.001467 TEMP = 200.

MAX ERR GH/RT = 0.002565 TEMP = 200.

T range = 200.000 to 1235.080 K

0.0002_8 REL LST SO ERR CP/R = 0.000351

0.00029_ REL IST SO ERR HH/RT 0.0008_8

0.000173 REL LST SQ ERR S/R = 0.000027

0.000058 REL LST SQ ERR GH/RT = 0.000067

0.000793 LST SQ ERR CP/R = 0.001101

0.000623 LST SQ ERR HH/RT = 0.001700

0.000889 LST SQ ERR $/R" = 0.001732

0.00050_ LST SO ERR GH/RT = 0.000357

AP

2989, P217. T range :

AVER REL ERR CP/R = 0.000027

AVER REL ERR HH/RT = 0.000098

AVER REL ERR $/R = 0.000072

AVER REL ERR GH/RT = 0.000297

AVER ERR CP/R = 0.000092

AVER ERR HH/RT = 0.000155

AVER ERR S/R = 0.000186

AVER ERR GH/RT = 0.000311

Argon, NSRDS-NBS 35, vl, 1971. Temperature cutoff. T range =

MAX REL ERR CP/R = 0.913460 TEHP = 18000. AVER REL ERR CP/R = 0.003116

MAX REL ERR HH/RT = 0,010980 TEHP = 20000. AVER REL ERR HH/RT = 0.001605

MAX REL ERR S/R = 0.002094 TEMP = 20000. AVER REL ERR S/R = 0.000174

MAX REL ERR GH/RT = 0.000335 TEHP = 20000. AVER REL ERR GH/RT = 0.000029

MAX ERR CP/R : 0.051_27 TEMP = 18000. AVER ERR CP/R = 0.009783

MAX ERR HH/RT = 0.052737 TEHP = 20000. AVER ERR HH/RT = 0.00_316

MAX ERR S/R = 0.961673 TEMP = 20000. AVER ERR S/R = 0.005045

MAX ERR GH/RT = 0.000956 TEMP = 20000. AVER ERR GH/RT = 0.000765

B(b) Boron beta. JANAF Jun.1983, p174.

MAX REL ERR CP/R = 0.002022 TEMP = 330.

MAX REL ERR HH/RT = 0.0011_8 TEMP = 230,

MAX REL ERR S/R = 0.000366 TEHP = 200.

MAX REL ERR GH/RT = 0.091705 TEMP = 230.

MAX ERR CP/R = 0.003175 TEMP = 400.

MAX ERR HH/RT = 0.000396 TEHP = 350.

MAX ERR S/R = 0.000280 TEMP = 350.

MAX ERR GH/RT = 0.000222 TEHP = qO0.

B(b) Boron beta. JANAF Jun.lgB3, p17_.

MAX REL ERR CP/R = 0.000113 TEMP = 600.

MAX REL ERR HH/RT = 0.000]00 TEHP = 600.

MAX REL ERR S/R : 0.000027 TEMP = 600.

MAX REL ERR GH/RT = 0.000088 TEMP = 600.

_AX ERR CP/R = 0.000283 TEMP : 600.

MAX ERR HH/RT = 0.000127 TEMP = 600.

MAX ERR S/R = 0.000065 TEMP = 1200.

• MAX ERR GH/RT = 0.000119 TEMP = 1000.

Br2(cr) Bromine Rhombic. TPIS 2989 vl,

MAX REL ERR CP/R = 0.000062 TEMP = 250.

MAX REL ERR HH/RT = 0.000872 TEMP = 200.

MAX REL ERR S/R = 0.000259 TEMP = 200.

MAX REL ERR GH/RT = 0.0011_8 TEMP = 200.

MAX ERR CP/R : 0.0004_ TEMP : 250.

MAX ERR HH/RT = 0.00q036 TEHP = 200.

MAX ERR S/R = 0.002920 TEMP = 260.

MAX ERR GH/RT = 0.006763 TEMP = 200.

100.000 T range =

AVER REL ERR CP/R = 0.000667

AVER REL ERR HH/RT = 0.000301

AVER REL ERR S/R = 0.000127

AVER REL ERR GH/RT = 0.000474

AVER ERR CP/R = 0.001001

AVER ERR HH/RT = 0,000127

AVER ERR S/R = 0.000085

AVER ERR GH/RT : 0.000101

100.000 T range =

AVER REL ERR CP/R = 0.000014

AVER REL ERR HH/RT = 0.000017

AVER REL ERR S/R = 0.000007

AVER REL ERR GH/RT = 0.000021

AVER ERR gP/R = 0.00_041

AVER ERR HH/RT = 0.000031

AVER ERR S/R = 0.000029

AVER ERR GH/RT = 0.000035

pt 2, P_I4. JANAF, 6/82. T range =

AVER RE/ ERR CP/R = 0.000022

AVER REL ERR HH/RF = 0.000615

AVER REL ERR S/R : 0.000208

AVER REL ERR GH/RT = 0.000826

AVER ERR CP/R = 0.000151

AVER ERR HH/RT = 0.002993

AVER ERR S/R = 0.00237_

AVER ERR GH/RT = 0.00536_

p_ 2, p31q. JANAF, 6/82. T range =

AVER REL ERR CP/R = 0.000019

AVER REL ERR HH/RT = 0.000163

AVER REL ERR S/R = 0,000050

AVER REL ERR GH/RT = 0.000310

AVER ERR CP/R = 0.000177

AVER ERR HH/RT = 0.001616

AVER ERR S/R = 0.00089_

AVER ERR GH/RT = 0.002422

Br2(1) Bromine l_quid. TPIS 1989 vI,

MAX REL ERR CP/R = 0.000088 TEMP = 300.

MAX REL ERR HH/RT = 0.000397 TEHP = 270.

MAX REL ERR 5/R = 0,00011_ TEMP = 290.

MAX REL ERR GH/RT = 0,000765 TEHP = 270.

MAX ERR CP/R = 0.000797 TEHP = 300.

MAX ERR HH/RT = 0.003953 TEHP = 270.

MAX ERR S/R = 0.002012 TEMP = 290.

MAX ERR GH/RT = 0,005689 TEMP = 270.

200.000 to 953.610 K

REL LST SQ ERR CP/R = 0.000031

REL LST SQ ERR HH/RT = 0.000254

REL LST SQ ERR SIR = 0.000202

REL LST Sq ERR GH/RT = 0.00007_

LST SQ ERR CP/R = 0.000107

LST SQ ERR HH/RT = D,000351

LST SQ ERR S/R = 0,000_67

LST 50 ERR GH/RT = 0.000815

6000.000 to 20000.000 K

REL LST SQ ERR CP/R = 0.00_363

REL LST SQ ERR HH/RT : 0.003960

REL LST 5Q ERR S/R = 0.000430

REL LST SQ ERR GH/RT = 0.000066

LST SQ ERR CP/R = 0.015202

LST SO ERR HH/RT = 0.010903

LST SQ ERR S/R : 9.012635

LST SQ ERR GH/RT = 0,001766

200.000 to 600.000 K

REL LST SQ ERR CP/R = 0.00092_

REL LST SQ ERR HH/RT : 0.000438

REL LST SQ ERR S/R : 0.000180

REL LST SQ ERR GH/RT = 0.000688

LST SQ ERR CP/R = 0.001_57

LST SQ ERR HH/RT = 0.000166

LST SQ ERR S/R = 0.000112

LST SQ ERR GH/RT = 0,00012_

600.000 to 2350.000 K

REL LST SQ ERR CP/R : 0.000025

REL IST SQ ERR HH/RT = 0.000028

REL LST SQ ERR S/R : 0.000010

REL LST Bq ERR GH/RT = 0.000032

LST _Q ERR CP/R : 0.000969

LST S0 ERR HH/RT : 0.00004_

LST SO ERR S/R = 0.000035

LST SQ ERR GH/RT = 0.0000_5

200.000 to 265.900 K

REL LST SQ ERR CPtR = 0.000030

REL LST SQ ERR HH/RT = 0.000662

REL LST SQ ERR S/R : 0.000223

REL LST SQ ERR GH/RT = 0.000889

LST SQ ERR CP/R = 0.000211

LST SO ERR HH/RT = 0.00321_

LST SQ ERR S/R 0.0025_0

LST S_ ERR GH/RT = 0.0037¢_

265.900 to 332.503 K

REL LST SQ ERR CP/R = 0,000035

REL LST SQ ERR HH/RT = 0.000239

REL LST S_ ERR S/R = 0.000069

REL LST SQ ERR GH/RT = 0.000_62

LST SQ ERR CP/R = 0.000316

LST SQ ERR HH/RT = 0,002374

LST SQ ERR S/R : 0.001232

LST SQ ERR GH/RT : 0.003583

NASA/TP-3287/REVI

205
TABLE X.- Continued.

C(gr) Graphite. TRC Tables VC,UC, TC-IOOO-IOO2,Apr 30,1983. T range =

HAX REL ERR CP/R = 0.001390 TEHP = 220. AVER REL ERR CP/R = 0.000580

MAX REL ERR HH/RT = 0.000621 TEMP = 250. AVER REL ERR HH/RT = 0.000249

HAX REL ERR S/R = 0.000353 TE_IP = 580. AVER REL ERR S/R = 0,000185

HAX REL ERR GH/RT = 0.000492 TEHP = 230. AVER REL ERR GH/RT = 0.000273

HAX ERR CP/R = 0.001202 TEHP = 320. AVER ERR CP/R 0,000542

blAX ERR HH/RT = 0.000183 TEHP = 380. AVER ERR HH/RT = 0.000105

MAX ERR S/R = 0.000361 TEMP = 420. AVER ERR 5/R = 0.000165

HA× ERR GH/RT = 0.00023_ TEHP = 600. AVER ERR GH/RT = 0.000098

C(gr) Graphite. TRC

MAX REL ERR CP/R = 0.000070

HAX REL ERR HH/RT = 0.000676

HA× REL ERR S/R = 0.000178

MAX REL ERR GH/RT = 0.00031_

HA× ERR CP/R = 0.000167

HA× ERR HH/RT = 0.000078

HA× ERR S/R = 0.000310

MAX ERR GH/RT = 0.00023_

Tables VC,UC,TC-]OOO-IOO2,Apr 30,1983.

TEMP = 800. AVER REL ERR CP/R =

TEHP = 600. AVER REL ERR HH/RT =

TEHP = 600 AVER REL ERR S/R =

TEHP = 600 AVER REL ERR GH/RT =

TEHP = 800 AVER ERR CP/R =

TEMP = 1400 AVER ERR HH/RT =

TEMP = 600 AVER ERR S/R =

TEHP = 600 AVER ERR GH/RT =

C(gr) Graphite. TRC

HAX REL ERR CP/R = 0.00003_

HAX REL ERR HH/RT = 0,00005_

FIAX REL ERR S/R = 0.000025

MAX RM_XI _R GH/RT = 0.000054 CP/R O.O00lO&

HAX ERR HH/RT = 0.0001_9

MAX ERR S/R = 0.000123

MAX ERR GH/RT = O.O00ZZO

200.000 to

REL L$T 50

REI LST Sq

REL LST Sq

REL LST SQ

IST SO

LST SQ

LST SQ

LST SQ

600.000 K

ERR CP/R = 0.000753

ERR HH/RT = 0.000310

ERR S/R = 0.000210

ERR GH/RT = 0.000302

ERR CP/R = 0.00066_

ERR HH/RT = 0.000118

ERR S/R = 0.000201

ERR GH/RT = 0.000120

T range = 600.000 _o 2000.000 K

0.000028 REL LST SQ ERR CP/R = 0.000036

0.000025 REL LST SO ERR HH/RT = 0.000033

0.000053 REL LST SQ ERR S/R = 0.000072

0.000108 REL LST Sq ERR GH/RT = 0.000138

0.000069 LST SO ERR CP/R = 0.000084

0.000036 IST 50 ERR HH/RT = 0.0000_4

0.000135 LST SQ ERR 3/R = 0.000160

0.000157 LST SQ ERR GH/RT = 0.000155

Tables VC, UC, TC-IOOO-IOO2,Apr 30,1983. T range = 2000.000 to

TEMP = ZSO0. AVER REL ERR CP/R = 0.000010 REL IST Sq

TEMP = 4500. AVER REL ERR HH/RT = 0.000016 REL LST SO

TEHP = 2000. AVER REL ERR S/R = 0.000009 REL LST SO

TEMP = ZOO0. AVER REL E_ GH/RT = 0.000026 REL LST SO TEMP = 2300. AVER E CP/R 0.000033 LST SQ

TEMP = 4500. AVER ERR HH/RT = 0.000042 LST Sq

TEMP = 2000. AVER ERR SIR = 0.000061 LST SO

TEMP = 4600. AVER ERR GH/RT 0.000102 LST 5O

Ca(a) Calcium Alpha Cryslal. Alcock, JPCRD 1992. T range =

MAX REL ERR CP/R = 0.00002] TEHP = 280. AVER REL ERR CP/R = 0.000010

MAX REL ERR HH/RT = 0.000053 TEMP = 200. AVER REL ERR HH/RT = 0.000033

MAX REL ERR S/R = 0.000019 TEMP = 200. AVER REL ERR S/R = 0.000013

MAX REL ERR GH/RT = 0.000017 TEMP = 200. AVER REL ERR GH/RT = 0.000007

MAX ERR CP/R = 0.000064 TEMP = 280. AVER ERR CP/R = 0.000029

MAX ERR HH/RT = 0.000106 TEMP = 200. AVER ERR HH/RT = 0.000071

MAX ERR $/R = 0.000078 TENP = 280. AVER ERR SIR = 0.000057

MAX ERR GH/RT = 0.000032 TEMP = 200. AVER ERR GH/RT = 0.00001_

Crystal. Alcock, JPCRD 1992. T range =

TEHP = 300. AVER REL ERR CP/R = 0.000151

TEMP = 450. AVER REL ERR HH/RT = 0.000004

TEMP = 450. AVER REL ERR S/R = 0.000002

TEMP = 500. AVER REL ERR GH/RT = 0.000002

TENP = 300. AVER ERR CP/R = 0.000491

TEFIP = _50_ AVER ERR HH/RT = 0.000011

TEHP = 450. AVER ERR S/R = 0.000016

TEMP = 700. AVER ERR GH/RT = 0.000009

Ca(a) Calcium Alpha

MAX REL ERR CP/R = 0.000983

MAX REL ERR HH/RT = 0.000015

MAX REL ERR 5/R = 0.000007

MAX REL ERR GH/RT = 0.000005

MAX ERR CP/R = 0.003050

MAX ERR HH/RT = 0.000038

MAX ERR S/R = 0.0000_7

MAX ERR GH/RT = 0.000013

200.000 _o

REL LST SO

REL LST SQ

REL IST 5Q

REL LST SQ

LST SQ

LST SQ

IST S_

LST Sq

Cd(cr) Cadmium Crystal. COOATA 1989, 0223.

MAX REL ERR CP/R = 0.000443 TEMP = 200.

MAX REL ERR HH/RT = 0.001832 TEMP = 200.

MAX REL ERR $/R = 0.000776 TEIAP = 100.

MAX REL ERR GH/RT = 0.002744 TEHP = 100.

MAX ERR CP/R = 0.001328 TEHP = 200,

MAX ERR HH/RT = 0.00_126 TEHP = 200.

MAX ERR S/R = 0.003263 TEHP = 200.

MAX ERR GH/RT = 0.003829 TEHP = 100.

298,150 ±o

REL IST SO

REL LST SQ

REL LST SQ

REL LST SQ

LST SO

LST SO

IST 50

LST SQ

C12 Chlorine gas.

HAX REI ERR CP/R = 0.0000]5

MAX REL ERR HH/RT = 0.000023

MAX REL ERR S/R = 0.000002

MAX REL ERR GH/RT = 0.000006

MAX ERR CP/R = 0.000067

MAX ERR HH/RT = 0.000092

MAX ERR S/R = 0.000070

MAX ERR GH/RT = 0.000152

5000.000 K

ERR CP/R = 0.000013

ERR HH/RT = 0.000022

ERR S/R = 0.000011

ERR GH/RT = 0.000029

ERR CP/R = 0.000041

ERR HH/RT = 0.000061

ERR S/R = 0.000069

ERR GH/RT = 0.000117

298.150 K

ERR CP/R = 0.000012

ERR HH/RT = 0.000057

ERR S/R = 0.000014

ERR GH/RT = 0.000009

ERR CP/R = 0.000036

ERR HH[RT = 0.000079

ERR S/R = 0.000063

ERR GH/RT = 0.000018

716.000 K

ERR CP/R = 0.000309

ERR HH/RT = 0,000006

ERR S/R = 0.000003

ERR GH/RT = 0.000002

ERR CP/R = 0.000965

ERR HH/RT = 0,000015

ERR S/R = 0.000021

ERR GH/RT = 0.000010

T range = 100.000 to 594,258 K

AVER REL ERR CP/R = 0.000107 REL LST SO ERR CP/R = 0.000184

AVER REL ERR HH/RT = 0.000430 REL LST 59 ERR HH/RT = 0.000774

AVER REI ERR S/R = 0.000219 REL IST SO ERR S/R = 0.0003_4

AVER REL ERR GH/RT = 0.000443 REL IST SQ ERR GH/RT = Q.001044

AVER ERR CP/R = 0.000330 LST 50 ERR CP/R = 0.000560

AVER ERR HH/RT = 0.0009]0 LST SO ERR HH/RT = 0.001665

AVER ERR S/R = 0.000923 LST SO ERR S/R = 0.001552

AVER ERR GH/RT = 0.000698 LST SO ERR GH/RT = 0.001484

T range =

0.000005

0.000013

0.000001

0.000003

0.00O023

0.000050

0.000037

0.000068

Ct2 Chlorine gas.

MAX REL ERR CP/R = 0.001682

MAX REL ERR HH/RT = 0.000211

MAX REL ERR S/R = 0.000055

HAX REL ERR GH/RT = 0.000012

MAX ERR CP/R = 0,007601

MAX ERR HH/RT = 0.000895

HAX ERR $/R = 0.00116¢

MAX ERR GH/RT = 0,000585

200.000 ±o

REL IST SQ

REL LST SQ

REL LST Sq

REI IST SQ

LST SQ

LST SQ

LST SO

LST SO

TPIS 1989, vl, pt2, 088.

TEMP = 600. AVER REL ERR CP/R =

TEHP = 200. AVER REL ERR HH/RT =

TEMP = 500. AVER REL ERR S/R =

TEMP = 200, AVER REL ERR GH/RT =

TEMP = 600. AVER ERR CP/R =

TEHP = 900. AVER ERR HH/RT =

TEMP = 600. AVER ERR S/R =

TEMP = 1000. AVER ERR GH/RT =

TPIS 1989, vl, pt2, p88.

TEMP = 1100. AVER REL ERR CP/R =

TEHP = 1200. AVER REL ERR HH/RT =

TEHP = 1300. AVER REL ERR S/R =

TEMP = 1500. AVER REL ERR GH/RT =

TEMP = 1100. AVER ERR CP/R =

TEHP = 1200. AVER ERR HH/RT =

TEMP = 1300. AVER ERR S/R =

TEMP = 2900. AVER ERR GH/RT =

1000.000 K

ERR CP/R = 0.000007

ERR HH/RT = 0.000015

ERR S/R = 0.000002

ERR GH/RT = 0.000003

ERR CP/R = 0.000030

ERR HH/RT = 0.000058

ERR S/R = 0.00004_

ERR GH/RT = 0.000086

T range = lO00.O00 _o 6000.000 K

0.000648 REI LST SO ERR CP/R = 0,000755

0.000062 REL LST SQ ERR HH/RT = 0.000079

0.000009 REL LST SQ ERR S/R = 0.000012

0.000008 REL LST SO ERR GH/RT = 0.000008

0.003186 LSY SO ERR CP/R = 0.003664

0.000276 LST SO ERR HHtRT = 0.000347

0.000332 LST SO ERR SIR = 0.000434

0.000247 LST S_ ERR GH/RT = 0,000254

206 NASA/TP-3287/REV 1
TABLE X.- Continued.

CoCa) Cobalt Alpha Crystal. JANAF, SEPT. 1967. T range =

MAX REL ERR CP/R = 0.000245 TEMP = 350. AVER REL ERR CP/R = 0.000078

MAX REL ERR HH/RT = 0.002518 TEMP = 250, AVER REL ERR HH/RT = 0,000338

HA× REL ERR S/R = 0.001281 TEMP = 250. AVER REL ERR 5/R = 0.000237

HAX REL ERR GH/RT = 0.001115 TEMP = 200. AVER REL ERR GH/RT = 0.000190

HAX ERR CP/R = 0.000758 TEMP = 350, AVER ERR CP/R = 0.0002_1

HA× ERR HH/RT = 0,00_3_5 TEMP = 250, AVER ERR HH/RT = 0,00059_

HA× ERR S/R : 0.003967 TEMP = 250. AVER ERR S/R : 0.000727

MAX ERR GH/RT = 0.001131 TEMP = 200, AVER ERR GH/RT = 0.000228

Co(a) Cobalt Alpha CrystaL. JANAF, SEPT, 1967,

MAX REL ERR CP/R = 0.000013 TEMP = 550. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000039 TEMP = 700. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000055 TEMP = 600. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000056 TEHP = 600. AVER REL ERR GH/RT =

MAX ERR CP/R = 0,0000_5 TEMP = 550. AVER ERR CP/R =

MAX ERR HH/RT = 0.000106 TEMP = 700. AVER ERR HH/RT =

MAX ERR S/R = 0.000205 TEMP = 600. AVER ERR S/R =

MAX ERR GH/RT = 0.000182 TEMP = 600, AVER ERR GH/RT =

Co(b) Cobalt Beta below Lambda transition. JANAF,9/1967.

MAX REL ERR CP/R = 0.000009 TEHP = 800, AVER REL ERR CP/R

MAX REL ERR HH/RT = 0.000097 TEMP = 800. AVER REL ERR HH/RT =

MAX REL ERR 5/R = 0,000037 TEMP = 800. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000046 TEMP = 700. AVER REL ERR GH/RT =

MAX ERR CP/R : 0,000035 TEHP = 800. AVER ERR CP/R =

HAX ERR HH/RT = 0.000286 TEMP = 800. AVER ERR HH/RT =

MAX ERR 5/R : 0.000263 TEMP = 800. AVER ERR S/R =

MAX ERR GH/RT : 0.000170 TENP = 700. AVER ERR GH/RT =

T range =

0.000010

0.000023

0.000020

0.000039

0.000036

0,000065

0,000117

0,000130

T range =

0.00000_

0.000067

0.000024

0.000026

0.000010

0.000196

0.000163

0.000097

Co(b} Cobalt Beta below tambda transition. JANAF, 9/1967. T range =

MAX REL ERR CP/R = 0.000581 TEHP = 1200. AVER REL ERR CP/R = 0.001854

MAX REL ERR HH/RT = 0.000312 TEMP = 1200. AVER REL ERR HH/RT = 0.0001_8

MAX REL ERR S/R = D.00_135 TEMP = 1200. AVER REL ERR $/R = 0.000066

MAX REI ERR GH/RT = C.000026 TEMP = 1300. AVER REL ERR GH/RT = 0.000016

MAX ERR CP/R = 0,023813 TEHP = 1200. AVER ERR CP/R = 0.009620

MAX ERR HH/RT = 0.00J079 TEMP = 1200. AVER ERR HH/RT = 0.000_97

t_AX ERR 5/R = _.901189 TZ_P = 1200. AVER ERR S/R = 0.000558

MAX ERR GH/RT • 0.0C01_8 TEHP = ]300. AVER ERR GH/RT = 0.000084

Co(b) Coheir _eta above tembda transitlon. JANAFp9/2967.

MAX REL ERR CP/R , C 000825 TEMP = ]599. AVER REL ERR CP/R =

HAX REL ERR HH/=T • 0 000929 TEMP = I_00, AVER REL ERR HH/RT =

MAX REL ERR $/R • 0 0000_6 TEMP = 1_00, AVER REL ERR S/R =

MAX REL ERR GHIRT • C 003040 TEMP = 1_00, AVER REL ERR OH/RT =

MAX ERR C_ • 0 _0_8 TEMP = 159_. AVER ERR CP/R =

MAX ERR HHtiT • 00_OIlO TEMP = 1400, AVER ERR HH/RT =

MAX ERR $/e ' _ 0_35,6 TEMP = i_00. AVER ERR S/R =

MAX ERR OH/R/ - O 000_0 TEMP = 1400. AVER ERR GH/RT =

Co(b) Col_l! let= above lembda trensJt$on. JANAF, 9/I967.

MAX REL ERR CP.e 0 ec,_22 TEMP = 1600. AVER REL ERR CP/R

MAX REL ERR H_'S: _ :cc_:_ TEMP = 1500.

_AX REL ERR 5re : _22_ TEMP = 1500.

MAX REL ERR GH mT : 0c_372 TEMP = 1768.

MAX ERR CP,_ C ::_?q_ TEHP = 1600.

MAX ERR HH'_I & 0_,05] TEMP = 1500.

MAX ERR S'_ ¢ _,:'10 TEMP = 1500,

MAX ERR Gff_RI _ Ooo_9[ TEMP = 1768.

=

AVER REL ERR HH/RT =

AVER REL ERR S/R =

AVER REL ERR GHtRT =

AVER ERR CP/R =

AVER ERR HH/RT =

AVER ERR S/R =

AVER ERR GH/RT =

June 1973.

ERR CP/R ERR HH/RT

ERR S/R =

ERR GH/RT =

ERR CP/R =

ERR HH/RT =

ERR S/R =

ERR GH/RT =

June 1973.

ERR CP/R =

ERR HH/RT =

ERR S/R =

ERR GH/RT =

ERR CP/R =

ERR HH/RT =

ERR S/R =

ERR GH/RT =

Cr(cr) Chr¢_ Cry=tel. Below lembda _rans. JANAF.

MAX REL ERR CP/R , © 000197 TEMP = 300. AVER REL

MAX REL ERR HH/R1 , C 0097_9 TEMP = 250, AVER REL

MAX REL ERR S/R • 0 000_28 TEHP = 250, AVER REL

MAX REL ERR GH/RI • 0 000_72 TEHP = 200. AVER REL

MAX ERR CP/R • 0.000556 TEMP = 300, AVER

MAX ERR HH/RT • 0.00106_ TEMP = 250. AVER

MAX ERR S/R _ 0.001009 TEMP = 250. AVER

MAX ERR GH/RT = 0.000506 TEHP = 200. AVER

CrCcr) Chromium Crystal. Above lambda trans. JANAF,

MAX REL ERR CP/R = 0.000321 TEMP = 600. AVER EEL

MAX REL ERR HH/RT = 0.000119 TEMP = 512, AVER REL

MAX REL ERR S/R = 0.00006_ TEHP = 350. AVER REL

MAX REL ERR GH/RT = 0.000207 TEHP = _50. AVER REL

MAX ERR CP/R = 0.001071 TEHP = 600. AVER

MAX ERR HH/RT = 0.000232 TEMP = 900. AVER

MAX ERR S/R = 0.000213 TEMP = 350. AVER

MAX ERR GH/RT 0.000307 TEHP = 350. AVER

T renge

0.000_13

0.000020

0.000022

0.00003I

0.002730

0,000075

0.000216

0,000281

T range =

0.001779

0.000286

0.0001_

0.000054

0.000210

0.001125

0.001474

0.000351

T ranga =

0.000085

0.000270

0.000119

0.000159

0.000230

0.000373

0.000281

0.000137

T reRge =

9.000155

0.000050

0.000028

0.000058

0.000506

0.000112

0.000118

0.000122

200.000 _o 500.000 K

REL LST SO ERR CP/R = 0.000116

REL LST Sq ERR HH/RT = 0.000891

REL LST Sq ERR S/R = 0.000082

REL LST Sq ERR GH/RT = 0,000q07

IST Sq ERR CP/R = 0.000365

LST Sq ERR HH/RT = 0.0015_8

LST S_ ERR S/R = 0.00146_

LST SQ ERR GH/RT = 0.000426

500,000 _o 700,1o0 K

REL LST SO ERR CP/R = 0.000011

REL LST S_ ERR HH/RT = 0.000027

REL LST 50 ERR S/R = 0.00002_

REL LST S_ ERR GH/RT = 0.0000_1

LST 5_ ERR CP/R = 0.000038

LST S_ ERR HH/RT = 0.000073

LST S_ ERR S/R = 0.000129

LST 5_ ERR GH/RT 0.000138

700.100 to 800.000 K

REL LST S_ ERR CP/R = 0.000006

REL LST S_ ERR HH/RT = 0.000073

REL LST S_ ERR S/R = 0.000027

REL LST S_ ERR GH/RT = 0.000033

LST S_ ERR CP/R = 0.000025

LST SO ERR HH/RT = 0.000216

LST SG ERR 5/R = 0.000191

LST SG ERR GH/RT = 0.000122

800.000 to 1390.000 K

REL LST SO ERR CP/R = 0,002358

REL LST S_ ERR HH/RT = 0.000177

REL LST S_ ERR 5/R = 0.000079

REL LST SO ERR GH/RT = 0.000018

LST SQ ERR CP/R = 0.0]2563

LST SQ ERR HH/RT = 0.000605

LST SQ ERR SiR = 0.000683

tST Sq ERR GH/RT = 0.000098

1394.000 to 1_00.000 K

REL LST Sq ERR CP/R = O.O00SB4

REL LST SQ ERR HH/RT = 0.000022

REL LST Sq ERR S_R = 0.000026

REL LST Sq ERR GH/RT 0.000032

LST 5q ERR CP/R = 0.003860

LST SO ERR HH/RT = 0.000083

LST S_ ERR S/R = 0.000252

LST 5_ ERR GH/RT = 0.000189

1_00.000 to 1760,000 K

REL LST 50 ERR CP/R = 0.002143

REL LST 5_ ERR HH/RT = 0.000527

REL LST 5_ ERR S/R = _.000155

REL LST sq ERR GH/RT = 0.000055

LST sq ERR CP/R = 0.009867

LST SR ERR HH/RT = 0.00128_

LST 5_ ERR S/R = _.001609

LST Sq ERR GH/RT = 0.000564

200.000 to _II.500 K

REL LST 5_ ERR CP/R = 0.000212

REL LST S_ ERR HH/RT = 0.00058_

REL LST 50 ERR S/R = 0.000197

REL LST S_ ERR GH/RT = 0.000235

LST SG ERR CP/R = 0.000_1I

LST S_ ERR HH/RT = 0.000528

/ST SO ERR S/R = 0.000_63

LST 5Q ERR GH/RT = 0.000165

311.500 to 1000.000 K

REL LST S_ ERR CP/R = 0.000180

REL LST 50 ERR HH/RT = 0.000059

REL LST SO ERR 5/R = 0.000055

REL LST 5_ ERR GH/RT = 0.000078

LST S_ ERR CP/R = 0.000588

LST S_ ERR HH/RT = 0.000129

LST SQ ERR S/R = 0,000130

LST 5Q ERR GH/RT = O.O00lq2

NASA/TP-3287/REV l 207
TABLE X. - Continued.

Cr(cr) Chromium Crystal. Above lambda trans. JANAF. June 1973.

MAX REL ERR CP/R = 0.000815 TEMP = 1200. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000057 TEMP = 1100. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000030 TEMP = 1100. AVER REL ERR S/R =

FlAX REL ERR GH/RT = 0.000031 TEMP = 1000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.003_47 TEMP = 1200. AVER ERR CP/R =

MAX ERR HH/RT = 0.000167 TEMP = 1100. AVER ERR HH/RT =

MAX ERR S/R = 0.000217 TEMP = 1100. AVER ERR S/R =

MAX ERR GH/RT = 0.000149 TEMP = 1800. AVER ERR GH/RT =

Cs(cr) Ce_ium Crystal. CODATA, 1989, p265.

MAX REL ERR CP/R = 0.000210 TEMP = 200.

MAX REL ERR HH/RT = 0.002567 TEMP = ]00.

MAX REL ERR S/R = 0.001344 TEHP = 100.

MAX REL ERR GH/RT = 0.005856 TEMP = 100.

MAX ERR CP/R = 0.000701 TEHP = 200.

MAX ERR HH/RT = 0.006637 TEHP = 100.

MAX ERR 5/R = 0.008897 TEMP = 200.

MAX ERR GH/RT = 0.015526 TEMP = 100.

Cs(1) Cesium Liquid. CODATA, 1989, pZ6S.

MAX REL ERR CP/R = 0.000011 TENP = 600.

MAX REL ERR HH/RT = 0.000054 TEHP = 302.

MAX REL ERR S/R = 0.000004 TEMP = 900.

MAX REL ERR GH/RT = 0.000014 TEMP = 302,

MAX ERR CP/R = 0.000041 TEMP = 600.

MAX ERR HH/RT = 0.000154 TEHP = 302.

MAX ERR S/R = 0.000063 TEHP = 900.

MAX ERR GH/RT = 0.000100 TEHP = 302.

Cs(1) Cesium Liquid. CODATA, 1989, p263.

MAX REL ERR CP/R = 0.000013 TEMP = 1300.

MAX REL ERR HH/RT = 0.000012 _EMP = 1000.

MAX REL ERR SIR = 0.000002 TEHP = 1900.

MAX REL ERR GH/RT = 0.000004 TEMP = 1900.

MAX ERR CP/R = 0.000063 TEHP = 1600.

MAX ERR HH/RT = 0.000046 TEMP = 1000.

MAX ERR S/R = 0.0000_2 TEMP = 1900.

MAX ERR GH/RT = 0.000055 TEMP = 1900.

T range =

0.000176

0.000016

0.000013

0.000016

0.000787

0.000051

0.000113

0.000086

T range =

AVER REL ERR CP/R = 0.000091

AVER REL ERR HH/RT = 0.000654

AVER REL ERR S/R = 0.000471

AVER REL ERR OH/RT = 0.001157

AVER ERR CP/R = 0,000321

AVER ERR HH/RT = 0,001739

AVER ERR S/R = 0.003570

AVER ERR GH/RT = 0.005284

T range =

AVER REL ERR CP/R = 0.000005

AVER REL ERR HH/RT = 0.000014

AVER REL ERR S/R = 0.000002

AVER REL ERR GH/RT = 0.000005

AVER ERR CP/R = 0.000017

AVER ERR HH/RT = 0.000055

AVER ERR S/R = 0.000028

AVER ERR GH/RT = 0.000048

T range =

AVER REL ERR CP/R = 0.000006

AVER REL ERR HH/RT = 0.000004

AVER REL ERR $/R = 0.000001

AVER REL ERR GH/RT = 0.000002

AVER ERR CP/R = 0.000030

AVER ERR HH/RT = 0.000017

AVER ERR S/R = 0.000021

AVER ERR GH/RT = 0.000022

Cu(cr) Copper Cubic Crystal. CODATA, 1989, p226. T range =

MAX REL ERR CP/R = 0.000192 TEMP = 400. AVER REL ERR CP/R = 0.000056

HAX REL ERR HH/RT = 0.000942 TEMP = 200. AVER REL ERR HH/RT = 0.000009

MAX REL ERR SIR = 0.000533 TEHP = 200. AVER REL ERR S/R = 0.000052

MAX REL ERR GH/RT = 0.000032 TEHP = 300. AVER REL ERR GH/RT 0.000015

MAX ERR CP/R = 0.000584 TEMP = 400. AVER ERR CP/R = 0.000175

MAX ERR HH/RT = 0.001519 TEMP = 200. AVER ERR HH/RT = 0.000162

MAX ERR S/R = 0.001522 TEMP = 200. AVER ERR S/R = 0.000199

MAX ERR GH/RT = 0.000148 TEMP = 1000. AVER ERR GH/RT = 0.000061

1000.000 to 2150,000 K

REL LST sq ERR CP/R = 0.000524

• EL LST S_ ERR HH/RT = 0,000023

REL LST SQ ERR S/R = 0.000015

REL LST SQ ERR GH/RT = 0.000018

LST SO ERR CP/R = 0.001353

LST SQ ERR HH/RT = 0.000069

LST SQ ERR S/R = O.O00]Z9

LST SO ERR GH/RT = 0,000093

DZ Deuterium, TPIS, 1989, vl, pt2,

MAX REL ERR CP/R = 0.000057 TEHP = 400.

HAX REL ERR HH/RT = 0.000079 TEHP = 200.

MAX REL ERR S/R = 0.000014 TEHP = ZOO.

MAX REL ERR GH/RT = 0.000009 TEMP = 400.

MAX ERR CP/R = 0.000199 TEHP = 400.

MAX ERR HH/RT = 0.000272 TEHP = 200.

MAX ERR S/R = 0.000225 TEMP = Z00.

MAX ERR GH/RT = 0.0001_1 TEMP = 400.

100.000 to 301,590 K

REL LST SO ERR CP/R = 0.0001]4

REL LST SO ERR HH/RT = 0.001182

REL LST SQ ERR S/R = 0.000751

REL LST $0 ERR GH/RT = 0.001904

LST SO ERR CP/R = 0.000595

LST SO ERR HH/RT = 0.005079

LST SO ERR SIR = 0.005624

LST SQ ERR GH/RT = 0.008458

501,590 to I000.000 K

REI LST SO ERR CP/R = 0.000006

REL LST 50 ERR HH/RT = 0.000016

REL LST SQ ERR S/R = 0.000002

REL LST Sq ERR GH/RT = 0.000007

LST SQ ERR CP/R = 0.000022

LST SQ ERR HH/RT = 0.00006_

LST SO ERR S/R = 0.000032

LST $0 ERR GH/RT = 0.000058

1000.000 _o 2000.000 K

REL LST SO ERR CP/R = 0.000008

REL LST SQ ERR HH/RT = 0.000006

REL LST S0 ERR S/R = 0.000001

REL LST S_ ERR GH/RT = 0.000002

[ST SQ ERR CP/R = 0.000037

LST Sq ERR HH/RT = 0.000022

LST SQ ERR S/R = 0.000026

LST SQ ERR OH/RT = 0.000028

200.000 to 1358.000 K

REL LST SQ ERR CP/R = 0.00008_

REL LST SO ERR HH/RT = 0.000255

REL LST SO ERR S/R = 0.000144

REL LST SQ ERR GH/RT = 0.000018

LST SO ERR CP/R = 0.000256

LST 5q ERR HH/RT = 0.000416

LST S0 ERR S/R = 0.000_25

LST Sq ERR GH/RT = 0.000074

pp_5-6. T range = 200.000 to 1000.000 K

AVER REL ERR CP/R = 0.000025 REL LST SO ERR CP/R = 0.000051

AVER REL ERR HH/RT = 0,000022 REL LST SO ERR HH/RT = 0.000031

AVER REL ERR $/R = 0,000003 REL LST SO ERR 5/R = 0.000005

AVER REL ERR GH/RT = 0.000005 REL LST SO ERR GH/RT = 0.000004

AVER ERR CP/R = 0.000089 LST 5Q ERR CP/R = 0.000113

AVER ERR HH/RT = 0.000075 LST Sq ERR HH/RT = 0.000107

AVER ERR 5/R = 0.000057 LST 50 ERR S/R = 0,000083

AVER ERR GH/RT = 0.000055 LST 5Q ERR GH/RT = 0.000066

D2 Deuterium. TPIS, 1989, vl, pt2, pp45-6. T range =

MAX REL ERR CP/R = 0.000170 TEMP = 6000. AVER REL ERR CP/R = 0.000047

MAX REL ERR HH/RT = 0.000031 TEMP = 1400. AVER REL ERR HH/RT = 0.000012

MAX REL ERR SIR = 0,000003 TEMP = 1400. AVER REL ERR S/R = 0.000001

MAX REL ERR GH/RT = 0.000004 TEHP = 2100. AVER REL ERR GH/RT 0.000001

MAX ERR CP/R = 0.000863 TEMP = 6000. AVER ERR CP/R = 0.000225

MAX ERR HH/RT = 0.000114 TEr4P = 5100. AVER ERR HH/RT = 0.000048

MAX ERR S/R = 0.000079 TEHP = 3600, AVER ERR S/R = 0.000036

MAX ERR GH/RT = 0.000081 TEMP = 2100. AVER ERR GH/RT = 0.000029

DZ Deuterium. TPIS, 1989, vl, ptZ, pp45-6. T range =

MAX REL ERR CP/R = 0.000228 TEMP = 20000. AVER REL ERR CP/R = 0.000092

MAX REL ERR HH/RT = 0.000027 TEMP = 18000. AVER REL ERR HH/RT = 0.000009

MAX REL ERR SIR = 0.000004 TEHP = 6600. AVER REL ERR 5/R = 0.000001

MAX REL ERR GH/RT = 0.000002 TEMP = I_500. AVER REL ERR GH/RT = 0.000001

MAX ERR CP/R = 0.000956 TEMP = 6200. AVER ERR CP/R = 0.000385

HAX ERR HH/RT = 0.000117 TEMP = 6600. AVER ERR HH/RT = 0.000042

MAX ERR 5/R = 0.000230 TEMP = 6600. AVER ERR S/R = 0.000039

MAX ERR GH/RT = 0.000068 TEHP = 14500. AVER ERR GH/RT = 0,000028

1000.000 to 6000.000 K

REL LST SQ ERR CP/R = 0,000059

REL LST SO ERR HH/RT = 0.000014

REL LST SO ERR S/R = O.0000OZ

REL LST S0 ERR GH/RT = O.00000Z

LST SO ERR CP/R = 0,000279

LST 50 ERR HH/RT = 0.000057

LST SO ERR S/R = 0.000042

LST SQ ERR GH/RT = 0.000035

6000.000 to ZO00O.O00 K

REL LST Sg ERR CP/R = 0.000108

REL LST 5O ERR HH/RT = 0.000012

REL LST SO ERR S/R = 0.000001

REL LST SO ERR GH/RT = 0.000001

LST SO ERR CP/R = 0.000440

LST SQ ERR HH/RT = 0.000055

LST 5q ERR S/R = 0.000047

LST SO ERR GH/RT = 0.000033

208 NASA/TP-3287/REV 1
TABLE X. - Continued.

F2 FluorSne gas. TP2$ 1989, vl, pt2, p73. T range =

MAX REL ERR CP/R = 0.000097 TEMP = 400, AVER REL ERR CP/R = 0.000039

MAX REL ERR HH/RT = 0.000140 TEHP = 20D. AVER REL ERR HH/RT 0.000024

MAX REL ERR S/R = 0.000020 TEMP = 200. AVER REL ERR $/R = 0.000005

MAX REL ERR GH/RT = 0.000005 TEHP = 400. AVER REL ERR GH/RT = 0.000002

FlAX ERR CP/R = 0.000584 TEHP = _00. AVER ERR CP/R = 0.00016_

MAX ERR HH/RT = 0.000491 TEHP = 200. AVER ERR HH/RT = 0.000088

MAX ERR S/R = 0,0004_8 TEMP = 200. AVER ERR 5/R = 0.000066

HAX ERR GH/RT = 0.000115 TEMP = 400. AVER ERR GH/RT = 0.000050

F2

Fluorine gas. TPIS 1989, vl, p_2, p73, T range =

MAX REL ERR CP/R = 0.001173 TEHP = 6000, AVER REL ERR CP/R = 0.000348

MAX REL ERR HH/RT = 0.000062 TEMP = 2200. AVER REL ERR HH/RT 0.000027

MAX REL ERR S/R = 0,000008 TEHP = 2300. AVER REL ERR S/R = 0.00000_

MAX REL ERR GH/RT = 0,000004 TEHP = 1200, AVER REL ERR GH/RT = 0.000001

MAX ERR CP/R = 0,004065 TEHP = 6000. AVER ERR CP/R = 0.001440

MAX ERR H1⁄2/RT = 0,000269 TEMP = 2200, AVER ERR HH/RT = 0.000118

NAX ERR S/R = 0.000275 TEHP = 2500. AVER ERR SIR = 0.000126

MAX ERR GH/RT = O.O0011S TEMP = 1200, AVER ERR GH/RT = 0.000036

Fe(a) Iron below Lambda transition. JANAF, MAR.1978. T range =

MAX REL ERR CP/R = 0.000061 TEMP = 250. AVER REL ERR CP/R = 0.000019

MAX REL ERR HH/RT = 0.000177 TEMP = 200, AVER REL ERR HH/RT 0.000065

MAX REL ERR S/R = 0.000079 TEHP = 200. AVER REL ERR SIR = 0.000015

HAX REL ERR GH/RT = 0.000108 _EMP = 250, AVER REL ERR OH/RT = 0.000054

MAX ERR CP/R = 0.000173 TEMP = 250. AVER ERR CP/R = 0.000058

MAX ERR HH/RT = 0,000234 TEMP = 200. AVER ERR HH/RT = 0,000111

HAX ERR S/R = 0.000170 TEHP = 200. AVER ERR 5/R = 0.000040

MAX ERR GH/RT = 0.000170 TEMP = 550. AVER ERR OH/RT = 0.000078

re(a) Iron beXo_ Lambda _rmnsition. JANAF, MAR.1978. T range •

MAX EEL ERR CP/R = 0.000095 TEHP = 700. AVER REL ERR CP/R = 0,000048

MAX REL ERR HH/RT = 0.000290 TEHP = 800. AVER REL ERR HH/RT = 0.000109

MAX REL ERR S/R = 0.0001_0 TEHP = 800. AVER REL ERR 5/R = 0.000048

HAX REL ERR GH/RT = 0.0000_1 TEHP = 550. AVER REL ERR GH/RT = 0.000016

HAX ERR CP/R = 0.000394 TEMP = 700. AVER ERR CP/R = 0-000192

MAX ERR HH/RT = 0.000875 TEMP = 800. AVER ERR HH/RT = 0.000_15

MAX ERR 5/R = 0.000956 TEHP = 800. AVER ERR $/R = 0.000312

MAX ERR GH/RT = 0.000116 TEHP = 550. AVER ERR OH/RT = 0.0000_9

Fa(a) Iron below Lambde transition, JANAF, MAR.1978. T range =

MAX REL ERR CP/R = 0.000794 TEMP = 1000. AVER REL ERR CP/R = 0.000373

MAX REL ERR HH/RT = 0.005283 TEMP = 1000. AVER REL ERR HH/RT = 0.001540

HAX REL ERR S/R = 0.002309 TEHP = 1000. AVER REL ERR $/R = 0.000658

MAX REL ERR GH/RT = 0.000205 TEHP = 950. AVER REL ERR GH/RT = 0.000094

MAX ERR CP/R = 0.006355 TEMP = 1050. AVER ERR CP/R = 0.002618

MAX ERR HH/RT = 0.018521 TEMP = 1000. AVER ERR HH/RT 0.005301

HAX ERR S/R = 0.018511 TEMP = lOgO. AVER ERR S/R = 0.005049

MAX ERR GH/RT = 0.000899 TEHP = 950. AVER ERR GH/RT 0.000_23

Fe(e) Iron abovo Lambda transition. JANAF, HAR,1978. T range :

MAX REL ERR CP/R = 0.001864 TEMP = 1100. AVER REL ERR CP/R = 0.000759

MAX REL ERR HH/RT = 0.018458 TEMP = 1100. AVER REL ERR HH/RT 0,009081

HAX REL ERR S/R = 0.008274 TEHP = 2100. AVER REL ERR S/R = 0.004204

MAX REL ERR OH/RT 0,001099 TEHP = 110_. AVER REL ERR GH/RT 0.0005_5

MAX ERR CP/R : 0.010401 TEMP = 1100. AVER ERR CP/R = 0.004375

MAX ERR HH/RT = 0.069582 TEMP = 1100, AVER ERR HH/RT = 0.034465

MAX ERR S/R = 0.071707 TEHP = 1100. AVER ERR 5/R = 0.0S6911

MAX ERR GH/RT = 0.005695 TEHP = 1184. AVER ERR GH/RT = 0.00Z766

Fe(c) Iron Oamma Crystal. JANAF, HAR.1978. T range

MAX REL ERR CP/R = 0.005611 TEMP = 1500. AVER REL ERR CP/R = 0.001955

MAX REL ERR HH/RT = 0.007758 TEHP = 1184, AVER REL ERR HH/RT = 0.006042

MAX REL ERR 5/R = 0.003978 TEMP = 1184. AVER REL ERR 5/R = 0.005475

MAX REL ERR GH/RT = 0.002111 TEHP = 1665. AVER REL ERR GH/RT = 0.001655

MAX ERR CP/R = 0.023522 TEHP = 1300, AVER ERR CP/R = 0.008315

MAX ERR HH/RT = 0,030677 TEMP = 1184. AVER ERR HH/RT = 0.024161 HAX ERR S/R 0.036570

MAX ERR GH/RT ; TEMP = 118_, AVER ERR 5/R = 0.035997

0.023817 TEMP : 1665. AVER ERR GH/RT 0.009856

Fefd) Zron Delta Crystal. JANAF, MAR.1978. T ranga :

MAX REL ERR CP/R = 0.001379 TEMP = 1700, AVER REL ERR CP/R = 0.000456

MAX REL ERR HH/RT = 0.004461 TEMP = 1665. AVER REL ERR HH/RT = 0.004162

MAX REL ERR $/R = 0.003020 TEHP = 1665. AVER REL ERR $/R = 0.002931

MAX REL ERR GH/RT = 0.002214 TEHP = 1800. AVER REL ERR GH/RT = 0.002168

HAX ERR CP/R = 0.006878 TEMP = 1700. AVER ERR CP/R = 0.002286

MAX ERR HH/RT 0.018408 TEMP = 1665. AVER ERR HH/RT = 0.017331

MAX ERR 5/R : 0.032226 TEHP = 2665. AVER ERR 5/R : 0.051952

MAX ERR GH/RT = 0.015238 TEMP = 1809, AVER ERR GH/RT = 0.014601

200.DO0 _o 1000.000 K

REL LST Sq ERR CP/R =

REL LST $Q ERR HH/RT =

REL LST $g ERR 5/R =

REL LST 50 ERR GH/RT =

LST Sq ERR CP/R =

LST SQ ERR HH/RT =

LST 5q ERR 5/R =

IST 5q ERR GH/RT =

1000,000 _o 6000.000 K

REL LST 5Q ERR CP/R =

REL LST SQ ERR HH/RT :

REL LST 50 ERR S/R =

REL IST 5Q ERR GH/RT =

LST SQ ERR CP/R =

LST 50 ERR HH/RT =

LST 50 ERR S/R =

LST 50 ERR GH/RT =

200.000 _o 500.600 K

REL LST Sq ERR CP/R =

REL LST 50 ERR HH/RT =

REL LST SQ ERR S/R =

REL LST SQ ERR GH/RT =

LST SQ ERR CP/R =

LST Sq ERR HH/RT =

LST 5Q ERR 5/R =

LST $q ERR GH/RT =

500.000 _o 800.000 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST SQ ERR S/R =

REL LST SQ ERR GH/RT =

LST SQ ERR CPIR =

LST SQ ERR HH/RT =

LST SQ ERR S/R =

LST SQ ERR GH/RT =

800,000 _o 10_2.000 K

REL LST 50 ERR CP/R =

REL LST SQ ERR 1⁄2H/RT =

REL LST SQ ERR S/R =

REL LST SQ ERR GH/RT =

LST SO ERR CP/R =

LST SQ ERR HH/RT =

LST SQ ERR 5/R =

LST SQ ERR GH/RT =

1042.000 to 1184,000 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST SQ ERR S/R :

REL LST SQ ERR GH/RT =

LST $Q ERR CP/R =

LST SQ ERR HH/RT =

LST 50 ERR S/R =

LST SQ ERR GH/RT

1184.000 to 1665.000 K

REL LST SQ ERR CP/R REL LST SQ ERR HH/RT

REL LST 5Q ERR $/R =

REL LST SQ ERR GH/RT =

LST SQ ERR CP/R LST $0 ERR HH/RT

LST $q ERR SIR =

LST SQ ERR GH/RT =

]665.00B to 1809.000 K

REL LST SO ERR CP/R =

REL LST $Q ERR HH/RT =

REL LST 50 ERR S/R =

REL LST 50 ERR GH/RT =

LST Sq ERR CP/R =

LST SQ ERR HHIRT :

LST Sq ERR SIR =

LST SQ ERR GH/RT =

0.000050

0.000046

0.000006

0.000003

0,000Z09

0,00016S

0.000144

0,000062

0,000409

0.000032

0.00000_

0,000001

0.0026_9

0.000159

0.0001_6

0.00004_

0.000027

0.000085

0.000029

0.000070

0.000079

0.000135

0.000066

0.000101

0.000059

0.000152

0.000071

0.000021

0.000257

0.000449

0.000_79

0.000065

0.000485

0.002246

0.000927

0.000107

0.005382

0.007394

0.007368

0.000481

0.001091

0.011607

0.005315

0.000685

0.006107

0.04_942

0.046446

0.003519

0.002623

0,006162

0.005492

0.001696

0.011071

0.024602

0.0540_7

0.010283

0,000722

0.004169

0.002932

0.002168

0.003620

0.017555

0.031935

0.014615

NASAfI'P-3287/REV l

209
TABLE X. - Continued.

Oe(cr) Germanium Cubic. TPI$ 1991, v2, p_l, p30B, p_2 p268, T range =

MAX REL ERR CP/R = 0.000129 TEHP = 300. AVER REL ERR CP/R = 0.000029

MAX REL ERR HH/RT = 0.000603 TEHP = 200. AVER REL ERR HH/RT = 0.000141

MAX REL ERR S/R = 0.000378 TEMP = ZOO. AVER REL ERR S/R = 0.000088

HAX REL ERR GH/RT = 0.001572 TEMP = 200. AVER REL ERR GH/RT = 0.000319

MAX ERR CP/R = 0.000360 TEMP = 300. AVER ERR CP/R = 0.000082

MAX ERR HH/RT = 0.000885 TEHP = 200. AVER ERR HH/RT = 0.000218

MAX ERR S/R = 0.001008 TEHP = 200. AVER ERR S/R = 0.000255

MAX ERR GH/RT = 0.00169] TEMP = ZOO. AVER ERR GH/RT : 0.000388

Oe(cr) Germanium Cubic. TPIS 1991, v2, ptl, p308, p_2 p268. T range =

MAX REL ERR CP/R = 0.000007 TEMP = 600. AVER REL ERR CP/R = 0.000004

MAX REL ERR HH/RT = 0.000005 TEMP = 400. AVER REL ERR HH/RT = 0.000002

MAX REL ERR S/R = 0.000008 TEMP = 400. AVER REL ERR $/R = 0.000005

MAX REL ERR GH/RT = 0.000013 TEMP = 400. AVER REL ERR GH/RT = 0.000008

HA× ERR CP/R = 0.000023 TEHP = 700. AVER ERR CP/R = 0.000012

HAX ERR HH/RT = 0,000008 TEMP = 1000, AVER ERR HH/RT = 0,000006

HA× ERR S/R = 0.000058 TEMP = 400. AVER ERR S/R = 0.000028

HA× ERR GH/RT = 0.000033 TEMP = 600. AVER ERR GH/RT = 0.000031

H2 Hydrogen. GLUSHKO ET.AL. vl, pt2, 1978, pp31-32. T range =

MAX REL ERR CP/R = 0.000430 TEMP = 250. AVER REL ERR CP/R = 0.000179

MAX REL ERR HH/R7 = 0.000153 TEMP = 400. AVER REL ERR HH/RT = 0.000059

MAX REL ERR S/R = 0.00002_ TEHP = 400. AVER REL ERR S/R = 0.000012

HAX REL ERR GH/RT = 0.000046 TEMP = 250. AVER REL ERR GH/RT = 0.000011

MAX ERR CP/R = 0.001465 TEMP = 250. AVER ERR CP/R = 0.000626

MAX ERR HH/RT = 0.000524 TEMP = 400, AVER ERR HH/RT = 0.000202

HAX ERR S/R = 0.000594 TEMP = 400. AVER ERR SIR = 0.000198

HAX ERR GH/RT = 0.0005_4 TEMP = 250. AVER ERR GH/RT = 0.000144

H2 Hydrogen. GLUSHKO ET.AL. vl, pt2, ]978, pp5]-32. T range =

MAX REL ERR CP/R = 0.000427 TEMP = 1100. AVER REL ERR CP/R = 0.000120

MAX REL ERR HH/RT = 0.000078 TEHP = 1300. AVER REL ERR HH/RT = 0.000016

HA× REL ERR S/R = 0.000008 TEHP = 1000. AVER REL ERR S/R = 0.000002

MAX REL ERR GH/RT = 0.000012 TEHP = 1100. AVER REL ERR GH/RT = 0.000005

rlA× ERR CP/R = 0.001569 TEMP = 1100. AVER ERR CP/R = 0.000534

MAX ERR HH/RT = 0.000277 TEMP = 1300. AVER ERR HH/RT = 0.000061

MAX ERR S/R = 0.000151 TEMP = 1000. AVER ERR S/R = 0.000055

MAX ERR GH/RT = 0.000196 TEMP = 1100. AVER ERR GH/RT = 0.000066

H2

MAX REL ERR CP/R =

HAX REL ERR HH/RT =

MAX REL ERR S/R =

HAX REL ERR GH/RT =

MAX ERR CP/R =

MAX ERR HH/RT =

MAX ERR S/R =

MAX ERR GH/RT =

Hydrogen. GLUSHKO ET.AL. vl, p_2, 1978, Pp31-32.

0.000310 TEMP = 6000. AVER REL ERR CP/R =

0.000024 TEHP = 6600. AVER REL ERR HH/RT =

0.000004 TEMP = 12500. AVER REL ERR S/R =

0.000004 TEMP = 6600, AVER REL ERR GH/RT =

0.001564 TEMP = 6000. AVER ERR CP/R =

0.000106 TEMP = 6600. AVER ERR HH/RT =

0.000118 TEMP = 12500. AVER ERR S/R =

0.000089 TEMP = 14500. AVER ERR GH/RT =

He Helium. NSRDS-NBS 55, 1971. Temperature cutoff.

MAX RFL ERR CP/R = 0.000324 TEMP = 17500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0,000057 TEMP = 19500. AVER REL ERR HH/RT =

HA× REL ERR S/R = 0.000006 TEHP • 19500. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000001 TEMP = 20000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000812 TEMP = 17500. AVER ERR CP/R =

MAX ERR HH/RT = 0.000142 TEHP = 19500. AVER ERR HH/RT =

HAX ERR S/R = 0.000154 TEMP = 19500. AVER ERR S/R =

HAX ERR GH/RT = 0.000015 TEMP = 20000. AVER ERR GH/RT =

Hg(cr) Mercury Tetragonal Crystal, JANAF, Dec. 1961

HAX REL ERR CP/R = 0.000105 TEMP = 150. AVER REL

MAX REL ERR HH/RT = 0.000185 TEHP = 100. AVER REL

MAX REL ERR S/R = 0.000038 TEHP = 100. AVER REL

MAX REL ERR GH/RT = 0.000087 TEHP = 100. AVER REL

HAX ERR CP/R = 0.000319 TEMP = 150. AVER

HAX ERR HH/RT = 0.000580 TEMP = 100, AVER

HAX ERR S/R = 0.000170 TEHP = 100. AVER

HA× ERR GH/RT = 0.000210 TEHP = 100. AVER

HE(l) Mercury Liquid. JAHAF, Dec. 1961.

MAX REL ERR CP/R = 0.000108 TEMP = 298.

MAX REL ERR HH/RT = 0.000086 TEMP = 350.

MAX REL ERR S/R = 0.000025 TEMP = 300.

MAX REL ERR GH/RT = 0.000032 TEHP = 250.

MAX ERR CP/R = 0.000565 TEMP = 298.

MAX ERR HH/RT = 0.000528 TEMP = 550.

MAX ERR S/R = 0.000208 TEMP = 300.

MAX ERR GH/RT = 0.0001_9 TEMP = 250.

ERR CP/R =

ERR HH/RT =

ERR S/R =

ERR OH/RT =

ERR CP/R =

ERR HH/RT =

ERR $/R =

ERR GH/RT =

T range =

0.000097

0.000008

0.000001

0.000001

0.000_17

0.000055

0.0000_0

0.000034

T range =

0.000042

0.000008

0.000001

0.000000

0.000105

0.000020

0.00002_

0.00000_

T range =

0.000037

0.000080

0.000014

0,0000_0

0.000115

0.000177

0.000068

0.000121

T range =

AVER REL ERR CPIR = 0.000044

AVER REL ERR HH/RT = 0.000039

AVER REL ERR $/R = 0.000014

AVER REL ERR GH/RT = 0.000011

AVER ERR CP/R = 0.000147

AVER ERR HH/RT = 0.000]42

AVER ERR S/R = 0.000137

AVER ERR GH/RT = 0.000065

200.000 _o _00.000 K

REL LST SQ ERR CP/R = 0.000058

REL LST $0 ERR HH/RT = 0.000275

REL LST $Q ERR S/R = 0.000171

REL LST SQ ERR GH/RT = 0.000703

LST SQ ERR CP/R = 0.000162

LST SQ ERR HH/RT = 0.000405

LST SO ERR S/R : 0.000461

LST SQ ERR GH/RT = 0,000846

400.000 _o 1211.400 K

REL LST SO ERR CP/R = 0.000005

REL LST SO ERR HH/RT = 0.000002

REL LST SQ ERR S/R = 0.000005

REL LST SQ ERR GH/RT = 0.000009

LST SQ ERR CP/_ = 0.000014

LST SQ ERR HH/RT 0.000006

LST SQ ERR S/R = 0.000029

LST SQ ERR GH/RT = 0.000031

200,000 to lO00.O00 K

REL LST SQ ERR CP/R = 0.000217

REL LST SO ERR HH/RT = 0.000080

REL LST S_ ERR S/R = 0.000013

REL L3T SQ ERR GH/RT = 0.000017

LST SQ ERR CP/R = 0.000758

LST SQ ERR HH/RT = 0.000275

LST SQ ERR S/R = 0.000222

LST SQ ERR GH/RT = 0.000206

1000.000 to 6000.000 K

REL LST SQ ERR CP/R = 0.000144

REL LST SO ERR HH/RT = 0.000023

REL LST SO ERR S/R = 0.000003

REL LST SO ERR GH/RT = 0.000004

LST SQ ERR CP/R = 0.000628

LST SQ ERR HH/RT = 0.000086

LST SQ ERR S/R = 0.000067

LST SQ ERR GH/RT = 0.000083

6000.000 to 20000.000 K

REL LST Sq ERR CP/R = 0.000117

REL LST 5@ ERR HH/RT = 0.000010

REL LST SQ ERR S/R = 0.000002

REL LST SO ERR GH/RT = 0.000002

LST SO ERR CP/R = 0.0005]8

LS7 SQ ERR HH/RT 0.000044

LST SQ ERR S/R = 0.0000_9

LST SO ERR GH/RT = 0.0000_2

6000.000 to 20000.000 K

REL LST SQ ERR CP/R = 0.000078

REL LST SO ERR HH/RT = 0.000017

REL LST SO ERR S/R = 0.000002

REL LST SQ ERR GH/RT = 0.000000

LST SQ ERR CP/R = 0.000195

LST Sq ERR HH/RT = 0.000043

LST SO ERR S/R = 0.0000_6

LST 50 ERR GH/RT = 0.000005

100.000 _o 2_4.290 K

REL LST SQ ERR CP/R = 0.000054

REL LST SQ ERR HH/RT = 0.00010_

REL LST SQ ERR S/R = 0.000020

REL LST 50 ERR GH/RT = 0.000051

LST Sq ERR CP/R = 0.000167

LST $Q ERR HH/RT = 0.000223

LST 5Q ERR SIR = 0.000094

LST SQ ERR GH/RT = 0.000146

Z34.290 to 600.000 K

REL LST SQ ERR CP/R - 0.000055

REL LST 50 ERR HH/RT = 0.000046

REL LST S_ ERR S/R = 0,000016

REL LST SQ ERR GH/RT = 0.000015

LST SQ ERR CP/R = 0.000184

LST SQ ERR HH/RT = 0.000171

LST SQ ERR S/R = 0.000157

LST SQ ERR GH/RT = 0.000084

210 NASA/TP-3287/REV 1
TABLE X.- Continued.

HE(1) Mercury Liquid. JANAF, Dec. I961.

MAX REL ERR CP/R = 0.000081 TEHP = 800, AVER REL

MAX REL ERR HH/RT = 0,000022 TEMP = 900. AVER REI

MAX REL ERR 5/R = 0.000007 TEHP = 1200. AVER REL

MAX REL ERR GH/RT = 0.000015 TEMP = 900, AVER REL

HAX ERR CP/R = 0.000269 TEHP = 800. AVER

MAX ERR HH/RT = 0.000076 TEMP = 900. AVER

MAX ERR S/R = 0.000102 TEMP = 1200. AVER

MAX ERR GH/RT = 0.000144 TEHP = 900. AVER

T range =

ERR CP/R = 0.000035

ERR HH/RT 0.000010

ERR S/R = 0.000003

ERR GH/RT = 0.000007

ERR CP/R = 0.000122

ERR HH/RT : 0.000033

ERR S/R = 0.0000_3

ERR GH/RT = 0.000071

II(cr) Iodine Rhombic Crvstal, TPIS 1989, vl, ptI, p515. T range =

MAX REL ERR CP/R : 0.002344 TEMP = 320. AVER REL ERR CP/R = 0.000446

MAX REL ERR HH/RT = 0.000232 TEHP = 200. AVER REL ERR HH/RT = 0.000057

MAX REL ERR S/R = 0.000101 TEHP = 200, AVER REL ERR S/R = 0.000022

MAX REL ERR GH/RT = 0.0000_6 TEMP = 270. AVER REL ERR GH/RT = 0.000010

MAX ERR CP/R = 0.015607 TEMP = 320. AVER ERR CP/R = 0.002953

MAX ERR HH/RT = 0.001115 TEMP = 200, AVER ERR HH/RT = 0,000292

HAX ERR S/R = 0.0011_8 TEMP = 200. AVER ERR S/R = 0.000285

MAX ERR GH/RT = 0.000372 TEMP = 270. AVER ERR GH/RT = 0.000082

K(cr) Potassium Cub£c Crystal.

HAX REL ERR CP/R = 0.00058_ TEMP =

MAX REL ERR HH/RT = 0.000237 TEMP =

MAX REL ERR 5/R = 0.000102 TEMP =

MAX REL ERR GH/RT = 0.000172 TEMP =

MAX ERR CP/R = 0.002085 TEMP =

MAX ERR HH/RT = 0.000701 TEMP =

MAX ERR S/R = O.O00B_O TEMP =

MAX ERR GH/RT 0.000660 TEMP =

600,000 to 2000.000 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT

REL LST SQ ERR S/R =

REL LST SQ ERR GH/RT =

LST SQ ERR CP/R =

LST SO ERR HH/RT =

LST SQ ERR S/R =

LST $0 ERR GH/RI =

200.000 _o 386,750 R

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST Sq ERR S/R =

REL LST SO ERR GH/RT =

LST Sq ERR CP/R =

LST SO ERR MH/RT =

LST SQ ERR S/R =

LST SQ ERR GH/RT =

CODATA 1909, p257. T range = 200.090 to 336.860 K

300. AVER REL ERR CP/R = 0,000156 REL LST 50 ERR CP/R =

337. AVER REL ERR HH/RT = 0.000105 REL LST SO ERR HH/RT =

357. AVER REL ERR 5/R = 0.000036 REL LST SQ ERR S/R =

ZOO, AVER REL ERR GH/RT = 0.000055 REL LST $Q ERR GH/RT =

300. AVER ERR CP/R = 0.000558 LST SO ERR CP/R =

337. AVER ERR HH/RT = 0.000295 LST SO ERR HH/RT =

337, AVER ERR S/R = 0.000282 LST SQ ERR 5/R =

200. AVER ERR GH/RT = 0.000227 LST SQ ERR GH/RT =

K(I) Potassium Liquid. CODATA 198% p257. T range =

MAX REL ERR CP/R = 0.000269 TEMP = Q00. AVER REL ERR CP/R = 0.000055

MAX REL ERR HH/RT = 0.000185 TEMP = 337. AVER REL ERR Hff/RT = 0.000036

MAX REL ERR S/R = 0,000093 TEMP = 337. AVER REL ERR 5/R = 0.000024

MAX REL ERR GH/RT = 0.0000_1 TEMP = 600, AVER REL ERR GH/RT = 0.000028

MAX ERR CP/R = 0.001022 TEHP = 000. AVER ERR CP/R = 0.000211

MAX ERR HH/RT = 0.000701 TEMP = 337. AVER ERR HH/RT = 0.000138

MAX ERR SIR = 0.000840 TEMP = 337. AVER ERR 5/R = 0.000290

MAX ERR GH/RT = 0.000359 TEMP = 900. AVER ERR GH/RT = 0.000261

Kr Krypton. NSRDS-N_S 35, 1971. Temperature cutoff.

MAX REL ERR CP/R = 0.000008 TEMP = 6000. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000000 TEMP = 6000. AVER REL ERR HH/RT =

MAX REL ERR SIR = 0.000000 TEMP = 6000. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000000 TEMP = 6000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000021 TEMP = 6000. AVER ERR CP/R =

MAX ERR HH/RT 0.000001 TEMP = 6000. AVER ERR HH/RT =

MAX ERR S/R = 0.000001 TEMP = 6000. AVER ERR 5/R =

MAX ERR GH/RT = 0.000000 TEMP = 6000, AVER ERR GH/RT =

Kr Krypton. NSRD$-NBS 35, 1971. Temperature cutoff.

MAX REL ERR CP/R = 0.021578 TEMP = 13500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.022716 TEMP = 20000. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.002741 TEMP = 20000. AVER REL ERR 5/R =

MAX REL ERR GH/RT = 0.000519 TEHP = 20000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.071605 TEMP = 19000. AVER ERR CP/R =

MAX ERR HH/RT = 0.070378 TEMP = 20000. AVER ERR HH/RT =

MAX ERR S/R = 0.084823 TEMP = 20000. AVER ERR 5/R =

MAX ERR GH/RT = 0.010445 TEMP = 20000. AVER ERR GH/RT =

0,000040

0.00O011

0.800004

0.000009

0.000139

0.000039

0.000052

0,000083

0.000682

0.000085

0.000055

0.00O015

0.004529

0,000422

0.000429

0.000121

0.000293

0,000143

0.000055

O.O00O&_

O.O010qq

0.000_09

0.000_30

0.0003_I

336.860 to 2200,000 K

REL LST SQ ERR CP/R = 0.000090

REL LST SQ ERR HH/RT = 0.000059

REL LST SQ ERR S/R = 0.000033

REL LST 5Q ERR GH/RT = 0.000028

LST SQ ERR CP/R = 0.000353

LST 50 ERR HH/R_ = 0.000225

LST 50 ERR 5/R = 0.000344

LST 5Q ERR GH/RT = 0.000268

Li(cr) Lithium Crystal. Gurvich 19B2,vIV,p_ Z,p245;p_ 2,p286.

MAX REL ERR CP/R = 0.000382 TEMP = 250. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0..002515 TEMP = ZOO. AVER REL ERR HH/RT =

MAX REL ERR SIR = 0.000075 TEMP = 200. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.003132 TEMP = 200. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.001074 TEMP = 250, AVER ERR CP/R =

MAX ERR HH/RT = 0.003255 TEMP = 200. AVER ERR HH/RT =

MAX ERR $/R = 0.000180 TEMP = 200, AVER ERR S/R =

MAX ERR GH/RT = 0.003075 TEHP = 200, AVER ERR GH/RT =

Li(cr) Lithium Crystal, Gurvich 1982,vZV,pt 1,pZ45;pt 2,p286.

MAX REL ERR CP/R = 0.000010 TEMP = 300, AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000001 TEMP = 350. AVER REL ERR HH/RT =

MAX REL ERR $/R = 0.000001 TEMP = 350. AVER REL ERR SIR =

MAX REL ERR GH/RT = 0.000000 TEMP = 450. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000029 TEMP = 500. AVER ERR CP/R =

MAX ERR HH/RT = 0.000002 TEHP = 550. AVER ERR HH/RT =

MAX ERR 5/R = 0.000002 TEMP = 350. AVER ERR 5/R =

MAX ERR GH/RT = 0.000001 TEHP = 454. AVER ERR GH/RT

T range = 1000.000 to 6000.000 K

0.000001 REL LST 50 ERR CP/R =

0.000000 REL LST S_ ERR HH/RT =

0.000000 REL LST SQ ERR S/R =

0.000000 REL LST sq ERR GH/RT =

0.000001 LST SQ ERR CP/R

0.000000 LST 5Q ERR HHIRT =

0.000000 LST SQ ERR S/R =

0.000000 LiT SQ ERR GH/RT =

6000.000 to 20000.000 K

REL LST SQ ERR CP/R =

REL LST SO ERR HH/RT =

REL LST 5Q ERR SIR =

REL LST 50 ERR GH/RT

LST $0 ERR CP/R =

LST SQ ERR HH/RT =

LST SQ ERR S/R =

LST 50 ERR GH/RT =

200.000 to 298.150 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST SQ ERR 5/R =

REL LST $0 ERR GH/RT =

LST SQ ERR CP/R =

LST SO ERR HH/RT =

LST SQ ERR S/R =

LST 5Q ERR GH/RT =

298,150 ¢o 453.690 K

REL LST SQ ERR CP/R =

REL LST SQ ERR flH/RT =

REL LST SQ ERR 5/R =

REL LST SO ERR GH/RT =

LST SQ ERR CP/R =

LST _q ERR HH/RT =

LST SQ ERR S/R =

LST sq ERR GH/RT =

T range =

0,005650

0,001650

0,0001_9

0.00003_

0.010127

0,004768

0.005730

0.001032

T tango =

0.000164

0.000839

0.0000_5

0.001005

0.000453

0.001198

0.000120

0,001678

T range =

0.000002

0.000000

0.000000

0,000000

0.000007

0.000001

0.000001

0.000000

0.000002

0.000000

0.000000

0.000000

O.O0000q

0.000000

0.000000

0.000000

0.007376

0.004231

0.000509

0.000099

0,025027

0.012991

0,015709

0.0027_2

0.000229

0.001302

0.000056

0.001010

0.000602

0.001889

0.000146

0.001778

0,000004

0.000001

0.000000

0.000000

0.000013

0,000001

0.000001

0.000000

NAS A/TP-3287/REV 1 211
TABLE X.- Continued.

Mn(a) Manganese Alpha crystal

MAX REL ERR CP/R = 0.002124 TEMP =

MAX REL ERR HH/RT = 0.002445 TEMP =

MAX REL ERR 5/R = 0.001259 TEMP =

MAX REL ERR GH/RT = 0.000582 TEMP =

MAX ERR CP/R = 0.0079_6 TEHP =

MAX ERR HH/RT = 0.006552 TEHP =

MAX ERR S/R = 0.007073 TEHP =

MAX ERR GH/RT = 0.002917 TEHP =

JANAF Sep.1967.

550. AVER REL ERR CP/R =

500. AVER REL ERR HH/RT =

500. AVER REL ERR SIR =

980. AVER REL ERR GH/RT =

550. AVER ERR CP/R =

500, AVER ERR HH/RT =

500. AVER ERR S/R =

980. AVER ERR GH/RT

Mnlb) I_nganeme )eta crystal.

MAX REL ERR CP/R = 0.000604 TEMP =

MAX REL ERR HH/RT = 0.000499 TEHP =

MAX REL ERR $/R = 0.0005_7 IEMP =

MAX REL ERR GH/RT = 0.000582 TEMP =

MAX ERR CP/R = 0.003138 TEMP =

MAX ERR HH/RT = 0.001795 TEMP =

MAX ERR S/R = 0.004725 TEMP =

MAX ERR GH/RT = 0.003357 TEHP =

JAHAF 3ep.1967,

1100 AVER REL ERR CP/R =

980 AVER REL ERR HH/RT =

980 AVER REL ERR S/R =

980 AVER REL ERR GH/RT =

1100 AVER ERR CP/R =

980 AVER ERR HH/RT =

1000 AVER ERR 5/R =

1361 AVER ERR GH/RT =

Mn(¢) Manganese Gamma crysCal.

MAX REL ERR CP/R = 0.000060 TEMP =

MAX REL ERR HH/RT = 0.000210 TEHP =

MAX REL ERR S/R = 0.000409 TEHP =

MAX REL ERR OH/AT = 0.000538 TEMP =

MAX ERR CP/R = 0.000515 TEMP =

MAX ERR HH/RT = 0.000856 TEMP =

MAX ERR 5/R : 0.00_213 TEMP =

MAX ERR GH/RT = 0.005557 TEMP =

T range =

0.00076_

0.000720

0.000_77

0.000290

0,002855

0.001945

0.003035

0.001133

Mn(d) Hanganese Delta crystal.

MAX REL ERR CP/R = 0,000139 TEMP =

MAX REL ERR HH/RT = 0.000186 TEMP =

MAX REL ERR S/R = 0.000387 TEMP =

NAX REL ERR GH/RT = 0.000521 TEMP =

MAX ERR CP/R = 0.000771 TEMP =

MAX ERR HH/RT = 0.000795 TEMP =

MAX ERR S/R = 0.00_122 TEMP =

MAX ERR GH/RT = 0.005_30 TEMP =

T ranVe =

0.000186

0.000355

0.000_78

0.000559

0.000859

0.001314

0.004437

0.003123

Mo(cr)

200,000 to

REL LST SQ

REL LST $q

REL LST SQ

REL LST $0

LST SQ

LST SO

LST SQ

LST SQ

980.000 to

REL LST SQ

REL LST SQ

REL LST SQ

REL LST SR

LST SQ

LST Sq

LST SQ

LST SQ

JANAF 5ep.1967. T range = 1361.000 to

1400. AVER REL ERR CP/R = 0.000026 REL LST SQ

1361. AVER REL ERR HH/RT = 0.000197 REL LST $0

1361. AVER REL ERR S/R = 0,000399 REL LST Sq

1561. AVER REL ERR GH/RT : 0.000529 REL LST Sq

1_00. AVER ERR CP/R = 0.000138 LST SQ

1561, AVER ERR HH/RT = 0.000808 LST SQ

1361. AVER ERR 5/R = o.00_154 LST $0

1361. AVER ERR GH/RT = 0,0033_5 LST 5q

JANAF Sep.1967.

1500 AVER REL ERR CP/R :

1412 AVER REL ERR HH/RT =

1_12 AVER REL ERR S/R =

1_12 AVER REL ERR OH/AT =

1500 AVER ERR CP/R :

1412 AVER ERR HH/RT =

1412. AVER ERR S/R =

1519. AVER ERR GH/RT =

T rmnge =

0.000068

0.000160

0.000373

0.000514

0.000374

0.000690

0.004070

0.003380

Molybdenum Crystal. JANAF Mar.1978. T range =

RAX REE ERR C_/R • 0.00_55_ TE_P = 455.

MAX REL ERR HH/RT = 0.000375 TEMP = 200.

MAX REL ERR S/R = 0.000117 TEMP = ZOO.

MAX REL ERR GH/RT = 0.000267 TEMP = 200.

MAX ERR CP/R = 0,001087 TEMP = 450.

MAX ERR HH/RT = 0.000526 TEMP = 200.

MAX ERR SIR = 0.000275 TEMP = 200.

MAX ERR GH/RT = 0.000251 TEMP : 200.

Mo(cr) Molybdenum Crystal, JAHAF _ar.1978.

MAX REL ERR CP/R = 0,000103 TEMP • 1200.

MAX REL ERR HH/RT = 0.0000_6 TEMP = 1200.

MAX REL ERR S/R = 0.000027 TEMP = 1200.

MAX REL ERR GH/RT = 0.000052 TEHP = ]100.

MAX ERR CP/R = 0,000566 TEMP = 1200.

MAX ERR HH/RT = 0.000105 TEMP • 1200.

MAX ERR S/R = 0.000214 TEMP = 1200.

MAX ERR GH/RT = 0.000149 TEMP = 1100.

0,000L15

0.000056

0.00002_

0.000040

0.000354

0.000102

0.000096

0.000068

A_ER REL ERR CP/R =

AVER REL ERR HH/RT =

AVER REL ERR 5/R =

AVER REL ERR GH/RT =

AVER ERR CPIR =

AVER ERR HH/RT =

AVER ERR S/R =

AVER ERR GH/RT =

1412.000 to

REL LST SQ

REL LST SQ

REL LST $0

REL LST Sq

LST SQ

LST 5Q

LST Sg

LST SQ

200.000 to

Mo(cr) Molybdenum Cryltal. JANAF Nat.1978.

MAX REL ERR CP/R = 0.002528 TEMP = 2800.

MAX REL ERR HH/RT = 0.000068 TEMP = 2700.

MAX REL ERR SIR = 0.00002_ TEMP = 2700.

HAX REL ERR OH/RT = 0.000019 TEMP = 2500.

MAX ERR CP/R = 0.015682 TEMP = 2800.

MAX ERR HH/RT = 0.000256 TEMP : 2700,

MAX ERR 5/R = 0.000264 TEMP = 2700.

MAX ERR GH/RT = 0.000138 TEMP = 2500.

AEL LST Sq

REL LST Sq

REL LST SQ

REL LST SQ

LST SO

LST sq

LST SQ

LST sq

T range = 1_0_.000 _o

AVER REL ERR CP/R = 0.000040 REL LST SQ

AVER REL ERR HH/RT = 0.000011 REL LST 5q

AVER REL ERR S/R = 0.000014 REL LST SQ

AVER REL ERR GH/RT = 0.000017 REL LST SQ

AVER ERR CP/R = 0.000156 LST SQ

AVER ERR HH/RT = 0.000053 LST SO

AVER ERR S/R : 0,000116 LST SQ

AVER ERR GH/RT = 0.000096 LST SQ

T range = 2200.000 to

AVER REL ERR CP/R = 0.000880 REL LST SO

AVER REL ERR HH/RT = 0.000034 REL LST SQ

AVER REL ERR $/R = 0.000012 REL LST Sq

AVER REI ERR GH/RT = 0.000011 REL LST sq

AVER ERR CP/R = 0.005188 LST SQ

AVER ERR HH/RT = 0.000129 lST Sq

AVER ERR $/R = 0,000137 LST Sq

AVER ERR GH/RT = 0.000080 LST SQ

980.000 K

ERR CP/R = 0.00106_

ERR HH/RT 0.001025

ERR S/R = 0.000650

ERR GH/RT = 0.000372

ERR CP/R = 0.003982

ERR HH/RT = 0.002767

ERR S/R = 0.00_029

ERR GH/RT = 0.001581

1361.000 K

ERR CP/R = 0.000307

ERR HH/RT = 0.000371

ERR S/R = 0.000_81

ERR GH/RT = 0.000560

ERR CP/R = 0.001412

ERR HH/RT = 0.001_6_

ERR SIR = 0.0044_2

ERR GH/RT 0.003127

1412.000 K

ERR CP/R = 0,000056

ERR HH/RT = 0.000198

ERR S/R = 0.000399

ERR GH/RT = 0,000529

ERR CP/R = 0.000191

ERR HH/RT = 0.000809

ERR S/R = 0.004154

ERR GH/RT 0.0033_5

1519.000 K

ERR CP/R = 0.000088

ERR HH/RT = 0.000161

ERR S/R = 0.000375

ERR GH/RT = 0.000514

ERR CP/R = 0.000489

ERR HH/RT = 0.00069_

ERR S/R = 0.004070

ERR GH/RT = 0.003380

I000.000 K

EAR CP/R = 0.000145

ERR flH/RT = 0.000109

ERR S/R = 0.000038

ERR GH/RT 0,000078

ERR CP/R = 0.000444

ERR HH/RT = 6.000167

ERR S/R = 0.000122

ERR GH/RT = 0.00009_

2200.006

ERR CP/R = 0.000051

ERR HH/RT = 0.000015

ERR S/R = 0.000015

ERR GH/RT = 0.000018

ERR CP/R = 0.000196

ERR HH/RT = 0.00004_

ERR S/R = 0.000125

ERR GH/RT = 0.000099

2896.000 K

ERR CP/R = 0.001173

ERR HH/RT = 0.000041

ERR S/R = 0.00001_

ERR GH/RT = 0.000012

ERR CP/R = 0.007067

ERR HH/RT = 0,000155

ERR S/R = 0.000160

ERR GH/RT = 0.000089

212 NASA/TP-3287/REV l
TABLE X. - Continued.

N? Nitrogen. GLUSHKO ET,AL. vl, pt2, 0207, 1978.

MAX REL ERR CP/R = 0,000056 TEHP = 500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000043 TEMP = 200. AVER REL ERR HH/RT =

HAX REL ERR S/R = 0.000004 TEMP = 200. AVER REL ERR $/R =

MAX REL ERR GH/RT = 0,000014 TEMP = 200, AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000198 TEHP = 500. AVER ERR CP/R =

MAX ERR HH/RT : 0.000151 TEMP : 200. AVER ERR HH/RT =

MAX ERR S/R = 0.000096 TEMP = 200. AVER ERR $/R =

MAX ERR GH/RT = 0.000247 TEHP = 200. AVER ERR GH/RT =

N2

MAX REL ERR CP/R =

MAX REL ERR HH/RT =

MAX REL ERR 5/R =

MAX REL ERR GH/RT =

MAX ERR CP/R ;

MAX ERR HH/RT =

MAX ERR S/R =

MAX ERR GH/RT =

Nitrogen, GLUSHKO ET,AL, vl, pt2, 0207s 1978.

0.000025 _EMP = 1200. AVER REL ERR CP/R =

0.000017 TEMP = 1100, AVER REL ERR HH/RT =

0,000002 TEMP = 1200, AVER REL ERR S/R =

0.000004 TEMP = 1200. AVER REL ERR GH/RT =

0.000100 TEMP = 1200. AVER ERR CP/R =

0.000061 TEHP = 1100. AVER ERR HH/RT =

0.000068 TEMP = 1200. AVER ERR S/R =

0.000091 TEMP = L200. AVER ERR GH/RT =

N2 Nitrogen. GLUSNKO ET.AL. vl, pt2, 0207, 1978.

MAX REL ERR CP/R = 0.002336 TEMP = 20000. AVER REL ERR CP/R =

MAX REL ERR Hfl/RT = 0.000210 TEHP = 12000. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000032 TEMP = 12000. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000012 TEMP = 20000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.016949 7ERr = 20000. AVER ERR CP/R =

MAX ERR HH/RT = 0,001013 TEHP = 12000. AVER ERR HH/RT =

HAX ERR S/R = O.OOlZZB TEMP = 12000. AVER ERR S/R =

MAX ERR GH/RT = 0.000454 TEMP = 20000. AVER ERR GH/RT =

Na(cr) 5odium Cubic Crystal. CODATA 1989t p254.

MAX REL ERR CP/R = 0,000942 TEMP = 300, AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.001032 TEMP = 371. AVER REL ERR HN/RT

HAX REL ERR S/R = 0.000490 TEMP = 200. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.001165 TEHP = 200. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.005200 TEMP = 300. AVER ERR CP/R =

MAX ERR HH/RT = 0.002881 TEHP = 37L, AVER ERR HH/RT =

MAX ERR S/R = D.0030qq TEHP = 371. AVER ERR S/R =

MAX ERR GH/RT = 0.003017 TEMP = 200. AVER ERR GH/RT =

Na(l) Sodium Liquid. CODATA 1989, p254.

MAX REL ERR CP/R = 0.001067 TEMP = 500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0,000793 TEMP = 371. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000391 TEMP = 371. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000197 TEMP = 600. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.003933 TEHP = 500. AVER ERR CP/R =

MAX ERR HH/RT = 0.002881 TEMP = 371. AVER ERR HH/RT =

MAX ERR S/R = 0.003044 TEHP = 571. AVER ERR S/R =

MAX ERR GH/RT = 0.001211 TEMP = 800. AVER ERR GH/RT =

Nb(cr) Niobium Crystal, JANAF, Dec. 1973,

MAX REL ERR CP/R = 0.000114 TEMP = 400. AVER REL ERR CP/R =

MAX REL ERR NH/RT = 0,000176 TEMP = 200. AVER REL ERR HH/RT =

HAX REL ERR S/R = 0.000024 TEHP = 250. AVER REL ERR S/R =

HAX REL ERR G1⁄2/RT = 0.000197 TEMP = ZOO, AVER REL ERR GH/RT =

MAX ERR CP/R = 0,0003_9 TEMP = 400. AVER ERR CP/R =

MAX ERR HH/RT = 0.000305 TEMP = 200. AVER ERR HH/RT =

MAX ERR SIR = 0.000096 TEMP = 500. AVER ERR S/R =

MAX ERR GH/RT = 0.000296 TEMP = 200. AVER ERR GH/RT =

Nb(cr) Niobium Crystal. JANAF, Dec. 1973.

MAX REL ERR CP/R = 0.000036 TEMP = 1700. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000022 TEMP = 1200. AVER REL ERR HH/RT

MAX REL ERR S/R = 0.00Q008 TEMP = 1500. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000018 TEMP = 1200. AVER REL ERR'GH/RT =

MAX ERR CP/R = 0.000137 TEMP = 1700. AVER ERR CP/R =

MAX ERR HH/RT = 0.000065 TEMP = 1200. AVER ERR HH/RT

MAX ERR S/R = 0.000081 TEMP = 1500. AVER ERR S/R =

HAX ERR GN/RT = 0.000107 TEMP = 1200. AVER ERR GH/RT =

T range =

0,000017

0.00_013

0.000001

0.000004

0,000063

0,0000_4

0.000035

0,000075

T range =

0.000009

0.000003

0.000001

0.000001

0.000039

O.O000ll

0.000029

0.000034

T range =

0.000893

0,000076

0.000011

0.000005

0.005769

0.000372

0.000421

0.000183

T rBnge =

0.000283

0.000337

0.000233

0.000311

0.000971

0.000905

0.001364

0.000829

T range =

0.000209

0.000145

0.000108

0.000119

0.000769

0.000532

0.001107

0.000955

T range =

0.000031

0.000031

0.000007

0.000037

0.000097

0.000067

0.000038

0.000089

T ranga =

0.000018

0.000005

0.000004

0.000008

0.000065

0.000018

0.000040

0.0000_8

NbCcr) Niobium CrystaI. JANAF, Dec. 197_. T range =

MAX REL ERR CP/R = 0.000636 TEHP = 2700. AVER REL ERR CP/R = 0,000203

MAX REL ERR HH/RT = 0.000023 TEMP = 2600. AVER REL ERR HH/RT = 0.000007

MAX REL ERR 5/R = 0.000009 TEMP = 2600. AVER REL ERR SIR = 0.000004

MAX REL ERR GH/RT = 0.000011 TEMP = 2100. AVER REL ERR GH/RT = 0,000003

MAX ERR CP/R = 0.003235 TEMP = 2700. AVER ERR CP/R = 0,000988

MAX ERR HH/RT = 0.000081 TEMP = 2600. AVER ERR HH/RT = 0.000023

MAX ERR S/R = 0,000105 TEMP = 2600. AVER ERR S/R = 0.000042

MAX ERR GH/RT = 0.000067 TEMP = 2100. AVER ERR GH/RT = 0.000036

200,000 to 1000.000 K

REL LST SO ERR CP/R = O,OO00Zq

EEL LST SQ ERR HH/RT = 0.000017

REL LST SQ ERR S/R = 0.000002

REL LST SQ ERR GH/RT = 0.000005

LST SQ ERR CP/R = 0,000086

LST SQ ERR NH/RT = 0.000061

LST SO ERR $/R = 0.000043

LST SO ERR GH/RT = 0.000095

1000.000 to 6000.000 K

REt LST SQ ERR CP/R = O.O000[Z

REL LST SO ERR HHIRT = O_OODO04

REL LST SQ ERR S/R = O.OODOO[

REL LST SQ ERR GH/RT = 0.000001

LST SQ ERR CP/R = 0.0000_7

LST SQ ERR HH/RT = 0.000015

LST SQ ERR SIR = 0.000053

LST SQ ERR GN/RT = 0.000039

6000.000 to 20000.000 K

REL IST SO ERR CP/R = 0.001038

REL LST SQ ERR HH/RT = 0,000092

REL LST SO ERR S/R = 0.00001_

REL LST SQ ERR GH/RT = 0.000006

LST SQ ERR CP/R = 0.007000

LST 50 ERR HH/RT = 0.000448

LST $0 ERR S/R = 0.0005_4

LST SQ ERR GM/RT = 0.000219

200.000 _o 371,010 K

REL LST SO ERR CP/R = 0.000476

REL LST SQ ERR HH/RT = 0.000534

RE/ LST SQ ERR SIR = 0.000329

REL LST SQ ERR GH/RT = 0.000583

LST SO ERR CP/R = 0.001621

LST sq ERR HH/RT = 0.001_76

LST SQ ERR S/R = 0.001935

LST S@ ERR GH/RT = 0.001512

371.010 to 2300.000 K

REL IST SO ERR CP/R = 0,000343

REL LST SQ ERR HH/RT = 0.000251

REL LST sq ERR S/R = 0.000146

REL LST SQ ERR GN/RT = 0.000125

LST Sq ERR CP/R = 0.001258

LST SQ ERR HH/RT = 0.000916

LST Sq ERR S/R = 0.001314

LST SQ ERR GH/RT = 0,000986

200,000 to I000,000 K

REL 1ST SQ ERR CPIR = 0.000045

REL LST Sq ERR HH/RT = 0.000054

REL LST Sq ERR S/R = 0.000011

REL LST Sq ERR GH/RT = 0.000065

LST SQ ERR CP/R = 0.000137

LST Sg ERR HH/RT = 0.000103

LST 50 ERR S/R = 0.000054

LST SQ ERR GH/RT = 0,000121

1000.000 to 2000.000 K

REL LST Sg ERR CP/R = 0.000023

REL LST SQ ERR HH/RT = 0.00D008

REL LST SQ ERR S/R = 0.000005

REL LST SQ ERR GH/RT = 0.000009

LST SO ERR CP/R = 0.000082

LST SQ ERR NH/RT = 0.000024

LST SQ ERR S/R = 0.000044

LST SO ERR GH/RT 0.000054

2000.000 to 2750.000 K

REL LST 50 ERR CP/R = 0.000289

REL LST SO ERR HH/RT = 0.000009

REL LST SQ ERR S/R = 0,000005

REL LST Sq ERR GH/RT = 0.000006

LST SQ ERR CP/R = 0.001441

LST SO ERR HH/RT = 0.000033

LST S_ ERR S/R = 0.000053

LST Sq ERR GH/RT = 0.000045

NASA/TP-3287/REV 1 213
TABLE X.- Continued.

No Neon. NSRDS-NBS 35, 1971, Temperature cutoff.

MAX REL ERR CP/R = 0.002585 TEHP = 17500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000465 TEMP = 19000. AVER REL ERR HH/RT =

HAX REL ERR 5/R = 0.000046 TEMP = 19500. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000006 TEHP = 20000. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.006625 TEMP = 17500. AVER ERR CP/R =

HAX ERR HH/RT = 0.001167 TEHP = 19000. AVER ERR HH/RT =

MAX ERR S/R = 0.001288 TEHP = 19500. AVER ERR S/R =

HAX ERR GH/RT = 0.000165 TEHP = 20000. AVER ERR GH/RT =

T range =

0.000386

0.000083

0.000009

0.000002

0.000983

0.000208

0.000242

0.000044

Hi(or) Nickel Crystal below lambda trens 631K. JANAF Dac.1976. T range =

MAX REL ERR CP/R = 0.000661 TEMP = 300. AVER REL ERR CP/R = 0.000141

MAX REL ERR HH/RT = 0.000382 TEHP = 200. AVER REL ERR HH/RT = 0.000161

HAX REL ERR S/R = 0.000144 TEHP = 350. AVER REL ERR $/R = 0.000041

HAX REL ERR GH/RT = 0.000372 TEHP = 200. AVER REL ERR GH/RT = 0.000123

MAX ERR CP/R = 0.002069 TEMP = 300. AVER ERR CP/R = 0.000437

HAX ERR HH/RT = 0.000692 TEHP = 350. AVER ERR HH/RT = 0.000284

HAX ERR SIR = 0.000592 TEHP = 350. AVER ERR S/R = 0.000147

HAX ERR GH/RT = 0.000367 TEMP = 200. AVER ERR GH/RT = 0.000155

Ni(cr) Nickel Crystal below lambda _rans 631K. JANAF Dec.1976. T range =

HAX REL ERR CP/R = 0.901505 TENP = 450. AVER REL ERR CP/R = 0.000458

HAX REL ERR HH/RT = 0.001880 7ENP = 631. AVER REL ERR HH/RT = 0.081008

HAX REL ERR 5/R = 0.001053 TEHP = 631. AVER REL ERR 5/R = 0.000596

RAX REL ERR GH/RT = 0.000569 TEMP = 631, AVER REL ERR GH/RT = 0.000235

MAX ERR CP/R = 0.005563 TEMP = 450. AVER ERR CP/R = 0.001726

MAX ERR HH/RT = 0.005350 TEMP = 631. AVER ERR HH/RT = 0.002652

MAX ERR S/R = 0.006618 TEMP = 631. AVER ERR SIR = 0.003381

MAX ERR GH/RT = 0.001268 TEMP = 631. AVER ERR GH/RT = 0.000734

Nifcr) Hickel Cryste] above lambda trans 631K. JANAF Dec.1976. T range =

MAX RE[ ERR CP/R = 0.007181 TEHP = 700. AVER REL ERR CP/R = 0.002420

MAX REL ERR HH/RT = 0.008451 TEHP = 700. AVER REL ERR HH/RT = 0.004102

HAX REL ERR S/R = 0.004226 TEMP = 700. AVER REL ERR 5/R = 0.002589

MAX REL ERR GH/RT : 0.001988 TEMP = 1200. AVER REL ERR GH/RT = 0.001467

MAX ERR CP/R _ 0.0?6596 TEMP = 700. AVER ERR CP/R = 0.009129

HAX ERR HH/RT = 0.024872 TEHP = 700. AVER ERR HH/RT = 0.012609

HAX ERR $/R = 0.028246 TENP = 700. AVER ERR $/R = 0.019520

MAX ERR GH/RT = 0.010794 TEHP = 1200. AVER ERR GH/RT = 0.006911

6000.000 to ZO000.O00 K

REL LST SQ ERR CP/R = 0.000630

REL LST SQ ERR HH/RT = 0,000161

REL LST Sq ERR S/R • 0.0000]6

NEt LST 50 ERR GH/RT = 0.000002

LST SO ERR CP/R = 0.001612

LST 50 ERR HH/RT = 0,000404

LST 50 ERR 5/R = 0.000447

LST 5q ERR GH/RT = 0.000058

200.000 to _00.000 K

REL LST $g ERR CP/R = 0.000275

REL LST $Q ERR HH/RT 0.000224

REL LST 50 ERR $/R = 0.000067

REL LST 50 ERR GH/RT = 0.000183

LST 50 ERR CP/R = 0.000859

LST 50 ERR HH/RT = 0.000393

LST $0 ERR S/R = 0.000255

LST 50 ERR GH/RT = 0.000208

400.000 to 631.000 K

REL LST 50 ERR CP/R = 0.000736

REL LST $0 ERR HH/RT = 0.001209

REL LST $0 ERR S/R = 0.000689

REL LST 50 ERR GR/RT = 0.000266

LST $0 ERR CP/R = 0.002715

LST 50 ERR HH/RT = 0.003197

LST SO ERR 5/R = 0.003945

LST $Q ERR GH/RT : 0.000853

631.000 to 1200.000 K

REL LST 50 ERR CP/R = 0.003432

REL LST SO ERR HH/RT = 0.004601

REL LST 50 ERR 5/R = 0.002741

REL LST sq ERR GH/RT = 0.001575

LST SQ ERR CP/R = 0.012823

LST 50 ERR HH/RT = 0.013969

LST SO ERR S/R = 0,020434

LST SO ERR GH/RT = 0,007660

Ni(cr) Nzck.l Crystal above lambda trans 631K. JANAF Dec.1976. T range = 1200.000 to 1728.000 K

HAX REL ERR CP/e • 0 C02648 TEHP • 1300. AVER REL ERR CP/R = 0.000996 REL LST SQ ERR CP/R = 0,001271

HAX REL ERR HH?RZ • 000?298 TEHP = 1200. AVER REL ERR HH/RT = 0.001451 REL LST 59 ERR HH/RT = 0.001522

HAX REL ERR S/R • 0 00_106 TEMP = 1200. AVER REL ERR S/R = 0.001776 REL LST SQ ERR S/R = 0.001786

MAX REL ERR G_/R_ , 0 001994 TEMP = 1300. AVER REL ERR OH/RT = 0.001955 REL LST SQ ERR GH/RT = 0.001956

HAX ERR CF'/K • 0 C]09g2 TEHP = 1300. AVER ERR CP/R = 0.004294 LST SQ ERR CP/R = 0.005383

HAX ERR H._RT • C C0,'630 TEHP = 1200. AVER ERR HH/RT = 0.005015 LST SO ERR HH/RT = 0.005213

MAX ERR 5"_ • _ C1_24 TEHP = 1200. AVER ERR 5/R = 0.017015 LST Sg ERR S/R = 0.017032

MAX ERR GH/R? . @ 017734 TEMP = 1700. AVER ERR GH/RT = 0.012000 LST SQ ERR GH/RT : 0.012020

OZ Owyge_ Gurvich et el. vl, pt 2, P9, 1989. T range =

HAX REL ERR EPtR , 0 ¢00_98 TEHP = 250. AVER REL ERR CP/R = 0.000094

MAX REL ERR _e' • C CO(C74 TEHP = 300. AVER REL ERR HH/RT = 0.000015

HAX REL ERR _/R C ¢P(01_ TEMP = 200. AVER REL ERR S/R = 0.000004

MAX REL ERR O,'g T , © O;;_l? TEMP = 200. AVER REL ERR GH/RT = 0.000006

HAX ERR CP,R • 00;O_9S TEHP : 250. AVER ERR CP/R = 0.000354

MAX ERR H_,RI - 0 0:_257 TEHP = 300. AVER ERR HH/RT = 0.00005_

MAX ERR S/R • 0 000_4 TEHP = 200. AVER ERR S/R = 0.000087

HAX ERR OH/RT , 0 0302_2 TEMP = 200. AVER ERR GH/RT = 0.000084

02 O=vean GurvJch at al. vl, pt Z, p9, 1989. T range =

NAX REL ERR CP/R • 0000537 TENP = 1100. AVER REL ERR CP/R = 0.000156

MAX REL ERR HH/RT • 0 000069 TEHP = 1300. AVER REL ERR HH/RT = 0.000018

HAX REL ERR SIR • 0 000012 TEHP = 1300. AVER REL ERR 5/R = 0.000003

MAX REL ERR GH/RT = 0.000005 TEHP = 3300. AVER REL ERR GH/RT 0.000003

HAX ERR CP/R • 0.002282 TEHP = 1100. AVER ERR CP/R = 0.000742

MAX ERR HH/RT • 0.000268 TEHP = 1500. AVER ERR HH/RT 0.000075

blAX ERR S/R = 0.000366 TEHP = 1300. AVER ERR 5/R = 0.000091

HAX ERR GH/RT = 0.000145 TEHP = 3300. AVER ERR GH/RT 0.000076

OZ Oxygen. Gurvich at el. vl_ pt 2, pg, 1989. T range =

MAX REL ERR CP/R = 0.000365 TEMP = 6_00. AVER REL ERR CP/R = 0.000156

MAX REL ERR HH/RT = 0.000038 TEMP = 7000. AVER REL ERR HH/RT = 0.000012

MAX REL ERR S/R = 0.000005 TEHP = 7000. AVER REL ERR SIR = 0.000002

HAX REL ERR GH/RT = 0.000003 TEHP • 8600. AVER REL ERR OH/RT = O.O0000I

HAX ERR CP/R = 0.001940 TEHP = 6400. AVER ERR CP/R = 0.000730

HAX ERR HH/RT = 0.000183 TEHP = 7000. AVER ERR HH/RT = 0.000055

HAX ERR S/R = 0.000178 TEMP = 7000. AVER ERR S/R = 0.000063

MAX ERR GH/RT = 0.000094 TEMP = 8600. AVER ERR GH/RT = 0.000042

200.000 to 1000.000 K

REL LST SQ ERR CP/R = 0.000113

REL LST SO ERR HH/RT = 0.000026

REL LST $0 ERR S/R = 0.000006

REL LST Sq ERR GH/RT = 0.000006

LST SQ ERR CP/R = 0.000420

LST sq ERR NH/RT = 0.000090

LST 50 ERR S/R = 0.000136

LST Sq ERR GH/RT = 0.000117

1000.000 to 6000.000 K

REL LST 50 ERR CP/R = 0.000189

REL LST SQ ERR HH/RT = 0.000024

REL LST SO ERR 5/R = 0.000004

REL LST SO ERR GN/RT = 0.000003

LST sq ERR CP/R = 0.000878

LST $0 ERR HH/RT = 0.000096

LST SO ERR S/R = 0.000124

LST 50 ERR GH/RT = 0.000082

6000.000 to 20000.000 K

REL LST SO ERR CPIR = 0.000175

REL LST SQ ERR HH/RT = 0.000015

REL LST SO ERR 5/R = 0.000002

REL LST SO ERR GH/RT = 0.000001

LST SO ERR CP/R = 0.000843

LST SO ERR HH/RT = 0.000074

LST SO ERR S/R = 0.000078

LST $0 ERR GH/RT = 0.000050

214 NASA/TP-3287/REV l
TABLE X. - Continued.

P(cr) Phosphorus Crystal(Nb_te), TPI$ 1989. JANAF June,1961. T range =

MAX REL ERR CP/R = 0,000617 TEMP = Z00, AVER REL ERR CP/R = 0.00015_

MAX REL ERR HH/RT = 0,000259 TEMP = 210. AVER REL ERR HH/RT = 0.009107

MAX REL ERR S/R = 0,000087 TEHP = 290. AVER REL ERR S/R = 0.000059

HAX REL ERR GH/RT = 0.000143 TEHP = 195. AVER REL ERR GH/RT = 0,000056

HAX ERR CP/R = 0.001564 TEHP = 200. AVER ERR CP/R = 0,000407

NAX ERR HH/RT = 0.000509 TEMP = 230. AVER ERR HH/RT = 0.000217

MAX ERR SiR = 0.000424 TEMP = 290. AVER ERR 5/R = 0.000263

HAX ERR GH/RT = 0,000289 TEMP = ZIO, AVER ERR GH/RT = 0.000130

Pbfcr) Lead Cubic. TPIS 1991, vZ, pAO0, v2, p337. 3 range =

HAX REL ERR CP/R = 0.000458 TEMP = 400. AVER REL ERR CP/R = 0.000175

HA× REL ERR HH/RT 0.002020 TEMP = 200. AVER REL ERR HH/RT = 0.000152

HAX REL ERR S/R = 0.000530 TEP|P = 200, AVER REL ERR 5/R = 0.000049

HAX REL ERR GH/RT : 0.001210 TEHP : ZOO. AVER REL ERR GH/RT = 0.000130

MAX ERR CP/R = 0.001552 TEHP = 400. AVER ERR CP/R = 0.000590

HA× ERR HH/RT = 0.002630 TEHP = 200. AVER ERR HH/RT = 0.000352

HAX ERR S/R = 0.002159 TEMP = 200. AVER ERR S/R = 0.000361

HAX ERR GH/RT = 0.004790 TEHP = ZOO. AVER ERR GH/RT = 0.000535

Rb(cr

PIAX

HA×

MA_

HAX

Rb([)

MAX

MAX

MAX

MAX

Rb(J)

) Rubidium Cubic Crystal. CODATA

REL ERR CP/R = 0.000699 TEMP = _00,

REL ERR HH/RT = 0.001181 TEMP = 100.

REL ERR S/R = 0.000767 TEHP = 200.

REL ERR GH/RT = 0.002037 TEMP = i00,

MAX ERR CP/R = 0.00262_ TEMP = 300.

MAX ERR HH/RT = 0.00205_ TEMP = lO0.

HA× ERR S/R = 0.006021 TEMP = 200.

HA× ERR GH/RT = 0.007879 TEHP = 200.

1989. p260. JAHAF 12/83, T range =

AVER REL ERR CP/R = 0.000214

AVER REL ERR HH/RT = 0.000_24

AVER REL ERR $/R = 0.0003_6

AVER REL ERR GH/RT = 0.000710

AVER ERR CP/R = 0.000775

AVER ERR HH/RT = 0.001126

AVER ERR $/R = 0.002561

AVER ERR GH/RT 0.003043

Rubidium Liquid. CODATA 1989, p260.

REL ERR CP/R = 0.000056 TEMP = _00,

REL ERR HH/RT = 0.000029 TEMP = 500.

REL ERR 5/R = 0.000019 TEMP = 312.

REL ERR GH/RT = 0.000020 TEMP = _00.

HAX ERR CP/R = 0.000207 TEHP = _00,

HAX ERR HH/RT = 0.000112 TEHP = 500,

HAX ERR S/R : 0.000199 TEHP = 322.

MAX ERR GH/RT = 0.000159 TEHP = 600.

Rubidium L2quid, CODATA 1989. p260.

MAX REL ERR CP/R = 0.000019 TEHP = I_00,

_AX REL ERR HH/RT = 0.000013 TEHP = 1400.

HAX R_L ERR SiR = 0.000007 TEMP = 1100.

MAX REL ERR GH/RT : 0.000010 TE_IP : IBgO,

M_X ERR CP/R = 0.000084 TEMP = |400.

MAX ERR HH/RT = 0.000049 TEMP = 1400.

MAX ERR S/R = 0,000101 TEMP = 2000,

MAX ERR GH/RT = 0,000127 TEMP = 1800.

S(a) Sulfur Al.ha Crystal. TPIS 1989.

MAX REL ERR CP/R : 0.000015 TEMP = 300.

ttAX REL ERR HH/RT = 0,000287 TEHP = 200,

HAX REL ERR SiR = 0,000165 TEMP = 200.

MAX REL ERR GH/RT = 0.000600 TEHP = 200.

MAX ERR CP/R = 0,000040 TEMP = 300,

MAX ERR HH/RT = 0,000405 TEMP = 200.

MAX ERR 5/R = 0,000_6_ TEHP = 200.

MAX ERR GH/RT = 0,000866 TEMP = 200.

S(bJ Sulfur Beta Crystal. TPI5 1989.

MAX REL ERR CP/R = 0.000004 TEMP = 388.

MAX REL ERR HH/RT = 0.000245 TEMP = 588.

HAX REL ERR S/R = 0,000019 TEMP = 368.

MAX REL ERR GH/RT = 0.000207 TEMP = 388.

HAX ERR CP/R = 0.000013 TEHP = 388.

MAX ERR HH/RT = 0.000529 TEMP = 388.

HAX ERR S/R = 0.000089 TEMP = 368.

MAX ERR GH/RT 0.000536 TEMP = 388.

T range =

AVER REL ERR CP/R = 0.000017

AVER REL ERR HH/RT = 0.000015

AVER REL ERR SIR = 0.000008

AVER REL ERR GH/RT = 0.000011

AVER ERR CP/R = 0.000063

AVER ERR HH/RT = 0.000059

AVER ERR 5/R = 0.000090

AVER ERR GH/RT = 0.000091

T range =

AVER REL ERR CP/R = 0.000007

AVER REL ERR HH/RT = 0.000007

AVER REL ERR S/R = 0.000005

AVER REL ERR GH/RT = 0,000005

AVER ERR CP/R 0.000030

AVER ERR HH/RT = 0.000027

AVER ERR S/R = 0.000045

AVER ERR GH/RT = 0.000057

195.400 _o 317.300 K

REE LST 50 ERR CP/R =

REL LST 50 ERR HH/RT

REL LST $0 ERR 5/R =

REL LST SQ ERR GH/RT =

LST $0 ERR CP/R =

LST 5_ ERR HH/RT =

LST SO ERR S/R =

LST 5q ERR GH/RT =

200.000 _o 600.650 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST SO ERR S/R =

REL LST SQ ERR GH/RT :

LST SQ ERR CP/R =

LST 5q ERR HH/RT =

LST SO ERR SiR :

LST Sq ERR GH/RT =

0.000221

0.000131

0.000064

0.000073

0,000568

0.000261

0.000288

0,000166

0.0002_2

0.000326

0.000106

0.000383

0.0008]4

0,00084_

0.00070?

0.001516

100.000 to 312,470 K

REL [ST S0 ERR CP/R = 0.000326

REL LST SQ ERR HH/RT = 0.000608

REL LST Sq ERR SIR = 0.000486

REL LST SQ ERR GH/RT : 0.661079

LST SQ ERR CP/R : 0.001201

LST Sq ERR HH/RT = 0.Q01575

LST SQ ERR SiR = 0.003629

LST SQ ERR GH/RT : 0.004438

512,470 _o I000,000 K

REL LST SQ ERR CPIR =

REL LST SQ ERR HH/RT =

REL L$T SQ ERR S/R =

REL LST SQ ERR GH/RT =

LST SO ERR CP/R =

LST $Q ERR HH/RT

L5T SQ ERR S/R =

LST SO ERR GH/RT =

1000.000 %0 2100.000 K

REL LST SO ERR CP/R =

REL LST SO ERR HH/RT =

REL LST SQ ERR S/R =

REL LST SQ ERR GH/RT

LST $Q ERR CP/R :

LST SQ ERR HH/RT :

LST SQ ERR 3/R :

LST SQ ERR GH/RT =

T range • 200.000 to 368.300 K

AVER REL ERR CP/R = 0.000005 REL LST 50 ERR CP/R =

AVER REL ERR HH/RT = 0.000157 REL LST SQ ERR HH/RT =

AVER REL ERR S/R = 0.000050 REL IST 50 ERR S/R =

AVER REL ERR GH/RT = 0.000238 REL LST SQ ERR GH/RT =

AVER ERR CP/R : 0.000013 LST Sg ERR CP/R =

AVER ERR HH/RT = 0.000259 LST 50 ERR HH/RT =

AVER ERR S/R = 0.000153 LST SQ ERR S/R =

AVER ERR GH/RT = 0.000_12 LST SO ERR GN/RT =

T range =

0.000002

0.000180

0,000010

0.000170

0.000007

0.000385

0.000048

0,000432

368.300 to 388.360 K

REL LST Sq ERR CP/R =

REL LST SQ ERR HH/RT =

REL LST SQ ERR SiR =

REL LST SQ ERR GH/RT =

LST 50 ERR CP/R =

LST SO ERR HH/RT =

LST SQ ERR S/R =

LST SQ ERR GH/RT =

200.000 _o 298.150 K

REL LST SQ ERR CP/R =

REL LST SQ ERR HH/RT =

REL lST S_ ERR _/R =

REL LST SQ ERR GH/RT =

LST SQ ERR CP/R =

LST SQ ERR HH/RT =

LST SQ ERR S/R =

L_T S; ERR GH/RT =

T range =

0,000514

0.002554

0.000861

0.001846

0,001082

0.002513

0.001254

0.001059

AVER REL ERR CP/R :

AVER REL ERR HH/RT =

AVER REL ERR S/R =

AVER REL ERR GH/RT =

AVER ERR CP/R =

AVER ERR HH/RT •

AVER ERR $/R =

AVER ERR GH/RT =

Si(cr) Silicon Cubic. TPIS 1991, vl, p237, v2, p220,

MAX REL ERR CP/R = 0.001154 TEMP = 250. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.006458 TEMP : 200. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.002271 TEMP = 200. AVER REL ERR $/R =

MAX REL ERR GH/RT = 0.00_528 TEMP : 200. AVER REL ERR GH/RT =

HAX ERR CP/R = 0.002516 TEMP = 250. AVER ERR CP/R =

MAX ERR HH/RT = 0.005604 TEMP = 200. AVER ERR HH/RT =

MAX ERR S/R : 0.00318_ TEMP = 200, AVER ERR 5/R =

MAX ERR GH/RT = 0,002_19 TEMP = 200. AVER ERR GH/RT =

0.000024

0.O00017

0.000009

0.00001_

0.000090

0.000067

0.00010_

0.000106

0.00000_

0.000008

0.000004

0.000006

0.000037

0.000030

0.000058

0,000067

0.000008

0.000191

0.000082

0.000326

0.000021

0.000_06

0.000238

0.000516

0,000003

0,000191

0.OO0014

0.000174

0,000010

O,O00Qll

0.000065

0.000_5

0.000703

0.005795

0.001323

0.002679

0.001513

0.003326

0.001868

O.O01Qbq

NASA/TP-3287/R.EV 1

215
TABLE X. - Continued.

Si(cr) Silicon Cubic. TPIS 1991, vl, p237, v2, p220.

MAX REL ERR CP/R = 0.000012 TEHP = 300. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000003 TEMP : 400. AVER REL ERR HH/RT :

MAX REL ERR 5/R = 0.000002 TEMP = 400. AVER REL ERR S/R =

HAX REL ERR GH/RT = 0.000001 TEMP = 600, AVER REL ERR GH/RT :

MAX ERR CP/R = 0.000028 TEMP = 300. AVER ERR CP/R =

HAX ERR HH/RT = 0.000004 TEMP = 400. AVER ERR HH/RT =

MAX ERR S/R = 0.000006 TEMP = 500. AVER ERR S/R =

MAX ERR GH/RT = 0.000003 TEMP = 900. AVER ERR GH/RT =

Sn(cr) Tin CrI,tetragonal. TPIS 1991, pt], p350, pt2, p300.

MAX REL ERR CP/R = 0.000098 TEHP = 500. AVER REL ERR CP/R =

HAX REL ERR HH/RT = 0.000582 TEMP = 200, AVER REL ERR HH/RT

MAX REL ERR S/R = 0.000323 TEHP = 200. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.001093 TEHP = ZOO. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000364 TEHP = 500. AVER ERR CP/R =

MAX ERR HH/RT = 0.001309 TEMP = 200. AVER ERR HH/RT =

MAX ERR S/R = 0.001578 TEMP = 200. AVER ERR S/R =

MAX ERR GH/RT = 0.002887 TEblP = 200. AVER ERR GH/RT =

Sr(a)

MAX REL ERR CP/R =

MAX REI ERR HH/RT =

MAX REL ERR SIR =

MAX REL ERR GH/RT =

MAX ERR CP/R =

MAX ERR MH/RT =

MAX ERR S/R =

MAX ERR GH/RT =

Strontium Alpha Crystal. Alcock, JPCRD 1992.

0.000052 TEMP = 260. AVER REL ERR CP/R =

0.000020 TEMP = 120. AVER REL ERR HH/RT =

0.000005 TEMP = 280. AVER REL ERR S/R =

0.000022 TEMP = 100. AVER REL ERR GH/RT =

0.000166 TEHP = 260. AVER ERR CP/R =

0.000039 TEHP = 120. AVER ERR HH/RT =

0.000034 TEMP = 280. AVER ERR S/R =

0.000032 TEMP = 100. AVER ERR GH/RT =

5r{a) SCrontium Alpha Crystal. hlcock, JPCRD 1992.

MAX REL ERR CP/R = 0.000476 TEMP = 300.

MAX REL ERR HH/RT = 0.000019 TEHP = 350.

HAX REL ERR 5/R = 0.000004 TEMP = 550.

MAX REL ERR GH/RT = 0.000002 TEMP = 600.

HAX ERR CP/R = 0.001536 TEHP = 300.

MAX ERR HH/RT = 0.000028 TEHP = 350.

MAX ERR S/R = 0.000034 TEMP = 450.

MAX ERR OH/RT = 0.000012 TEMP = 800.

Ta(cr) Tantalum Crystal. JANAF Dec. 1972.

MAX REL ERR CP/R = 0.000591 TEMP = 250.

MAX REL ERR HH/RT = 0.000264 TEMP = 200

MAX REL ERR 5/R = 0.000137 TEMP = 200

HAX REL ERR GH/RT = 0.000019 TEMP = 250

MAX ERR CP/R = 0.001802 TEHP = 900

MAX ERR HH/RT = 0.000515 TEHP = 200

MAX ERR S/R = 0.000520 TEMP = 200

MAX ERR GH/RT = 0.000095 TEMP = 900.

Ta(cr) Tantalum Crystal. JANAF Dec. 1972.

MAX REL ERR CP/R = 0.000572 TEMP = 1800.

MAX REL ERR HH/RT = 0.000038 TENP = 1200.

MAX REL ERR S/R = 0.000008 TEHP = 1900.

MAX REL ERR GH/RT : 0.000024 TEMP = 1200.

MAX ERR CP/R = 0.001346 TEMP = 1800.

MAX ERR HH/RT 0.000116 TEMP = 1200.

MAX ERR 5/R = 0.000086 TEMP = 1900.

MAX ERR GH/RT = 0,000157 TEMP = 1200.

Ta{cr) Tantalum Crystal. JANAF Dec. 1972.

MAX REL ERR CP/R = 0.000058 TEMP = -2000.

MAX REL ERR HH/RT = 0.000020 TEMP = 2000

MAX REL ERR S/R = 0.000000 TEMP = 2100

MAX REL ERR GH/RT = 0.000012 TEMP = 2100

MAX ERR CP/R = 0.000219 TEMP = 2000

HAX ERR HR/RT = 0.000065 TEMP = 2000

MAX ERR S/R = 0.000110 TEMP = 2400

MAX ERR GH/RT = 0.000105 TEMP = 3200

AVER REL ERR CP/R =

AVER REL ERR HH/RT =

AVER REL ERR 5/R =

AVER REL ERR GH/RT =

AVER ERR CP/R =

AVER ERR HH/RT =

AVER ERR S/R =

AVER ERR GH/RT =

AVER REL ERR CP/R =

AVER REL ERR HH/RT =

AVER REL ERR S/R =

AVER REL ERR GH/RT =

AVER ERR CP/R =

AVER ERR HH/RT =

AVER ERR S/R =

AVER ERR GH/RT =

T range =

0.000002

0.000001

0.000001

0.000001

0.000005

0.000001

0.000002

0.000002

298.150 to 1690.000 K

REL LST SO ERR CP/R = 0.000003

REL LST 50 ERR HH/RT = 0.000001

REL LST SQ ERR 5/R = 0.000001

REL LST 50 ERR GH/RT = 0.000001

LST SQ ERR CP/R = 0.000008

LST SQ ERR HH/RT = 0.000002

LST SO ERR S/R = 0.000003

LST SQ ERR GH/RT = 0.000002

T range = 200.000 to 505.118 K

Q.000049 REL LST SQ ERR CP/R = 0.000061

0.000150 REL LST SO ERR HH/RT = 0.000229

0.000045 REL LST 50 ERR 5/R = 0.000114

0.000180 REL LST SQ ERR GH/RT = 0.000391

0.000172 LST SO ERR CP/R = 0.000216

0.000374 LST 50 ERR HH/RT =- 0.000535

0.000231 LST SQ ERR 5/R = 0.000559

0.000547 LST SQ ERR GH/RT : 0.001048

T range =

0.000016

0,000012

0.000003

0.000006

0.000049

0,000027

0.000015

0.000015

T range =

0.000075

0.000004

0,000002

0.000001

0.000247

0.000012

0.000016

0.000007

100.000 to 298.150 K

REL LST SO ERR CP/R : 0.000021

REL LST SO ERR HM/RT = 0.000013

REL LST SO ERR $/R = 0.000003

REL LST Sq ERR GH/RT = 0.000009

LST SO ERR CP/R = 0.000066

LST 5Q ERR HH/RT = 0.000029

LST SO ERR S/R = 0.000018

LST SO ERR GH/RT = 0.000016

Z98.150 to 820.000 K

REL LST 50 ERR CP/R = 0,000155

REL LST 5q ERR HH/RT = 0.000005

REL LST 50 ERR 5/R = 0.000005

REL LST SO ERR GH/RT = 0.000001

LST Sq ERR CP/R = 0,000501

LST 50 ERR HH/RT = 0.0000]6

LST SO ERR S/R = 0.000020

LST 5Q ERR OM/RT = 0.000009

T range = 200.000 ±o I000.000 K

0.000276 REI LST SO ERR CP/R = 0.000545

0.000057 REL LST 50 ERR HH/RT = 0.000086

0.000025 REL LST 50 ERR S/R = 0.000042

Q.QO0007 REL LST SO ERR GH/RT = 0.000009

0.000878 LST 50 ERR CP/R = 0.001094

0.000137 LST SQ ERR HH/RT 0.000188

0.000156 LST SO ERR 5/R = 0.000197

0.000050 LST SO ERR GH/RT = 0.000057

T ranga = 1000.000 to 2000.000 K

AVER REL ERR CP/R = 0.0001_0 REL IST 50 ERR CP/R = 0.000171

AVER REL ERR HH/RT = 0.000018 REL LST SO ERR HH/RT = 0.000021

AVER REL ERR S/R = 0.000004 REL LST SO ERR S/R = 0.000004

AVER REL ERR GH/RT = 0.000008 REL LST SO ERR GH/RT = 0.000011

AVER ERR CP/R = 0.000499 LST SO ERR CP/R = 0.000614

AVER ERR HH/RT = 0.000057 LST SQ ERR HH/RT = 0.000066

AVER ERR S/R : 0.000059 LST 5Q ERR S/R = 0.0000_S

AVER ERR GH/RT : 0.000056 LST SQ ERR GH/RT = 0.000071

T range = 2000.000 to 3258.000 K

0.000010 REL LST SO ERR CP/R = 0.000018

0.000004 REL LST SO ERR HH/RT = 0.000007

0.000006 REL LST 50 ERR 5/R = 0.000007

0.000007 REL LST 50 ERR GH/RT = 0.000008

0.000040 1ST SO ERR CP/R = 0.000068

0.000015 LST 5q ERR MH/RT = 0.000022

0.000074 LST SQ ERR S/R = 0.000080

0.000062 LST SQ ERR GH/RT = 0.000070

AVER REL ERR CP/R =

AVER REL ERR HH/RT =

AVER REL ERR S/R =

AVER REL ERR GH/RT =

AVER ERR CP/R =

AVER ERR HH/RT =

AVER ERR S/R :

AVER ERR GH/RT =

Th(a) Thorium Alpha Crystal. CODATA 1959, p239.

MAX REL ERR CP/R = 0.000137 TEMP = 500. AVER REL ERR CP/R =

MAX REL ERR HH/RT = O.O00lll TEMP = 200. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000187 TEMP = 200. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000440 TEMP = 200. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000_62 TEMP = 500. AVER ERR CP/R =

MAX ERR Hfl/RT = 0.000255 TEMP = 200. AVER ERR HH/RT =

MAX ERR S/R = 0.000933 TEMP = 200. AVER ERR S/R =

MAX ERR GH/RT = 0.001188 TEMP = 200. AVER ERR GH/RT =

T range =

0.000049

0.000025

0.000017

0.000058

0.000181

0.000062

0.000104

0.000157

200.000 to 1650.000 K

REL LST SO ERR CP/R = 0.000061

REL LST 50 ERR HH/RT = 0.000037

REL LST SO ERR S/R = 0.000046

REL LST SO ERR GH/RT = 0.000109

LST SO ERR CP/R = 0.000219

LST SQ ERR HH/RT = 0.000095

LST SO ERR 5/R : 0.000237

LST SQ ERR GH/RT = 0.000303

216 NASA/TP-3287/REV 1
TABLE X.- Continued.

Th(b) Tharium Beta Crystal. CODATA ]989. p239.

HAX REL ERR CP/R = 0.000005 TEMP = 1700.

MAX REL ERR HH/RT = 0.000008 TEMP = 2023.

HAX REL ERR 5/R = 0,000007 TEHP = 2000.

MAX REL ERR GH/RT = 0.000009 TEMP = 1650.

MAX ERR CP/R = 0.000022 TEHP = 1700.

MAX ERR HH/RT = 0.000053 TEHP = 2023.

- MAX ERR S/R = 0.000102 TEMP = 2000.

HAX ERR GN/RT = 0.000077 TEMP = 1650.

TJfa_ Titanium Alpha Crystal. CODATA

MAX REL ERR CP/R = 0.000527 TEHP = 500.

HAX REL ERR HH/RT = 0.000832 TEMP = 200.

MAX REL ERR S/R = 0.000615 TENP = 200.

HAX REL ERR GH/RT = 0,000310 TEMP = ZOO.

HAX ERR CP/R = 0.001754 TEHP = 500.

HAX ERR HH/RT = 0.001240 TEMP = 200.

MAX ERR S/R = 0.001568 TEHP = 200,

MAX ERR GH/RT = 0.000320 TEMP = ZOO.

T range = 1650.000 to 2023.000 K

AVER REL ERR CP/R = O.O0000Z REL LST SQ ERR CP/R =

AVER REL ERR HH/RT = 0,000005 REL LST SQ ERR HH/RT =

AVER REL ERR S/R = 0.000005 REL LST SQ ERR S/R =

AVER REL ERR GH/RT = 0.000006 REL LST SQ ERR GH/RT =

AVER ERR CP/R = 0.000010 LST SQ ERR CP/R =

AVER ERR HH/RT = 0.000019 LST 5Q ERR HH/RT =

AVER ERR S/R = 0.000061 LST SO ERR S/R =

AVER ERR GH/RT = 0.000055 LST 50 ERR GH/RT =

1989. p250. T range = 200.000 to 900.000 K

AVER REL ERR CP/R = 0,000]60 REL LST 50 ERR CP/R =

AVER REL ERR HH/RT = 0.000155 REL LST Sq ERR HH/RT =

AVER REL ERR S/R = 0.000118 REL LST 5Q ERR S/R :

AVER REL ERR GH/RT = 0.000088 REL LST SQ ERR GH/RT =

AVER ERR CP/R = 0.000524 LST SO ERR CP/R =

AVER ERR HH/RT = 0,000286 LST 50 ERR HH/RT =

AVER ERR S/R = 0.000457 LST Sq ERR S/R =

AVER ERR GH/RT = 0.000203 LST sq ERR GH/RT =

Ti(a) Titanium Alpha Crystal. CODATA 1989. p230,

MAX REL ERR CP/R = 0.000033 TEMP = 900. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0,000017 TEMP = 1100. AVER REL ERR HH/RT =

MAX REL ERR SIR = 0.000043 TEHP = 900. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000068 TENP = 1100. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000123 TENP = 900. AVER ERR CP/R =

MAX ERR ffH/RT = 0.000052 TEI4P = 1100. AVER ERR HH/RT =

MAX ERR SIR = g.000320 TEHP = 900. AVER ERR S/R =

MAX ERR GH/RT = 0.000343 TEHP = 1100. AVER ERR GH/RT =

Ti(b) Titanium Beta Crystal. CODATA 1989, p230.

MAX REL ERR CP/R = 0.000030 TEMP = 1200. AVER REL ERR CP/R =

HAX REL ERR HH/RT = 0.000021 TEMP = 1500. AVER REL ERR HH/RT =

MAX REL ERR $/R = 0.000027 TEMP = 1156. AVER REL ERR S/R =

MAX REL ERR GH/RT = 0.000047 TEMP = 1300. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000102 TEMP = 1200. AVER ERR CP/R =

MAX ERR HH/RT = 0.000077 TEMP = 1500. AVER ERR HH/RT =

MAX ERR $/R = 0.000236 TEHP = 1300. AVER ERR S/R =

HAX ERR OH/RT = 0.000287 TEHP = 1500. AVER ERR GH/RT =

U(a) Uranium Alpha Crystal. CODATA,

MAX REL ERR CP/R = 0.000489 TEMP = 500.

HAX REL ERR HH/RT = 0.000250 TEHP = 400.

MAX REL ERR S/R = 0.001055 TEMP = 200.

MAX REL ERR GH/RT = 0.001987 TEMP = 200.

MAX ERR CP/R = 0.001881 TEHP = 50_.

MAX ERR HH/RT 0.000699 TENP = 400.

HAX ERR S/R = 0,005011 TEHP = 200,

HAX ERR GH/RT = 0.004973 TEMP = 200,

1909, p254.

AVER REL ERR CP/R =

AVER REL ERR HH/RT =

AVER REL ERR S/R =

AVER REL ERR GH/RT =

AVER ERR CP/R =

AVER ERR HH/RT =

AVER ERR S/R =

AVER ERR GH/RT

U(1) Uranium Liquid. CODATA, 1989, p254.

MAX REL ERR CP/R = 0.0000_4 TEHP = 1600.

MAX REL ERR HH/RT = 0.000014 TEMP = 2300.

MAX REL ERR S/R = 0.000019 TEMP = 1408.

_AX REL ERR GH/RT = 0.00_0_2 TEMP = 1600.

MAX ERR CP/R = 0.000253 TEMP = 1600.

MAX ERR HH/RT = 0.000081 TEMP = 2300.

MAX ERR S/R = 0.000279 TEMP = 1900.

MAX ERR GH/RT = 0.000511 TEMP = 3100,

T range =

0.000014

0.000007

0.000032

0.000054

0.000056

0.000022

0.000251

0.000260

V(cr) Vanadium Crystal. JANAF Jun.1973.

MAX REL ERR CP/R = 0.00069_ TEHP = 600.

MAX REL ERR HH/RT = 0.000647 TEMP = 200.

MAX REL ERR $/R = 0.000275 TEMP • 200.

MAX REL ERR GH/RT : 0.000088 TEMP = 250.

MAX ERR CP/R = 0.002186 TEMP = 400.

MAX ERR HH/RT = 0.000667 TEMP = 250.

MAX ERR 5/R = 0.000646 TEMP = 200.

MAX ERR GH/RT = 0.000215 TEMP = 600.

V(cr) Vanadium Crystal. JANAF Jun.1975,

MAX REL ERR CP/R = 0.000623 TEMP = 1200.

MAX REL ERR HH/RT = 0.0000_7 TEMP = 1000.

MAX REL ERR S/R = 0.00005_ TEMP = 600.

MAX REL ERR GH/RT = 0.000068 TEMP = 600.

MAX ERR CP/R = _.OOZ38q TE'/4P = 1200.

mAX ERR HH/RT = 0.000137 TEMP = 1000.

MAX ERR S/R = 0.000509 TEMP = 600.

mAX ERR GH/RT 0.000237 TEMP = 900.

T range =

0.00O012

0.000011

0.000020

0.000039

0.000048

0.000040

0.000201

0.000238

900.000 to 1156.000 K

REL LST _q ERR CP/R =

REL LST Sq ERR HH/RT =

REL LST Sq ERR S/R =

REL LST $Q ERR GH/RT

LST SQ ERR CP/R =

LST SO ERR HH/RT =

LST SO ERR S/R =

LST SQ ERR GH/RT

1156.000 to 1944.000 K

REL LSI 50 ERR CP/R =

REL LST SQ ERR HH/RT

REL LST SQ ERR S/R =

REL LST $Q ERR GH/RT =

LST SQ ERR CP/R =

LST 54 ERR HHIRT =

LST SO ERR S/R :

LST SQ ERR GH/RT =

T range = 200.000 to 942.000 K

0.000183 REL LST 50 ERR CP/R =

0.000052 REL LST SQ ERR HH/RT :

0.000141 REL LST SQ ERR $/R =

0.000227 RE_ LST SO ERR GH/RT =

0.000744 LST SO ERR CP/R =

0.000153 LST SQ ERR HH/RT =

0.000805 LST SO ERR S/R =

0.000664 LST SO ERR GH/RT =

T range =

AVER REL ERR CP/R = 0.000015

AVER REL ERR HH/RT = 0.000009

AVER REL ERR S/R = 0.000011

AVER REL ERR GH/RT O.OOOOZO

AVER ERR CP/R = 0.000080

AVER ERR HH/RT = 0.000050

AVER ERR S/R = 0.000193

AVER ERR GH/RT = 0.000241

T PInge

AVER REL ERR CP/R = 0.000195

AVER REL ERR HH/RT = 0.0001_0

AVER REL ERR S/R = 0.000086

AVER REL ERR GH/RT = 0.000045

AVER ERR CP/R = 0.000606

AVER ERR HH/RT = 0.000253

AVER ERR $/R = 0.000315

AVER ERR GH/RT = 0.000097

T range =

AVER REL ERR CP/R = 0.000_12

AVER REL ERR HH/RT = 0.00002_

AVER REL ERR S/R = 0.000022

AVER REL ERR GH/RT = 0.000044

AVER ERR CP/R = 0.001145

AVER ERR HH/RT = 0.000064

AVER ERR S/R = 0.000155

AVER ERR GH/RT = 0.000185

0.000003

0,000005

0.000005

0.000006

0.000014

0.000022

0.000069

0.00005_

0.000219

0.000293

0.000216

0.000120

0.000722

0.000_65

0.000636

0.000224

0.000019

0.000009

0.000033

0.000055

0.000073

0,00_029

0.000258

0.00O269

0.000015

0.000013

0.000021

0.000039

0.000058

0.000047

0.000202

0.000239

0.0002_5

0,000091

0.000337

0.000629

0.000922

0.000259

0.001632

0.001586

1408.000 to 4000,000 K

REL LST 5Q ERR CP/R = 0.000019

REL LST 50 ERR HH/RT = 0.000009

REL LST SQ ERR S/R = 0.000012

REL L$T Sq ERR GH/RT = 0.000021

LST SQ ERR CP/R = 0.000113

LST SO ERR HH/RT = 0.000053

LST sq ERR S/R = 0.000199

LST SQ ERR GH/RT = 0.0002_3

200.000 to 600.000 K

REL LST SQ ERR CP/R = 0.000289

REL LST SO ERR HH/RT = 0.000205

REL LST $Q ERR S/R = 0.000117

REL LST Sq ERR GH/RT = 0.000051"

LST SQ ERR CP/R = 0.000905

LST SQ ERR HH/RT = 0.000335

LST SO ERR S/R = 0.000368

LST SQ ERR GH/RT = 0,000118

600.000 to 1400.000 R

REL 1ST SQ ERR CP/R = 0.000375

REL LST 5Q ERR HH/RT = 0.000027

REL LST SQ ERR S/R = 0.000027

REL LST 50 ERR GH/RT = 0.000D4_

LST 54 ERR CP/R = 0.001379

LST S_ ERR HH/RT = 0.000078

LST S_ ERR S/R : 0.000181

LST S_ ERR GM/RT = 0.000190

NASA/rP-3287/REV l

217
TABLE X.- Continued.

V(cr) Vanadium CrystaL. JANAF Jun.1973. T range _ 1400.000 to 2190.000 K

PIAX REL ERR" CP/R = 0.000885 TEHP = 1900. AVER REL ERR CP/R = 0.000463 REL LST SQ ERR CP/R = 0.000544

MAX REL ERR HH/RT 0.000068 TEHP = 1500. AVER REL ERR HH/RT = 0.000039 REL LST 50 ERR HH/RT = 0.0000_4

MAX REL ERR SIR = 0.000016 TEMP = 2000. AVER REL ERR SIR = 0.000007 REL LST SQ ERR S/R = 0.000009

HAX REL ERR GH/RT = 0.000031 TEMP = 1600. AVER REL ERR GH/RT = 0.000020 REL LST SQ ERR GH/RT = 0.000021

HAX ERR CP/R = 0.004211 TEHP = 1900. AVER ERR CP/R = 0.002169 LST SQ ERR CP/R = 0.002565

MAX ERR HH/RT = 0.000220 TEHP = 1500. AVER ERR HH/RT = 0.000150 LST Sq ERR HH/RT = 0.0001_8

MAX ERR S/R = 0.000160 TEf4P = 2000. AVER ERR S/R = 0.000068 LST Sq ERR S/R = 0.000087

MAX ERR QH/RT = 0.000184 TEMP = 1600. AVER ERR GH/RT 0.000123 LST Sq ERR GH/RT = 0.000129

N(cr) Tungtan Crystal. JANAF Jun.1966. T range = 200.000 to 1000.000 K

MAX REL ERR CP/R = 0.001029 TEMP = 350. AVER REL ERR CP/R = 0.000258 REL LST SQ ERR CP/R = 0.000566

MAX REL ERR HH/RT = 0.000865 TENP = 200. AVER REL ERR HH/RT = 0.000155 REL LST SQ ERR HH/RT = 0.000261

HAX REL ERR S/R = 0.000355 TEMP = 200. AVER REL ERR S/R = 0.000087 REL LST SQ ERR S/R = 0.000119

MAX REL ERR GH/RT = 0.000326 TEMP = 200. AVER REL ERR GH/RT = 0.000078 REL LST SQ ERR GH/RT = 0.000111

MAX ERR CP/R = 0.005051 TEMP = 350. AVER ERR CP/R = 0.000775 LST SQ ERR CP/R = 0.00]086

MAX ERR HH/RT = 0.001584 TEHP = 200. AVER ERR HH/RT = 0.000305 LST Sq ERR HH/RT = 0.000_55

HAX ERR SIR = 0.000993 TEHP = 290. AVER ERR SIR = 0.000_07 LST SQ ERR $/R = 0.000475

HAX ERR GH/RT = 0.000390 TEHP = 200. AVER ERR GH/RT = 0.000196 LST SQ ERR GH/RT = 0.00022_

14(cr) Tungsten Crystal. JANAF Jun.1966. T range = 1000.000 to 2600.000 K

MAX REL ERR CP/R = 0.000127 TEMP = 1100. AVER REL ERR CP/R = 0.000049 REL LST 59 ERR CP/R = 0.000061

MAX REL ERR HH/RT = 0.000056 TEHP = 1800. AVER REL ERR HH/RT = 0.00001q REL LST SQ ERR HH/RT = 0.000022

MAX REL ERR SIR = 0.000037 TEHP = 2100. AVER REL ERR $/R = 0.000027 REL LST 50 ERR SIR = 0.000028

MAX REL ERR GH/RT = 0.000061 TEMP = 1400. AVER REL ERR GH/RT = 0.000047 REL LST SO ERR GH/RT = 0.000048

MAX ERR CP/R = 0.000428 TENP = 1100. AVER ERR CP/R = 0.00018! LST SO ERR CP/R = 0.000218

MAX ERR HH/RT = 0.000111 TEMP = 1800. AVER ERR HH/RT = 0.000060 LST SO ERR HH/RT = 0.000069

HAX ERR $/R = 0.000405 TEHP = 2600. AVER ERR S/R = 0.000255 LST SO ERR S/R = 0.000260

MAX ERR GH/RT = 0.000355 TEMP = 1400. AVER ERR GH/RT = 0.000505 LST SO ERR GH/RT = 0.000305

N(cr) Tungsten Crystal. JANAF Jun.1966. T range = 2600.000 to 5200,000 K

MAX REL ERR CP/R = 0.001425 TEMP = 5000. AVER REL ERR CP/R = 0.000559 REL LST SO ERR CP/R = 0.000765

HAX REL ERR HH/RT = 0.000057 TEHP = 2800. AVER REL ERR HH/RT = 0.000051 REL LST SO ERR HH/RT = 0.00005_

MAX REL ERR 5/R = 0.000058 TEMP = 3100. AVER REL ERR 5/R = 0.000055 REL LST SO ERR S/R = 0.000056

HAX REL ERR GH/RT = 0.000041 TEHP = 3100. AVER REL ERR GH/RT = 0.000037 REL LST $0 ERR GH/RT = 0.000057

MAX ERR CP/R = 0.007025 TEMP = 5000. AVER ERR CP/R = 0.0027q2 LST 50 ERR CP/R = 0.0037_9

MAX ERR HH/RT = 0.000196 _EHP = 2800. AVER ERR HH/RT = 0.000109 LST Sq ERR HH/RT = 0.600118

HAX ERR 5/R = 0.000461 TEHP = 3100. AVER ERR $/R = 0.000_14 LST SO ERR S/R = 0.000415

HAX EIR GH/RT = 0.000346 TEMP = 5100. AVER ERR GH/RT = 0.000_05 LST SO ERR GH/RT 0.000307

N(cr) Tungsten Crystal. JANAF Jun.1966. T range = 5200.000 to 3680.000 K

MAX REL ERR CP/R = 0.002147 TEHP = 5600. AVER REL ERR CP/R = 0.001258 REL LST 5Q ERR CP/R = 0.001402

HAX REL ERR HH/RT = 0.000050 TEMP = 3500. AVER REL ERR HH/RT = 0.000033 REL LST SO ERR HH/RT = 0.000056

MAX REL ERR S/R = 0.000039 TEMP = 3500, AVER REL ERR S/R = 0.000022 REL LST SO ERR $/R = 0.000025

MAX REL ERR OH/RT = 0.000040 TEHP = 5200. AVER REL ERR GH/RT = 0.000055 REL LST SO ERR GH/RT = 0.000036

NAX ERR CP/R = 0.013938 TEHP = 3600. AVER ERR CP/R = 0.008399 LST SO ERR CP/R = 0.009596

HAX ERR HH/RT = 0.000200 TEHP = 3680. AVER ERR HH/RT = 0.000126 LST 59 ERR HH/RT = 0.0001_1

MAX ERR S/R = 0.000498 TEHP = 5500. AVER ERR SIR = 0.000275 LST SO ERR SIR = 0.000509

HAX ERR GH/RT = 0.0003_2 TEMP = 5200. AVER ERR GH/RT = 0.000511 LST SO ERR GH/RT = 0.000312

Xe Xenon. NSRDS-NBS _5, 1971. Temperature cutoff. T range = 1000.000 to 6000.000 K

MAX REL ERR CP/R = 0.000012 TEMP = 6000. AVER REL ERR CP/R = 0.000005 REL LST SO ERR CP/R = 0.000004

MAX REL ERR HH/RT 0.000001 TEHP = 1500, AVER REL ERR HH/RT = 0.000000 REL LST S_ ERR HH/RT = 0.000000

MAX REL ERR $/R = 0.000000 TEMP = 1300. AVER REL ERR 5/R = 0.000000 REL LST $0 ERR S/R = 0.000000

MAX REL ERR GH/RT = 0.000000 TE_tP = 1700. AVER REL ERR GH/RT = 0.000000 REL LST SO ERR GH/RT = 0.000000

MAX ERR CP/R = 0.000030 TEHP = 6000. AVER ERR CP/R = 0.000007 LST SO ERR CP/R = 0.000009

MAX ERR HH/RT 0.000002 TEMP = 1500. AVER ERR HH/RT = 0.000001 LST SO ERR HH/RT = 0.00000!

MAX ERR S/R = 0.000002 TEMP = 1500. AVER ERR S/R = 0.000001 LST 50 ERR S/R = 0.000001

MAX ERR GH/RT = 0.000001 TEHP = 1700. AVER ERR GH/RT = 0.000000 LST SO ERR _H/RT = 0.000000

Xe Xenon. NSRDS-NBS 35, 1971. FIXEDN = 5 with FILL. T range = 6000.000 to 20000.000 K

MAX REL ERR CP/R = 0.014245 TEMP = 10500. AVER REL ERR CP/R = 0.006884 REL LST 30 ERR CP/R = 0.007885

MAX REL ERR HH/RT = 0.001917 TEHP = IZ000. AVER REL ERR HH/RT = 0.00069_ REL LST 5_ ERR HH/RT = 0.000855

MAX REL ERR S/R = 0.000201 TEMP = 12000. AVER REL ERR S/R = 0.000070 REL LST $q ERR S/R = 0.000090

MAX REL ERR GH/RT = 0.000052 TEHP = 13500. AVER REL ERR GH/RT 0.000028 REL LST SO ERR GH/RT = 0.000052

MAX ERR CP/R = 0.092926 TEMP = 20000. AVER ERR CP/R = 0.050230 LST SQ ERR CP/R = 0.057331

MAX ERR HH/RT = 0.00_945 TEMP = 12000. AVER ERR HH/RT = 0.001946 LST SO ERR HH/RT = 0.002346

MAX ERR S/R = 0.005973 TEHP = 12000. AVER ERR SIR = 0.002099 LST SQ ERR S/R = 0.002700

MAX ERR GH/RT = 0.001_56 TEMP = 13500. AVER ERR GH/RT = 0.000771 LST SO ERR GH/RT = 0.000887

Zn(cr) Zinc CrysteJ. CODATA 1989, 0221.

HAX REL ERR CP/R = 0.000061 TEHP = _00.

MAX REL ERR HH/RT = 0.001027 TEHP = 200.

MAX REL ERR S/R = 0,000636 TEMP = 200.

HAX REL ERR GH/RT = 0.002352 TEMP = 200.

MAX ERR CP/R = 0.000193 TEMP = _00.

MAX ERR HH/RT = 0.001994 TEHP = 200.

MAX ERR S/R = 0.002_35 TEMP = 200.

MAX ERR GH/RT = 0.00_429 TEMP = 200.

T range = 200.000 to 692.730 K

AVER REL ERR CP/R = 0.000017 REL LST SQ ERR CP/R = 0.000026

AVER REL ERR HH/RT = 0.000166 REL LST SQ ERR HH/RT = 0.000389

AVER REL ERR 5/R = 0.000102 REL LST SO ERR S/R = 0.000241

AVER REL ERR OH/RT = 0.000544 REL LST SO ERR GH/RT = 0.000089

AVER ERR CP/R = 0.000054 LST Sq ERR CP/R = 0.000081

AVER ERR HH/RT = 0.000555 LST SQ ERR H_/RT = 0.000757

AVER ERR S/R = 0.000419 LST SO ERR S/R = 0.000927

AVER ERR GH/RT = 0.000664 LST $Q ERR GH/RT = 0.001675

218 NASA/TP-3287/REV 1
TABLE X.- Concluded.

Zr(a) Zirconium Alpha Crystal, JANAF Jun.1979.

MAX REL ERR CP/R = 0.000682 TEHP = 600. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000|3_ TEMP = 200. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0.000060 TEHP = 200. AVER REL ERR S/R =

HAX REL ERR GH/RT = 0.000056 TEHP = 300. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.002237 TEHP = 600. AVER ERR CP/R =

MAX ERR HH/RT = 0.0002_9 TEHP = 200, AVER ERR HH/RT =

MAX ERR S/R = 0,00022A TEMP = ZOO. AVER ERR S/R =

MAX ERR GH/RT = 0.000138 TEHP = 300. AVER ERR GH/RT =

Zr(b) Zirconium Beta Cry_tal. JANAF Jun.1979,

MAX REL ERR CP/R = 0,000010 TEMP = 1_00. AVER REL ERR CP/R =

MAX REL ERR HH/RT = 0.000011 TEHP = 1_00. AVER REL ERR HH/RT =

MAX REL ERR S/R = 0,000005 TEMP = 1500. AVER REL ERR S/R =

MAX REL ERR OH/RT = 0.0000]0 TEHP = 1700. AVER REL ERR GH/RT =

MAX ERR CP/R = 0.000035 TEHP = 1_00. AVER ERR CP/R =

MAX ERR HH/RT = 0.000037 TEMP = 1_00. AVER ERR HH/RT =

MAX ERR S/R = 0,000058 TEPTP = 2000. AVER ERR S/R =

MAX ERR GH/RT = 0.000076 TEMP = 1700. AVER ERR GH/RT =

T range = 200.000 to 1135.000 K

0.000149 REL LST SO ERR CP/R = 0.000231

0.000036 R'EL LST SQ ERR HH/RT = 0.000051

0.000015 REL LST 50 ERR S/R = 0.000022

0.000017 REL LST sq ERR GH/RT = 0.000023

0.000_83 LST SQ ERR CP/R = 0.000749

0.00008_ LST SQ ERR HH/RT = 0.000117

0.000085 L$T SO ERR 3/R = 0.000109

0,000055 LST SO ERR GH/RT = 0.000069

T range = 1135,000 to 2125.000 K

0.000003 REL LST SQ ERR CP/R = 0.00000_

0.00000_ REL LST SQ ERR HH/RT = 0.000005

0.000003 REL LST SQ ERR S/R = 0.00000_

0.000005 REL LST Sq ERR GH/RT = 0.000006

0.000013 LST SO ERR CP/R = 0,0000]6

0.000015 LST SO ERR HH/RT = 0.000018

0.000036 LST SQ ERR S/R = 0.0000_1

0.000039 LST Sq ERR GH/RT = 0.0000_

NASA/TP-3287/REV 1 219
i 31

24

20

Original Data for Ag (cr,e)

.... 1 " " "'" 1 .... I .... I " • " " I ....

..,I .... I .... 1 .... I,,,.! .....

1000 2_ 3_ 4OOO 50O0 6000

Temp. [K]

3S

i 3L2_

[,.) 24

2O

0

Coef Data for Ag (cr, e)

.... I .... _ " " " I " "'" " I .... I ....

._ + . I . . _ . I .... I .... I .... I ....

I000 3.000 30OO 40O0 .mOO0 _00

Temp. [K]

35

211

Original Data for A1 (cr,_')

.... I " ' " " I .... I .... I .... "I''_ • "

. + . I . . . , I .... I .... I .... 1 ....

1000 20(X} 30OO _ 500o 6O0O

Temp. [K]

-1+

O

i...i

L)

3_

28

Coef Data for A1 (cr,e)

''_ "T .... l .... I .... I _ "'"I'''

70_.... I ..... I .... I .... ! .... I . . . ,

10C0 2000 ]IX30 4000 5000

Temp. [K]

000

40

_, 3J

r',.

2O

0

Original Data for Ar

.... I .... I .... I .... l .... I ....

; , . . _ .... r'+"t"_-:, i.-_... J .... a ....

3333 6667 I0000 1_333 16667 20000

Temp. [K]

40

2O

0

Coef Data for Ar

,"-v , | "_ " + " I .... 1 .... I .... | .....

.2

'.:: ....._ : _ .... J :............

3333 6667 I_ 131133 11_67 20000

Temp. [K]

Rgure1.--Comparisonof selected(labeledoriginal)C_ valuesgivenin table]1]withvaluescalculatedfromthe

9-constantcoefficientsgivenintableVL

220 NASA/TP-3287/REV 1
28

12

Original Data for B (13,e)

.... I .... I .... I .... | .... I ....

.., I .... I .... I . , _ , I .... ! ....

1000 2OO0 3OOO 400O 5000 6000

Temp. [K]

282O

Coef Data for B (13,e)

35 .... I .... I .... , .... 'i .... i ....

_. . . I .... i .... I .... I .... t ....

50 10_0 2OO0 3O00 4OOO 5000

Temp. [K]

Original Data for Ba (a,e) Coef Data for Ba (a,e)

40

4O

29 25 ..... " ' '_00' " 4000 5000

25 0 1000 2000 _00 _ 5000 6600 0 t00o 2000

Temp. [K] Temp. [K]

40

25

10

Original Data for Be (a,I],£) Coef Data for Be (o_,13,g)

40

" ' " I .... I .... l .... I .... t ....

..... i l _ ., . I I0 II_0 2000 11000 4000 6000

I000 2OOO 3000 4O00 5O00

Temp. [K] Temp. [K]

Figure 1 .--ConUnued.

221

NASA/TP-3287/REV 1
8O

7"2

4(-

la,

U ss

SO

0

Original Data for Br 2 (cr,£)

.... I .... I .... I .... I .... "i ....

• , . I .... I .... I .... I .... I ....

833 1667 2500 3333 4167 5000

Temp. [K]

Coef Data for Br 2 (cr, e)

80 ....

72

_.) st

5O

0

I .... '1 .... t .... I .... I .... '

.... ! .... ! ..... I ..... 1..... ! . . , ,

833 1667 2500 3333 4167 51100

Temp. [K]

]0

24

5 o

Original Data for C (gr) Coef Data for C (gr)

.... I .... _ .... I .... I .... I .... 30| .... I .... I .... I "'" " " J """ " " I " " ''_ "

o

- LI

,h ,_. _ _;. 4,',,5= , J

, • . I .... I .... I ..... I .... I ....

833 1667 2500 33_3 416"/

Temp. [K] Temp. [K]

_ 35

o iginal Data for Ca (a,13,e)

.... I " " " s I .... I .... I .... I ....

/j -

10G0 20O0 _m00 a,C00 _00

Temp. [K]

40

i 35

30

Coef Data for Ca (a,13,e)

/j --

Temp. [K]

Figure1.--Continued.

222 NASA/TP-3287/REV 1
30

i +25

_.) 22

20

0

Original Data for Cd (cr,e)

j _ _ i ==========================

. , . . I .... | .... _ .... i .... L ....

I OO3 2000 3000 400<] 5000

Temp. [K]

Coef Data for Cd (cr, e)

3o[_./=++..... ,...... ,, ....... , . _

i_ 2S

25

22

20 .... 1 .... I .... I .... I .... I ....

0 10(30 _ 3O(]0 40OO 5_00

Temp. [K]

i"

p-,

3O

0

Original Data for C12

• . + I .... I .... 1 .... I .... I ....

Temp. [K]

45

_ 41

Coef Data for C12

.... , .... +t.... _ .... J .... + ....

tmo _ :moo 4ooo moo +am

Temp. [KI

55

29

Original Data for Co (a,13,e)

t00o 2000 3OO0 400O _ _00

Temp. [K]

4638

20

0

Coef Data for Co (e,13,e)

1.0_ 2000 _ 4<]00 _00 6000

Temp. [K]

F_Jre 1.--Continued.

NASA/TP-3287/REV 1 223
6O

4936

_ 26

tS

0

65

SS

35

25

0

Original Data for Cr (cr,e)

.... I .... 1 .... I .... 1 .... I ....

.., | .... _ .... t .... I .... I ....

10l_ 2OOO 3O0O 4000 5OO0 ¢_00

Temp. [K]

6O

49

25

|5

Original Data for Cs (cr, Q

.... ! .... i .... I .... I .... I .... 65

!+4S

1'_ 35

_,33 66? ItO00 1333 1567 2000

Temp. [K]

Coef Data for Cr (cr, Q

.... I .... I " "'" ' ! ' ' "

.... | .... 1 .... | . . .

Temp. [K]

• I .... ! ....

. i .... I • . , ,

Coef Data for Cs (cr,Q

.... I .... I .... I .... I .... I ....

333 66; I000 13133 I_? 2900

Temp. [K]

35

24

20

0

Original Data for Cu (cr,e)

.... I .... I .... I .... I " " " " I "' " • "

, . . l .... I .... I .... I , , , . l ....

lOOO 2OOO 3OO0 410OO _m)O0 6000

Temp. [K]

35

31

28

24

20

0

Coef Data for Cu (cr,e)

.... I .... I .... l . . ,.. | .... [ ....

.... i .... I .... | .... I .... I ....

tim0 2000 3O0O 4COO _C0 6000

Temp. [K]

Figure 1.--Continued.

224 NASAfTP-3287/REV I
45

40

35

25

Original Data for D 2

• ,_T_ I +_ " *] .... I '-: * I .... I " ' "-_;

.... 1 ..... L ..... J . + . . I _ . . . I ....

3333 6667 I0000 13333 16667 2000(

Temp. [K]

4O

O

35

Coef Data for D 2

45 .... 1.... + + " " " I .... I .... I . " _ ."

25

0

,t. + . t .... l .... I , . • -I .... I ....

3333 6667 I0000 13333 16667 lOGO0

Temp. [K]

_-_ 21

Original Data for Electron

;_ " " " I • _ " " I _ "" ' + '1 .w, . '7 _" + _ I ....

0

± . . I .... I . . • I . + +

Jl1_ 1,667 I0(1_ 13333 16667

Temp. [K]

24

2Oo

Coef Data for Electron

.... | .... I ..... l'" " " +'"r" • " " I .....

.... t .... i .... I .... i .... J ....

3333 6667 IGO00 13333 164567 20000

Temp. [KI

40

U 29

0

Original Data for F 2

..... _ - - + I .... 'I " "'" I .... ""

l<l_O 20<20 _ ,,4+000 .5000

Temp. [KI

4O

29

"6OO0 IS0

Coef Data for F 2

.... 1 .... I .... I .... 1 .... I _ . .

llmO 201_0 3OOO 4OOO .5OOO

Temp. [K]

Figure1.--Continued.

NASA/TP-3287/REV 1 225
Original Data for Fe (ot,_,,G,e)

O

0 1000 2000 3000 4000 .5000 6(100

Temp. [K]

Coef Data for Fe (et,'y,G,e)

R$

i $2

0 I000 20O0 _ _ 5O0O 600O

Temp. [K]

_ 28

0

Original Data for Ge (cr,O

.... I_"" " I .... "1 " " T : I .... I ....

. . . I .... I .... I .... I .... I,, . . .

_0QO 2O0O _ 400O $QO0 6OO0

Temp. [K]

3O

2_

U 22

2O

Coef Data for Ge (cr,e)

.... I .... t ..... I ' ''" " I .... I "'" "' '

.... I .... |, , , , I .... I .... I ....

10_0 _ 3000 4000 $000 G000

Temp. [K]

45

35

0

Original Data for H 2

.... I T--" " " I .... I .... I " " "'' I " " ""

, . . • I .... I .... | .... I .... ! ....

33.33 6667 l_ 13333 16_? :_OOC

Temp. [K]

403S

0

Coef Data for H 2

.... I .... I .... I .... I .... I "" " "

.... t. , b, I .... I . . _ , I , , - - I ....

3333 6667 10000 13333 16667

Temp. [K]

Figure 1 .--Continued,

226 NASA/TP-3287/REV 1
24

t_

22

k...a

r..) zl

20

0

Original Data for He

-- _ "'1 " '_ " " r- I .... | .... I'" " ' '

• , I .... t .... [ .... I .... ! ....

3333 6667 100(30 13333 16667 20000

Temp. [K]

25

-, 24

o

2O

Coef Data for He

.... _"" " • " I 7''q" " I .... I " _ ' ' _ ....

.... ! .... S .... I .... | .... I ....

3333 666? I0000 13333 16667 20000

Temp. [K]

3$

32

tZ

25

0

Original Data for Hg (cr,_')

"_ " "'1 ' " " ; I "_ " " " _ .... I " "'" " 1"L "

333 667 1000 1333 1567 2000

Temp. [K]

35

,o

0

Coef Data for Hg (cr,_')

4

333 667 10130 t333 156"/ 2000

Temp. [K]

Original Data for 12 (cr,e)

_ 5s

_0

0 1000 20O0 30O0 4OOO 5O0O 6OO0

Temp. [K]

8O

72

"6

6S

_) 5s

Coef Data for 12 (cr, f)

•1

50 .... I .... I .... I . , . • I .... I .....

0 10G0 20O0 3O00 4OOO _ 6OO0

Temp. [K]

Figure 1 .--Gontlnued.

NASA/TP-3287/REV 1 227
65

i

M

O

,-.,

t_

'25

0

Original Data for K (cr, e)

.... I .... I _. , T . t " " " I .... l " " "' _ 65

_ 35

367 733 11130 1467 1833 22(_

Temp. [K]

Coef Data for K (cr,e)

I I I |

367 733 1100 1467 1833 2200

Temp. [K]

55

46

t,,,,,,a

20

0

Original Data for Kr

.... ! .... 1 " ' " _"1 '"'" " I .... I .... 55

g29

]]!1 m,_t. ? IGOU0 13333 16667 201X_ 0

Temp. [K]

Coef Data for Kr

.... I "* * " I " *'" " I .... I " " " " I " '" " "

3333 6667 10_0 13533 16667 20000

Temp. [K]

_ 35

O

t_

f.,) 25

2O

Original Data for Li (cr,e)

500 1000 1500 2000 2_100

Temp. [K]

Coef Data for Li (cr,e)

35 -

0

t,...,,t

r,.)

20 0 . i i | i

1300 .%00 Iollo I_ 21100 250(3 3000

Temp. [K]

Figure1.--ConSnu_l.

228 NASA/TP-3287/REV 1
35,

2O

Original Data for Mg (cr, e)

IOOG 2000 _00 4000 5tX)O 60OC

Temp. [K]

Coef Data for Mg (cr, Q

..... I .... I .... [ .... I .... [ ....

1000 2OOO .1000 _00 $_00 60O0

Temp. [K]

i 42

0

Original Data for Mn (ct,[3,y,_,Q

i

.., I , , , , ! .... I .... I . . .'. ! ....

1000 _000 _00 4OOO 5OOO 6OO0

Temp. [K]

5O

2O

0

Coef Data for Mn (e_,ll,%8,Q

_rii _ r : 2 z 7::-z :-27: z-_-:_ : 7 z I-77z2 -7_A 77_7

.... I .... I .... I ..... ! .... I ....

Temp. [K]

55

i"

2O

0

Original Data for Mo (cr,e)

i .... I "'* " " I _" "' "--f"* " " " ! .... i * " _"

i ......... | I ....

IOO0 1000 300O s,0t]0 5000 6000

Temp. [K]

Coef Data for Mo (cr,e)

29 1

20 | 1

0 1000 2OOO _ 4O00 _ 6OOO

Temp. [K]

Figure 1 .--Continued.

NASA/TP-3287/REV 1 229
70

59

48

3_

25

0

Original Data for N 2

.... } .... I .... • .... I .... L .-- ,

3333 6f_O 100O0 13333 16667

Temp. [K]

7O

39

48

25

0

Coef Data for N2

.... I .... " I .... I " "="" I .... I ....

.... I .... I .... I ...__ I .... l ....

3333 _67 10(300 13333 16667 20000

Temp. [K]

SO

44

i..,.a

la.

U

25

0

Original Data for Na (cr, e)

.... ] .... I .... T .... r .... r "_-_ -

383 "/67 I I_) 1533 191 '7 23_

Temp. [K]

50

44

L) 31

25

Coef Data for Na (cr,e)

..... I .... I. , , • I .... I .... l . • .

3113 767 I I_0 1t33 1917 7.__100

Temp. [KI

45

3932

0

Original Data for Nb (cr,e)

"*'l .... _''"'_ .... ¿''""l''''" 45

.... I .... t_ , . 20

|000 2000 3000 4000 5000 (_GO 0

Temp. [K]

Coef Data for Nb (cr,()

.... I ""'" " " t .... I _'" " " I .... "1 "--" "

.... I .... I .... i .... I .... I ....

I0_0 200O 300O 4WaO JO00 6O0O

Temp. [K]

Figure 1 .--Continued.

230 NASA/TP-3287/REV 1
25

24

O

22

2t

20

0

Original Data for Ne

3333 6667 IDO00 13333 16667 20_0

Temp. [K]

Coef Data for Ne

25

.... 1 "=_ '" "'1 ..... I .... '| .... I ....

O

(.) 2t

20 ....

0

i .... i . i

3333 6667 100130 13333 16667 20000

Temp. [K]

Original Data for Ni (cr,e) Coef Data for Ni (cr,_')

_,35 _,,, ,

300 I000 2000 -3000 4000 5000 6000 0 I000 2000 3000 4000 5000 6000

Temp.[K] Temp.[K]

45

35

25

0

Original Data for 0 2

. : . _ I .... I .... I .... | .... I ....

3333 6667 1000(3 13333 16667 00130

Temp. [K]

45

tO35

25

0

Coef Data for 0 2

.... I .... I .... I .... t .... ] , .

3333 6667 113000 13333 16667

Temp. [K]

2OO0O

Figure 1 .--Continued.

NASA/TP-3287/REV 1 231
3O

"6

25

[.) 22

20

0

Original Data for P (cr,e)

.... I "'" ' ' t .... I .... 1 .... I ....

1000 2OOO 3OOO 400O 5OOO 6OOO

Temp. [K]

Coef Data for P (cr,£)

28

0

J

1(300 20OO 3OOO 4000 5OOO 600O

Temp. [K]

Original Data for Pb (cr, e)

" " " " I .... | .... ! " " """ I .... I ....

3S

f_ 1200 ISO0 24OO 3O0O

Temp. [K]

i 32

30

23 25

0 0

Coef Data for Pb (cr,e)

.... J .... I " " | I " k ....

.... t .... I .... I .... t .... I ....

t200 LIKI0 2400 3000 :3600

Temp. [KI

Original Data for Rb (cr,e)

65{ .... I "'" " " I" * " _'1 .... | ""'' I'" " ' '" 65

|

55 " i $5

45 - 45

3.5 35

25 • 25

0 _SO _ IOSO 14130 1750 21_

Temp. [K]

Coef Data for Rb (cr,e)

.... I .... I .... I " "'" " I .... I ....

1 350 700 1050 1400 1750 2100

Temp. [K]

Figure 1 .--Continued.

232 NASA/TP-3287/REV 1
Original Data for S ((_, 13,/?)

O

24

[/

15II , . , I .... I .... 1 .... t .... 1 ....

o |ooa 2o0o 3ooo 4o0o 5ooo

Temp. [K]

5O

O

"12

24

Coef Data for S (_,[3,0

15 , , . ( .... ! .... I .... I .... ) ....

0 1_ 2O00 _00 40OO 5O0O

Temp. [K]

E

Original Data for Si (cr,#)

O

_ 22 22

_,_ 19 19

15 _ ( .... ! .... I .... ! . 15

0 JO00 2000 _00 4GO0 5000 _lO00 0

Temp. [K]

Coef Data for Si (cr,e)

_-_:. • I .... t .... I , .

loco 2oo0 _oo _oo ,_ooo

Temp. [K]

Original Data for Sn (cr,£)

35 --- , - - I .... I .... I " _'" I " " " _1 .... -

>, I

0 783 1:567 2350 " 3133 3917 4700

Temp. [K]

35

3O

250

Coef Data for Sn (cr, O

.... [ .... I .... f"" "1 .... I _ " "

783 1567 2350 3133 39 I'1 4700

Temp. [K]

Figure 1 .---Continued.

NASA/TP-3287/REV 1 233
4O

36

32

29

25

Original Data for Sr (o_, 13,e)

10(30 2000 3OOO 4000 J{3o0 6000

Temp. [K]

3632

Coef Data for Sr (ot,13,g)

10G0 200O 300[I 40130 50O0 6OO0

Temp. [K]

Original Data for Ta (cr, e)

45

39

26

20

0 !_0 2000 3000 40130 5000 6060

Temp. [K]

45

i 3932

20

0

Coef Data for Ta (or,e)

.... ! .... i .... I .... I .... I ....

t_0 20O0 3000 _ SO00 6000

Temp. [K]

50

44

,-,,

_--) 31'

2J

Original Data for Th (c_,13,e)

' " ' " " I .... l_' _'" " l-" " " " I .... I ....

.... I .... I .... I ....

1OO13 20130 3OO0 4000 5OOO 61300

Temp. [K]

5O

i A,4 38

Coef Data for Th (¢x,13,e)

.... I .... i .... '1-'" " " " I .... '1 ....

.... 1 .... I .... I ....

IO00 2000 3O00 4000 50O0 6000

Temp. [K]

Figure 1 ..--Continued.

234 NASA/TP-3287/REV 1
Original Data for Ti (e_, 13,e)

50 ' _' " I " " '_I .... 1 ' ' ' _1 .... i _ " " '

42 i ::-:

35

C.) 28

20 .... I .... ) . , , . I.. , , ,

0 106O 2CX_0 3000 4O00 5OOO 6OOO

Temp. [K]

Coef Data for Ti (c_,13,e)

t

_, ,2

_ 35

U 2g

20 _, . . . I .... I , ! I I

0 1000 20_ 3000 4000 30OD 6000

Temp. [K]

34

Original Data for U (ec,[3,y,£)

_'' ' " P " ''""t .... I'" " ' " 1 .... I " " " s'

/

. ._.. ! .... ( .... ! .... I .... I ....

667 1333 2000 2667 3333 4000

Temp. [K]

6O

i 5142

0

Coef Data for U (a,I],y,e)

.... I_ "'' " I" '"'" I .... I .... ! ....

_7 m3 2o6o _7 3333 ,o0o

Temp. [K]

$0

42

20

0

Original Data for V (cr, g)

.... I .... I" "'1 .... _"1''" "" "l ....

I , , , | , . , • I .... I .... I .... _ ....

1000 5000

Temp. [K]

5O

i 42

35

2O

60O0 0

Coef Data for V (or, e)

,I

.... I .... I ..... I .... I .... _ ....

1000 2000 3000 4000 30_ 6000

Temp. [K]

Figure 1 ._Contlnued.

NASA/TP-3287/REV 1 235
TO

51

45

f,.) 3,2

2O

Original Data for W (cr,e)

................ I + , , j 1 ....

lOGO 2000 3000 4OOO 50OO

Temp. [K]

7O

4_

2O

0

Coef Data for W (cr, e)

L

.... I .... 1 .... J .... I ..... I ....

LOC_ 2000 _ 4000 SO00 6000

Temp. [K]

105

2O

0

Original Data for Xe

.... I "_ ' :'-I " " ' '" I .... I " " "" " "l .... II_

,,,J I • 20

3333 666") I0000 13333 16667

Temp. [K]

Coef Data for Xe

" "'' + I" " """ I .... _ .... l """_+ I ....

3333 6667 I0000 13333 1666T 20000

Temp. [K]

35

@

2s

_.) z+

2O

0

Original Data for Zn (cr,O

r-- ..... e ..... J ...... ,, • -.

' '" ' _ I " I I " I

. . . 1 .... I .... I .... I .... I ....

1(300 2000 _ 4000 JO00 6000

Temp. [K]

35

3|

.r-,.

(J 24

Coef Data for Zn (cr,e)

.... I .... I .... I .... "I' .... 'I "_ " "

20_ ' " " " I .... I .... I .... I .... • .... 100O 20OO 3O(7O 4OOO JO00

Temp. [K]

Figure 1.--ConUnued.

236 NASA/TP-3287/REV 1
4S

39

C_

[..) 26

2O

0

Original Data for Zr (o_,l],e)

.... I .... I .... I

. . . I .... I .... I .... I .... I . . .

]000 2000 3000 4000 5000

Temp. [K]

32

• 20

Coef Data for Zr (e,13,e)

'* I .... t .... I .... 1 ....

1000 200O 3000 4000 5000

Temp. [K]

Figure 1.--Concluded.

NASA/TP-3287/REV 1 237
REPORT DOCUMENTATION PAGE FormApproved

OMB No. 0704-0188

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1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED

February 2001 Tectinical Paper

4. TITLE AND SUBTITLE 5. FUNDING NUMBERS

Thermodynamic Data for Fifty Reference Elements

6. AUTHOR(S)

Bonnie J. McBride, Sanford Gordon, and Martin A. Reno

7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)

National Aeronautics and Space Administration

John H. Glenn Research Center at Lewis Field

Cleveland, Ohio 44135-3191

9. SPONSORING/MONITORING AGENCY NAME(S) AND ADDRESS(ES)

National Aeronautics and Space Administration

Washington. DC 20546-0001

WU-708-87-13-00

8. PERFORMING ORGANIZATION

REPORT NUMBER

E-6874-1

10. SPONSORING/MONITORING

AGENCY REPORT NUMBER

NASA TP-3287-REV 1

11. SUPPLEMENTARY NOTES

Bonnie J. McBride, NASA Glenn Research Center, Sanford Gordon, Sanford Gordon and Associates, 4078 Stonehaven

Road, Cleveland, Ohio 44121, and Martin A. Reno, Heidelberg College, Tiffin, Ohio 44883. Responsible person,

Bonnie J. McBride, organization code 5830, 216---433-5870.

12a. DISTRIBUTION/AVAILABILITY STATEMENT 12b. DISTRIBUTION CODE

Unclassified - Unlimited

Subject Category: 77 Distribution: Standard

Available electronically at hno://ehrs.mc.nasa._ov/GLTRS

This publication is available from the NASA Center for AeroSpace Information. 301-621-0390.

13. ABSTRACT (Maximum 200 words)

This report is a compilation of thermodynamic functions of 50 elements in their reference state. The functions are _p,

{H°(T)--H°(O)}, S°(T), and - {G°(T)-H°(O)} for the elements Ag, AI, Ar, B, Ba, Be, Br 2, C, Ca, Cd, CI 2, Co, Cr, Cs, Cu,

F 2, Fe, Ge, H 2, He, Hg, 12, K, Kr, Li, Mg, Mn, Mo, N 2, Na, Nb, Ne, Ni, 02, P, Pb, Rb, S, Si, Sn, Sr, Ta, Th, Ti, U, V, W,

Xe, Zn, and Zr. Deuterium D 2 and electron gas e- are also included. The data are tabulated as functions of temperature as

well as given in the form of least-squares coefficients for two functional forms for C_p with integration constants for

enthalpy and entropy. One functional form for _ is a fourth-order polynomial and the other has two additional terms, one

with T -1 and the other with T -2. The gases Ar, D2, e-, H 2, He, Kr, N2, Ne, 02, and Xe are tabulated for temperatures from

100 to 20 000 K. The remaining gases CI 2 and F 2 are tabulated from 100 to 6000 K. The polynomial functional form for

fCooPfOrall these gases is split into two temperature intervals--200 to 1000 K and 1000 to 6000 K. The second functional

rm for C_p has an additional interval from 6000 to 20 000 K for the gases tabulated to 20 000 K. The fits are constrained

so that the properties match at the common temperature endpoints. The temperature ranges for the condensed species vary

with range of the data, phase changes, and shapes of the C_p curves.

14. SUBJECT TERMS

Thermodynamic properties; Chemical elements

17. SECURITY CLASSIFICATION

OF REPORT

Unclassified

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OF THIS PAGE

Unclassified

19. SECURITY CLASSIFICATION

OF ABSTRACT

Unclassified

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241

16. PRICE CODE

All

20. LIMITATION OF ABSTRACT

Standard Form 298 (Rev. 2-89)

Prescribedby ANSI Std. Z39-18

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