NASA Technical Paper 1384 

LOAN COPY: RSYL!:' 

AWL TECHNiCAL B;! 

KIRTLAND AFB, N 

Space Shuttle Afterbody 

Aerody namics/Plume 

Simulation Data Summary 

Kenneth L. Blackwell and Leroy M. Hair 

DECEMBER 1978 

https://ntrs.nasa.gov/search.jsp?R=19790009639 2018-05-14T12:43:15+00:00Z
TECH LIBRARY KAFB, NM 

NASA Technical Paper 1384 

Space Shuttle Afterbody 

Aerody namicslPlume 

Simulation Data Summary 

Kenneth L. Blackwell 

George C. Marshall Space Flight Center 

Marshall Space Flight Center, Alabama 

and 

Leroy M. Hair 

REMTECH, Inc. 

Huntsville, A labama 

National Aeronautics 

and Space Administration 

Scientific and Technical 

Information Office 

1978 

TABLE OF CONTENTS 

Page 

SUMMARY ....................................... 

I . INTRODUCTION .............................. 

11 . TECHNICAL APPROACH ........................ 

A . GroundRule .............................. B . Saturn V Experience ......................... C . Fundamental Phenomena ...................... D . Simulation Status ........................... E . Technical Approach Details .................... 

111 . APPARATUS ................................. 

A . Test Facilities ............................ B . Description of Models ........................ C . Description of Auxiliary Equipment ............... D . Description of Instrumentation .................. 

Tv . TEST COKDITIONS ............................ 

A . Wind-On Tests ............................. B . Nozzle Calibrations ......................... 

V . SUMMARYOFDATA ........................... 

A . Basic Pressure Data ........................ B . Plumesize ............................... C . Nozzle Performance ......................... D . Space Shuttle Base Pressure Simulation Procedure .... 

REFERENCES ..................................... 

1 

1 

3 

11 

11 

12 

23 

26 

31 

31 

31 

33 

33 

41 

41 

46 

49 

iii 

. 
TABLE OF CONTENTS (Concluded) 

Page 

APPENDIX A - DATA OF PRIMARY INTEREST. ............. 51 

APPENDIX B - COMPLETE PRESSURE DATA .............. 74 

APPENDIX C - NOZZLE CALIBRATION DATA .............. 172 

APPENDIX D - BIBLIOGRAPHY OF TEST DATA REPORTS. ..... 181 

iv 
LIST OF ILLUSTRATIONS 

Figure Title Page 

2 

5 

8 

8 

10 

11 

13 

14 

15 

25 

26 

27 

1. Shuttle launch configuration . . . . . . . . . . . . . . . . . . . . . 

2. Plume induced aerodynamic trends . . . . . . . . . . . . . . . . 

3. Experimental concept . . . . . . . . . . . . . . . . . . . . . . . . . 

4. Schematic of gases used . . . . . . . . . . . . . . . . . . . . . . 

5. Overall program schematic . . . . . . . . . . . . . . . . . . . . 

6. Wind tunnel density variability . . . . . . . . . . . . . . . . . . . 

7. Model summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

8. Nozzle summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

9. Model details . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

10. Model installations . . . . . . . . . . . . . . . . . . . . . . . . . . . 

11. Heater schematic. . . . . . . . . . . . . . . . . . . . . . . . . . . . 

12. Gas generator design for Tests 2 and 6 . . . . . . . . . . . . . 

13. Base pressure trends for classic geometry 

(B~A~, B~A,). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 34 

Base pressure 36 14. trends for Orbiter class (BiAi) . . . . . . . . 

Base pressure trends for ET tap on ET/SRB class 

(BiA3S1, B2A4S2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15. 

38 

Base pressure trends for SRB tap on ET/SRB class 

( B iA3S1, B,A&) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16. 

39 

V 
LIST OF ILLUSTRATIONS (Concluded) 

Figure Title Page 

17. Base pressure trends for SRB-alone class 

(S3F1, S3FJ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 

18. Range of plume sizes . . . . . . . . . . . . . . . . . . . . . . . . . 42 

19. Example of wall pressure distribution from nozzle 

calibrations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43 

20. Effect of chamber pressure on wall pressure ratio . . . . . 43 

21. Comparison of analysis and experiment for 

nonair cases. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45 

22. Basic simulation procedure . . . . . . . . . . . . . . . . . . . . . 46 

23. Multiple body simulation procedure . . . . . . . . . . . . . . . . 48 

vi 
LI ST OF TABLES 

Table 

1 . 

2 . 

3 . 

4 . 

5 . 

6 . 

7 . 

8 . 

9 . 

10 . 

A-1 . 

A-2 . 

A.3 . 

A.4 . 

B.1 . 

B.2 . 

Title 

General Test Matrix .......................... 

Wind Tunnel Characteristics .................... 

Nozzle Dimensions (Summary) .................. 

N31 Measured Dimensions ...................... 

Configuration Buildups (Showing Test Numbers) ....... 

Base and Body Pressure Instrumentation Locations ..... 

Nozzle Pressure Instrumentation Locations Used 

in Wind-On Tests ............................ 

Estimated Instrumentation Errors ................ 

Test Quality Summary ........................ 

Test Condition Summary ....................... 

Test Data of Primary Interest . Classic Geometry ..... 

Test Data of Primary Interest . Orbiter Class ........ 

Test Data of Primary Interest . ET/SRB Class ....... 

Test Data of Primary Interest . SRB-Alone Class ..... 

Base and Body Surface Pressure Ratios (P/P ) for 43 Classic Geometry ............................ 

Base and Body Surface Pressure Ratios (P/ Pa ) for 

Orbiter Geometry ........................... 

Page 

9 

12 

18 

22 

24 

28 

29 

30 

32 

32 

53 

61 

67 

71 

76 

103 

vii 
LI ST OF TABLES (Concluded) 

Table Title Page 

B-3. Base and Body Surface Pressure Ratios (P/P OD ) 

for ET/SRB Class.. . . . . . . , . . . . . . . . . . . . . . , . . . 127 

B-4. Base and Body Surface Pressure Ratios (P/Pm ) 

for SRB-Alone Class . . . . . . . . . . . . . . . . . . . . . . . . . 150 

B-5. Nozzle Wall Pressures for Classic Geometry . . . . . . . . . 156 

B-6. Nozzle Wall Pressures for Orbiter Geometry . . . . . . . . . 161 

B-7. Nozzle Wall Pressures for ET/SRB Class . . . . . . . . . . . 165 

B-8. Nozzle Wall Pressures for SRB Class . . . . . . . . . . . . . . 170 

c-1. Nozzle Pressure Instrumentation Locations Used 

Only for Calibration Runs . . . . . . . . . . . . . . . . . . . . . . 173 

c-2. Nozzle Calibration Data for Classic Geometry . . . . . . . . 174 

c-3. Nozzle Calibration Data for Orbiter Class . . . . . . . . . . . 178 

c-4. Nozzle Calibration Data for SRB-Alone Class . . . . . . . . . 180 

viii 
NOMEN CLAN RE 

Symbol 

a 

A 

b 

CTPB 

d, D 

L 

m 

M 

MOC 

n 

P 

PBAN 

psi 

R 

C 

T 

V 

Definition 

Speed of sound 

Area 

Constant in nozzle pressure correction; see equation (2) 

Ca rb oxy-term inated p olybu tad i ene 

Diameter 

Length 

Gradient in nozzle pressure correction; see equation (2) 

Mach number 

Method of characteristics 

Exponent on y in simulation parameter 

Pressure 

Polybu tadiene acrylonitrile 

Pounds per square inch 

Dynamic pressure 

Radius 

Radius of curvature of nozzle throat profile 

Temperature 

Specific volume 

ix 
NOMENCLATURE (Continued) 

Symbol 

X 

Y 

E 

n 

e 

V 

Subscripts 

amb 

b 

C 

ex 

j 

t 

W 

a, 

* 

Definition 

Axial distance 

Specific heat ratio 

Initial slope of exhaust plume 

Nozzle expansion ratio, A /A* 

Nozzle wall angle 

Prandtl-Meyer angle 

Angular position of pressure tap 

ex 

Ambient 

Base 

Chamber 

Nozzle exit 

Plume boundary immediately after nozzle exit 

Total 

Wall 

Freestream 

Throat 

X 
NOMENCLATURE (Concluded) 

Configuration Buildups - (see Table - 5) ~~ 

*I*, Body, cone-ogive-cylinder, small; with short afterbody 

BIA2 Body, cone-ogive-cylinder, small; with long afterbody 

1A3S I Body, cone-ogive-cylinder, small; with ET-class afterbody 

and small SRB's 

B2A4S2 Body, cone-ogive-cylinder, large; with ET-class afterbody 

and large SRB' s 

S3FI SRB-alone with 10 deg flare 

s3 F2 SRB-alone with 20 deg flare 

Other Configuration Elments 

GI Gas - air 

G2 Gas - CF4 

G3 

G4 

G5 

Gas - from 2 percent aluminum/ CTPB/ ammonium 

perchlorate solid propellant 

Gas - from 16 percent aluminum/ PBAN/ammonium 

perchlorate solid propellant No. 1 

Gas - from 16 percent aluminum/ PBAN/ ammonium 

perchlorate solid propellant No. 2 

Nozzle - see Figure 8 and Table 3 i, i=1-34 N 

xi 
SPACE SHUTTLE AFTERBODY AERODYNAMI CSI PLUME 

SIMULATION DATA SUMMARY 

SUMMARY .I 

A series of parametric wind tunnel tests was conducted to provide a data 

base for developing a simulation of afterbody/base aerodynamics for multibody/ 

multibase rocket-powered vehicles ( such as the Space Shuttle) which use 

unheated air as the simulant gas in development wind tunnel tests. The tests 

described herein were parameterized on external configuration, nozzle internal 

configuration, base geometry, propulsion gas type ( air, CF4, solid propellant 

exhausts), and freestream Mach number (0.5 to 3.5). The tests were conducted 

over a 4 year period in the MSFC 14-Inch Trisonic, AEDC-PWT-4T, and Ames 

11-Foot wind tunnels. This report presents the data and pertinent reference 

information which would be necessary to perform an analysis which would lead 

to a simulation procedure. 

The type of data obtained during the tests described herein include model 

base, afterbody, and nozzle internal surface static pressure distributions, model 

chamber pressure and temperature, and freestream conditions. 

Also included is a brief description of simulation procedures that have 

been used by the Space Shuttle program. 

1. INTRODUCTION 

Design of rocket-powered vehicles such as Saturn I and V, Space Shuttle, 

and large military rockets is considerably influenced by the aerodynamic effect 

induced by the main propulsion rocket engines. Besides stability, control, and 

performance, there are structural considerations such as base heat shield loads, 

engine hinge torques, and interelement attach loads in multibody configurations. 

Aerodynamic design data for these vehicle types are usually obtained from wind 
tunnel tests of scaled vehicle models where the main propulsion engine plumes 

are simulated by flowing gases such as air or some product of combustion 

through model nozzles. 

The present study, which began in 1973, concerns the development of a 

plume simulation procedure for use in design of the Space Shuttle Launch Vehicle 

(SSLV) . The approach taken is based on knowledge gained during the Saturn 

programs. At the coinpletion of the Saturn V program, a study [ 11 was conducted 

to evaluate techniques used to obtain design base pressure values. Comparison 

of design values with those from flight telemetry were in variance by as much 

as 50 to 100 percent in the transonic Mach number range. These inaccuracies 

were attributed to several factors that had existed in the Saturn V wind tunnel 

simulations (e. g., a lack of knowledge of the prototype and model engine plume 

characteristics, insufficient parametric variation for model tests, simulation 

techniques, and test conditions). 

Because the SSLV is a more complex configuration than previous vehicles 

with its multibase/engine arrangement (Fig. 1) , it was estimated that the vehicle 

performance and structural integrity would be more sensitive to plume effects. 

Furthermore, the accuracies achieved during the Saturn V program were considered inadequate for Space Shuttle plume si.mulation. The literature was also 

probed for comparison of flight base pressure with that predicted by wind tunnel 

LIQUID-PROPEL 

SOLID ROCKET 

BOOSTER (SRB) 

D-PROPELLANT 

ROCKETS 

.LANT 

SOLID ROCKET 

BOOSTER (SRB) 

- ROCKETS 

EXTERNAL TANK (ET) 

Figure 1. Shuttle launch configuration. 

2 
simulations on large military launch vehicles. Again, similar base pressure 

prediction accuracies were found. It was then determined that a program should 

be initiated to develop improved plume simulation technology. 

The basic plan called for conducting a series of parametric wind tunnel 

tests that had sufficient controls to allow independent assessment of the pertinent 

variables. Variables included nozzle geometry, propellant gas type, chamber 

pressure, and chamber temperature for fixed model external geometry and 

wind tunnel freestream conditions. The previously mentioned matrix of variables 

was then repeated for configuration types which are important to the SSLV such 

as multiple nozzles and multiple bases. The propellant gases were chosen to 

encompass both air and SSLV prototype gasdynamic characteristics. Then, 

correlations could be tried until one was found which would reasonably overlay 

the base pressure effects using either air or prototype propellant gases. This 

approach could also be attempted for the various external configuration types 

and freestream Mach numbers to determine their applicability over the range of 

conditions that would be encountered with the SSLV. The objective of this report 

is to present the results of these tests in a compact synthesized form that will 

allow easy access to pertinent information for present and future analysis. 

11. TECHNICAL APPROACH 

A. Ground Rule 

Unheated air was chosen as the simulant gas to be used for conducting 

SSLV wind tunnel tests where the main propulsion plumes were to be simulated 

for steady-state aerodynamic purposes other than heating. The reasons for this 

decision were economics of data acquisition and previous experience with prototype simulations. For the number of data points required to describe the SSLV 

aerodynamics, combustion process simulations would be too slow and expensive. 

Furthermore, experience with the Saturn V program indicated that combustion 

process simulations were no better than cold flow simulations in describing the 

plume induced aerodynamic effects. 

B. Saturn V Experience 

There were several facts learned from the Saturn V program which influenced the approach taken for the Shuttle plume simulations. 

cult to model the plume or to calculate the plume flowfield properties of the 

First, it was diffi3 
prototype engines (F-1) of the Saturn V due to engine design peculiarities. 

The F-1 had an oxygen-to-fuel ratio gradient throughout the engine nozzle and 

plume. Furthermore, exhaust products from the engine turbines (that drive 

the main pumps) were dumped into the engine nozzle bell. The emphasis here 

is the fact that if the prototype flowfield characteristics are unknown, it will be 

impossible to provide an adequate simulation. Therefore, in conducting a 

program to provide a simulation for Shuttle, the ability to model and calculate 

engine plume characteristics must be considered. Second, only design point 

test conditions were obtained on the Saturn program, which limited the analysis 

that could be conducted as well as limiting the data application to a nominal 

trajectory. 

not adequately established, which further limited post-test/ flight analysis. 

Therefore, it was believed that for a plume simulation program to be a success 

it would be necessary to fully understand the model and prototype nozzle and 

plume flowfields, and to conduct the wind tunnel tests with some parametric 

variations. 

Finally, performances of the Saturn wind tunnel model nozzles were 

C. Fundamental Phenomena 

The basic phenomena of main propulsion plume induced aerodynamics are 

understood in terms of overall flowfield characteristics. However, due to its 

complexity the ability to compute the interacting flow between the engine plume 

and the external flow has eluded investigators (except for some simple geometries 

such as a cylindrical or boattailed afterbody with a single main propulsion nozzle) . Similarly, the problem has caused difficulty for the experimenters who would 

like to develop wind tunnel simulation procedures by which design data could be 

obtained for rocket-propelled vehicles with plume induced aerodynamic effects. 

The following discussion of the basic plume interaction phenomena provides a 

basis for this study. 

Base pressure is a prime indicator of the overall effect of a propulsion 

plume on the aerodynamics of the remainder of the vehicle. Figure 2 illustrates 

the general trend of base pressure as a function of engine chamber pressure. 

As chamber pressure increases from zero, base pressure decreases from the 

power-off value to a lesser value due to viscous aspiration by the plume. Then, 

as the plume size increases, there is an increasing compression effect until the 

point where there is separated flow on the afterbody of the vehicle. Various 

vehicles will operate over all or parts of this range of conditions. In Figure 2 

the insets 0, @ , and @ characterize the flowfields for aspiration, 

4 
BASE 

PRESSURE 

RATIO, 

ASPIRATION 

-I-- 

SSION 

1 .o FLOW SEPARATION FORWARD OF BASE 

COMPRESSION 

BOUNDARY 

LAY E R 

4- .- EDGE 

I 

Figure 2. Plume induced aerodynamic trends. 
compression without separation, and compression with afterbody flow separation, respectively. From an SSLV load sensitivity viewpoint, the main region 

of interest is from the aspiration region to high in the region of compression 

without separation. Although the SSLV eventually reaches altitudes where afterbody flow is separated, by then the loads have subsided. Therefore, the present 

plume simulation efforts were primarily concerned with the area between the 

aspiration region to the compression region short of flow separation. 

For this plume induced aerodynamic phenomenon, base pressure is 

hypothesized to be the fundamental quantity of interest. Then, to investigate 

this simulation problem in a parametric fashion, it is desired to know the 

measurable parameters considered for this investigation: model external geometry, external flow conditions (Moo , P - air assumed), nozzle internal 

geometry, and internal flow conditions (P , T , y, R, etc. - thermochemical 

characteristics which are fixed for each exhaust gas). 

, Tt a) t 

cc 

D. Sim u lation Status 

At the time this effort began, a study had been completed by Lott, et al. 

[ 11 of Saturn V flight base pressure results compared with those predicted 

through wind tunnel simulation, including a survey of the literature to expose 

and compare all known methods for simulation of rocket exhaust plumes and 

their effect on base pressure. The prime simulation used for the Saturn V cold 

flow tests was that of Goethert and Barnes [2]. The Goethert and Barnes 

procedure calls for a geometrically similar wind tunnel model test at trajectory 

Mach number in air with the rocket exhaust simulated by matching the P m /Pex 

and dv/dp. (For small plume expansion angles, matching dv/dp causes plume 

shape to be matched; however, for large expansions considerable error can 

occur.) However, Saturn flight results did not compare favorably with wind 

tunnel data employing the Goethert and Barnes simulation [ 11. Besides shortcomings in the simulation parameters, the lack of correlation was attributed to 

several factors: lack of sufficient nozzle calibration, lack of knowledge of complex prototype plume, and Reynolds number deficiencies. Furthermore, neither 

this simulation parameter nor any others proposed in the literature had been 

subjected to a systematic parametric investigation to ascertain their validity with 

a controlled prototype compared to a simulant. This study was initiated to provide a data base from which a simulation could be determined. 

6 
E. Technical Approach Detai Is 

After considering the problem of obtaining an improved plume simulation for use in Space Shuttle wind tunnel testing, it was decided that a building 

block parametric approach would be best. The approach would be empirical 

where a set of experimental (wind tunnel) data would be gathered to form the 

basis for developing simulation parameters. Then, variations of simulation 

parameters found in the literature would be compared to this data base to 

attempt a correlation of a "prototype" and a simulant gas for constant external 

conditions. Using basic physical concepts and aerodynamic theories, the 

correlation ( i. e. , simulation) parameters would be further molded to a form 

which could be used in a practical wind tunnel test situation. From this concept a set of generic tests was formulated to provide the parametric data 

required. Parameters to be considered included configuration, nozzle geometry, prototype and simulant gases, gas temperature and pressure, and 

freestream Mach and Reynolds numbers. It was decided to use a simple classic 

configuration (e. g. , the cone-ogive-cylinder) as a baseline for investigation of 

the plume-to-freestream interaction in the base region (Fig. 3). Initially, the 

base geometry was limited to two configurations: (1) a classic single nozzle 

with the exit plane aft of the base and (2) a triple nozzle arranged symmetrically 

on the base with the exit planes also aft of the base (Orbiter class). Using 

these configurations as baselines, the remaining parameters were varied. As 

illustrated in Figure 4, two gases were chosen as prototypes: (1) CF4 for its 

variable y characteristics at medium temperatures and (2) an aluminized solid 

propellant for its two-phase and high temperature characteristics. Air was 

used as the primary simulant gas. Later, helium was used to obtain a different 

constant y flow. Table 1 lists the matrix of gases and configurations that was 

used during this test series. When testing of these baseline configurations was 

completed, data were obtained for a configuration whose aft portion was modeled 

after the Shuttle External Tank (ET) /Solid Rocket Booster (SRB) combination 

to obtain configuration variations for the flared base SRB and the nearby 

unpowered ET base. Figure 5 shows the overall test program matrix. The 

tests have been assigned a test series number from 1 to 10. The NASA series 

numbers are cross-referenced in Figure 5. The figure also shows the type 

gas, configuration, and test facility used during each test series. It should be 

noted that data from three tests were not included because of their questionable 

quality; elements of those tests vital to the program goals were incorporated 

into other tests. 

7 
CLASSIC 

GEOMETRY 

SINGLE 

NOZZLE 

TRIPLE NOZZLE BASE 

(ORBITER LIKE) 

c=ck<qE 

'ET" 

MULTIBASE 

SOLID ROCKET BOOSTER 

(APPROACH FLOW FIELD EFFECTS) 

{ PROTOTYPES 

VAhlOUS FLARE ANGLES u-7 

SI MU LANTS 

Figure 3. Experimental concept. 

PROPELLANT 

COMBUSTION MODEL \' 

E4 HELIUM 

I I IH 

Figure 4. Schematic of gases used. 

8 
TABLE 1. GENERAL TEST MATRIX 

ET/SRB Class 

Gas (Triple Body) 

SRB Class 

( Flare) 

Helium 

Air 

CF4 

a 2% Aluminum 

b I 16% Aluminum 1 

Classic 

Geometry 

(Single 

No z z 1 e) 

d 

d 

d 

d 

d 

Model Configuration 

Orbiter 

Class 

(Triple 

Nozzle) 

a. Combustion products of ammonium-perchlorate-based solid 

propellant with 2 percent aluminum in CTPB binder. 

b. Combustion products of ammonium-perchlorate-based solid 

propellant with 16 percent aluminum in PBAN binder. 

Fundamental to this program was an understanding of the model nozzle 

performance at least to the exit plane. Based on experience with the Saturn V 

base pressure program and observation of other programs, it was believed 

that errors between flight and wind tunnel may have been the result of a lack of 

knowledge concerning the flow in the prototype and model nozzles. To conduct 

a parametric program such as this, it would be imperative to be able to 

accurately quantify parameters that would possibly be used in a simulation 

equation [ e. g., temperature and pressure (and thus y or other thermodynamic 

properties) 1. Therefore, great care was taken to provide instrumentation from 

which the nozzle performance could be determined. Furthermore, each nozzle 

was calibrated under quiescent external flow conditions. 

Finally, with known external flow properties at the base (essentially 

freestream for this slender cylinder) and known nozzle exit conditions, a position is established from which an empirical analysis of a set of parametric wind 

tunnel data can be conducted. This analysis would establish whether a simulation 

parameter exists for general use within the range of conditions encompassed by 

the test parameter variations and, if so,- would define it. 

9 

-_ 
CLASSIC ORBITER ET/SRB 

GEOMETRY CLASS CLASS 

(SINGLE NOZZLE) (TRIPLE NOZZLE) (TRIPLE BODY) 

SOLID 

EL LANTS 

TEST SERIES 2 

(MA11 F) 

-.- .- 

BASIC 

-_- - / 

/5 

(FA71 

<TI- 

' ,TRANSONIC Li_ - 

6 

(FA221 

CORRECTION 

/ 

I 

', 

/ 

'\ 

BASIC 

- __--- 

4-A 

TRANSONIC 

___-- - -. 

AIR, CF4 - - 

BASIC ___ ~ ~~ 

3 

(FA1 1) -=Ez= 

LOW 4 

4-9 

(FA61 

TRANSONIC 

-DATA QUESTIONABLE, ' NOT PRESENTED 

9-A 9-9 

(FA151 (FA151 

/' - L.- - 

/ ---. 

FILL IN GAPS 

(ALSO, He) 

SRB 

CLASS 

AIR, CF4 ~- ~ 

c DATA QUESTIONABLE, 

/' NOT PRESENTED 

CORRECTION 

a 

(FA231 

c=I@ 

0 LID PROPELLANTS 

\ 

\ 

I 

/ LOCAL MACH NO. 

(FLARE) ~ - ~~ ~~ ~ 

Figure 5. Overall program schematic. 

10 
I 11. APPARATUS 

Four types of equipment were used in this test program: wind tunnels, 

models, auxiliary equipment, and instrumentation. Each is described in the 

following paragraphs . 

A. Test Facilities 

There were three wind tunnels used in this program. The first facility 

was the NASA/MSFC 14 x 14 Inch TWT [ 31, an intermittent blowdown, variabledensity type with a 35.6 x 35.6 cm (14 x 14 in. ) square test section. The 

nozzles are symmetric about a horizontal plane. Speeds are varied in the subsonic range by a controllable diffuser, in the transonic range by regulating 

plenum suction around the perforations on all four tunnel walls, in the low supersonic range by interchangeable nozzle blocks, and in the higher supersonic range 

by tilting fixed-countour blocks. 

0.3 to 5.0. Reynolds number is proportional to Mach number for this and all of 

the other facilities used (Fig. 6). 

The Mach number range of the TWT is from 

10 x 106 

5 

E2 

01 

5 0.5 

\ 

0 

72 

v) 

A 

0 

Z 

U 

0.2 

0.1 0 1 2 3 4 5 

MACH NO. 

Figure 6. Wind tunnel density variability. 

11 
The second facility used was the NASA/Ames ll-Foot leg of the Unitary 

Plan Wind Tunnel [ 41 It is of the closed-return, continuous flow, variabledensity type with a 335 x 335 cm (11 X 11 ft) square test section. The nozzle 

has adjustable sidewalls. All four walls are slotted for transonic operation. 

The Mach number range is continuously variable from 0.5 to 1.4. 

The third facility used was the USAF/AEDC 4T [ 51, a closed-return, 

continuous flow, variable-density type with a 122 x 122 cm (4 x 4 ft) square 

test section and four perforated walls. The nozzle contour is fixed and speed 

is controlled by the pressure ratio across the nozzle and by regulating plenum 

suction around the perforated test section. 

Table 2 summarizes the characteristics of these three facilities. 

TABLE 2. WIND TUNNEL CHARACTERISTICS 

Test Section: 

Width, cm (in. ) 

Height, cm (in.) 

Length, cm (in.) 

Operational Mode 

Mach Number Range 

NASA/ MSFC 

14 X 14 Inch 

' Trisonic 

Wind Tunnel 

36 ( 14) 

51 (20) 

36 (14) 

B1 ow dow n 

0.3 to 5.0 

Designation 

NASA/Ames 

11 x 11 Foot 

Transonic 

Wind Tunnel 

335 (132) 

335 (132) 

670 (264) 

Continuous 

0.5 to 1.4 

B. Description of Modeis 

USAF/AEDC 

Pr opul si on 

Wind Tunnel 

4T 

122 (48) 

122 (48) 

381 (150) 

Continuous 

0.1 to 2.0 

There were four basic models used in this program. Figure 7 shows 

the model geometries and Figure 8 the associated nozzles. All details of the 

model external geometries are shown in Figure 9, and all internal nozzle 

dimensions are given in Tables 3 and 4. Instrumentation is discussed in 

Section III.D. 

12 
9.0 0 

1 Ci D = 3.810 em (1.500 in.) I ;J -4 t 

ii---’\ A2 

?f 

k4 

A1 

61 

(a) CLASSIC AND ORBITER CLASS FOR GASES AND SOLID PROPELLANTS 

0 = %E10 em (1.500 in.) ,065 D 

(b) ET/SRB CLASS FOR GASES 

* 

12.5d 9.78 D 

11 

0 = 18.334 em (7.21 8 in.) .027 D 

II 

82 

(e) ET/SRB CLASS FOR SOLID PROPELLANTS 

I= 11.960 I 

t 

0 = 2.385cm (.939 in.) 

4 n F 

(d) SRB CLASS FOR GASES 

Figure 7. Model summary. 

13 
I I, I.,,,,, I ...,I. 111 ,...- ---.--- 

SYMBOL APPROX. DE~ 

0 7.9 cm (3.1 in.) 

0 

O 

n 

2.3 cm (.9 in.) 

1.8 cm (-7 in.) 

1.6 cm (.&I in.) 3 

0 10 30 

LIP WALL ANGLE, 8, (deg) 

Figure 8. Nozzle summary. 

14 

- . . . . ... . .. 
(a) BIA1 - D = 3.810 cm (1.500 in.) 

(b) BlA2 - D = 3.810 cm (1.500 in.) 

(SAME AS BlAl UNLESS NOTED) 

Figure 9. Model details. 
7k.355d 1 

.090 d SPHERICAL RADIUS '1.315d DlAM 

.58xw1 5' t 

I 

I 4 .333 D 

9.783 D P 

r- n 

,225 D \ 

RADIUS 

.693 D 

SPHERICAL 

RADIUS 

\ 

L- '. 

1.081 

(2.441 

3 

D 

d) 

(c) B1 A3S1 - D = 3.81 0 em (1.500 in.); d = 1.687 cm (0.664 in.) 

(SAME AS B1 A1 UNLESS NOTED) 

,098 d SPHERICAL RADIUS 1.316 d DlAM 

p- 9.783 D Y 

\ .693 D 

SPHERIC AL 

RADIUS 

DlAM 

(d) B2A4S2 - D = 18.334 cm (7.21 8 in.); d = 8.108 em (3.192 in.) 

Figure 9. (Continued). 

16 
SPHERIC A1 

RADIU!: 

1.333 

2.1 30 

4.772 D 

I" 

1314D 

11.955 D DIAM, 1 

\ 

.319 D \ 

1.204 D 1.331 D 

(e) S3Fi - D = 2.385 em (0.939 in.) 

Figure 9. ( Concluded). 

Models BiAl and BiA, were approximately 0.4 percent scale of the Shuttle 

Orbiter and 1.0 percent scale of the Shuttle SRB. The design of model BlAl 

provided for ducting of heated high-pressure gases through the supporting strut 

to a plenum in the cylindrical portion and mounting within the afterbody (Ai) 

various nozzle designs connecting to this plenum. There were up to 47 pressure 

and 6 temperature instrumentation leads within the model mold lines. Model 

BiA, was as similar to BiAi as practical. The only difference in external shape 

was a modest length increase to incorporate the solid-propellant-burning gas 

generator (discussed in Section III. C) . However, the significantly different 

internal requirements led to a separate, complete model. As with model BlAl, 

various nozzle designs were mounted within the afterbody ( A2). There were 12 

pressure instrumentation leads plus ignition wires accommodated within the 

model mold lines. 

17 
TABLE 3. NOZZLE DIMENSIONS (SUMMARY) 

I a Design Measured 

Nozzle 

1A 

1B 

1c 

1D 

1E 

2A 

ex D* L D ex 

D 

n cm n cm cm cm 

e 

Gas (deg) E ( in.) C /R* (deg) E (in. ) (in. ) (in. ) 

e 

I 2B 

2 2.41 

394 

394 

394 

394 

394 

394 

I 

15 

15 

15 

15 

15 

15 

15 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

8.0 

8.0 

8.0 

8.0 

8.0 

4.0 

4.0 

- 

6.34 

3.63 

3.63 

3.59 

3.44 

3.79 

3.82 

Classic Geometry 

15.1 

14.9 

14.7 

15.0 

15.0 

15.2 

15.0 

8.03 

7.88 

7.88 

7.92 

7.97 

4.05 

4.09 

2.33 

(0.918) 

1.88 

1.77 

(0.697) 

1.77 

1.77 

(0.696) 

1.77 

(0.698) 

1.79 

(0.706) 

1.78 

(0.700) 

1.78 

(0.700) 

(0.696) 

, 

0.625 

(0.246) 

0.630 

(0.248) 

0.630 

(0.248) 

0.630 

(0.248) 

0.635 

(0.250) 

0.884 

(0.348) , (0.740) 

0. 879 1.85 
TABLE 3. (Continued) 

(0.526) 

1.18 

(0.466) 

0.73 

(0.289) 

3.01 

(1.186) 

1.81 

(0.711) 

I 

1 

I 

Nozzle 

! 

1 

: 

a Design 

3.1 

3.1 

Measured 

7.86 

(3.09) 

7.86 

( 3.09) 

____lj I 

L' 

(in.) 

2.80 

3.35 

E 

20.4 

20.2 

ex 

D 

cm 

(in.) 

4.46 

(1.757) 

4.46 

(1.757) 

ex 

cm 

( in. ) 

D 

5.72 

(2.252) 

6.21 

(2.446) 

D* 

em 

( in.>) R /R, Gas C E 

25 

35 

35 

3.5 

6.5 

3.5 

1.78 

(0.700) 

1.78 

(0.700) 

1.78 

(0.700) 

4.04 

3,64 

0.86 

25.0 

35.1 

34.9 

3.58 

6.51 

3.52 

1.78 

(0.700) 

1.77 

(0.694) 

1.78 

(0.700) 

0.942 

(0.370) 

0.691 

(0.272) 

0.947 

(0.373) 

SRB - Alone Class 

15 

25 

8.0 

5.0 

2.31 

2.31 

(0.909) 

(0.909) 

11 

12 

3.78 

- 

8.19 

5.14 

2.30 

(0.907) 

2.31 

(0.911) 

0.805 

(0.317) 

1.02 

(0.402) 

2 14.9 

25.1 

ET/SRB Class 

21A 

21B 

20 

20 

3.10 

3.09 

7.88 

(3.093) 

7.84 

(3.088) 
TABLE 3. (Continued) 

C 'R* Nozzle 

n 

e 

(deg) 

22A 

22B 

2 3A 

23B 

24A 

24B 

4.06 

3.97 

4.00 

4.00 

3.96 

31Ab 

31Bb 

31 Cb 

14.9 

15.0 

25.2 

24.9 

35.0 

Gas 

6 5.3 1.03 - 6.4 5.34 1.02 0.442 

6 5.3 1.03 - 9.1 5.28 1.02 0.445 

6 5.3 1.03 - 6.6 5.33 1.03 0.445 

(0.404) (0.402) (0.174) 

(0.404) (0.402) (0.175) 

( 0.404) ( 0.404) ( 0.175) 

- 

1 

1 

1 

- 

1.63 

(0.640) 

1.62 

(0.639) 

1.64 

( 0.647) 

a 

Design 

15 

15 

25 

25 

35 

35 

~~ 

E 

8.0 

8.0 

5.0 

5.0 

8.0 

8.0 

ex 

D 

cm 

(in.) 

1.63 

(0.643) 

1.63 

(0.643) 

1.63 

(0.643) 

1.63 

(0.643) 

1.63 

(0.643) 

1.63 

(0.643) 

Measured 

E 

8.01 

7.99 

4.92 

4.92 

8.09 

8.04 

ex 

cm 

(in. ) 

D 

1.61 

(0.634) 

1.61 

(0.633) 

1.60 

(0.632) 

1.60 

(0.632) 

1.63 

(0.640) 

1.62 

(0.638) 

D* 

cm 

(in.) 

0.569 

(0.224) 

0.569 

(0.224) 

0.724 

(0.285) 

0.724, 

(0.285) 

0.572 

(0.225) 

0.572 

(0.225) 

~~ 

1 

cm 

(in.) 

2.09 

(0.821) 

2.08 

(0.819) 

1.27 

(0.500) 

1.25 

1.12 

(0.440) 

1.11 

(0.438) 

(0.494) 
TABLE 3. ( Concluded) 

Nozzle 

32A 

32B 

32 C 

33A 

33B 

33c 

34A 

34B 

34 c 

Gas 

a 

Design 

10 

10 

10 

15 

15 

15 

25 

25 

25 

E 

4.0 

4.0 

4.0 

8.0 

8.0 

8.0 

4.0 

4.0 

4.0 

ex 

D 

cm 

( in. ) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

(0.404) 

1.03 

( 0.404) 

1.03 

(0.404) 

R /R, 

C 

4.12 

4.10 

4.08 

5.42 

5.53 

5.53 

3.98 

4.07 

4.05 

10.1 

10.0 

10.1 

14.8 

15.0 

15.1 

24.6 

25.4 

25.2 

Measured 

E 

4.06 

4.00 

3.96 

8.30 

8.29 

8.29 

4.04 

4.16 

4.08 

ex 

cm 

(in.) 

D 

1.02 

( 0.401) 

1.02 

(0.400) 

1.02 

( 0.400) 

1.04 

(0.409) 

1.03 

(0.406) 

1.03 

( 0.406) 

1.03 

(0.404) 

1.03 

(0.406) 

1.03 

(0.404) 

a. Design R /R, = 4.0 unless noted. 

b. Contoured profile: see Table 4 for coordinates; design R /R, = 3.1. 

C. Calculated from other measured parameters. 

NOTE: Measurements were rounded from English to nearest SI unit. 

C 

C 

D* 

cm 

(in.) 

0.505 

0.508 

0.511 

0.361 

(0.142) 

0.358 

(0.141) 

0.358 

(0.141) 

0.511 

0.505 

0.508 

(0.199) 

( 0.200) 

(0.201) 

(0.201) 

(0.199) 

(0.200) 

1 

cm 

(in.) 

1.53c 

(0. 603c) 

1.53c 

(0.603C) 

1.51c 

1.37 

(0.540) 

1.36 

1.37 

(0.538) 

0.79 

(0.311) 

0.79 

(0.310) 

0.79 

(0.312) 

( 0.5959 

(0.537) 
TABLE 4. N,i MEASURED DIMENSIONS 

X/ R, 

DESIGN 

0 

0.274 

0.558 

0.843 

1.128 

1.413 

1.698 

1.983 

2.268 

2.553 

2.838 

3.123 

3.408 

3.693 

3.978 

4.262 

4.547 

4.832 

5.117 

50 402 

5.687 

5.972 

6.257 

6.542 

6.827 

7.112 

7.397 

Design 

1.000 

1.004 

1.020 

1.048 

1.090 

1.143 

1.213 

1.284 

1.360 

1.433 

1.504 

1.575 

1.641 

1.706 

1.769 

1.827 

1.883 

1.935 

1,986 

2.034 

2,081 

2.124 

2,163 

20 202 

2.237 

2.271 

2.303 

__ _ 

R/ R, 

DESIGN 

A 

0.992 

1.007 

1.025 

1.052 

1.086 

1.141 

1.204 

1.274 

1.351 

1.426 

1.494 

1.565 

1.634 

1.696 

1.756 

1.814 

1,871 

1.927 

1,977 

2.023 

2.067 

2.111 

2.149 

2,188 

2.222 

2,259 

2,291 

~-~ -. 

Measured 

B 

0.997 

1.004 

1.027 

1.061 

1.108 

1.169 

1.243 

1.316 

1.390 

1.463 

1.534 

1.594 

1.667 

1.731 

1.788 

1.847 

1, 901 

1.952 

2.000 

2.048 

2.092 

2,136 

2.173 

2.211 

2.249 

2.294 

- 

__ .~ 

- 

~ 

C 

0.997 

1.006 

1.022 

1.051 

1.087 

1.140 

1.206 

1.280 

1.355 

1.431 

1.502 

1.566 

1.639 

1.703 

1.765 

1.824 

1.880 

1,933 

1,986 

2,032 

2.079 

2.123 

2.164 

2.197 

2.230 

2.269 

2.302 

22 
Model BiA3S~ was approximately 0.5 percent scale of the Shuttle ET/ SRB 

combination and used much of the model BiAi hardware. Afterbody A, carried 

the heated high-pressure gases from the Bi plenum to secondary plenums in 

each of the attached model SRB' s (Si) . The aft end of Si permitted the mounting 

of various nozzle designs. 

the outside of Si to a port in the side of Bi; all other instrumentation leads were 

routed internally. Model B,A4S, was approximately 2.2 percent scale of the 

Shuttle ET/SRB combination and 481.2 percent scale of the BiA,Si model. The 

only gas ducting needed on this model was for a small amount of ignition gas to 

the SRB' s (S,) , detailed in Section III. C. Transducers for the 29 pressure 

leads were mounted within B,. 

routed on the outside of S, to a port in the side of B,; all other instrumentation 

leads were routed internally. Model S,F was approximately 0.6 percent scale 

of the Shuttle SRB. The design of model S3 was similar to that of Bi, providing 

for ducting of heated high-pressure gases through the strut to a plenum in the 

cylindrical portion, which connected to the various nozzle designs mounted in 

the aft end. There were thirteen pressure leads and one temperature instrumentation lead accommodated within the model mold lines. 

Pressure leads for SRB pressures were routed on 

Pressure leads for the SRB base pressures were 

All of the various configuration buildups that were tested are defined in 

Table 5. 

respective wind tunnels. 

Figure 10 shows installation photographs of some of the models in their 

C. Description of Auxiliary Equipment 

There were two significant pieces of auxiliary equipment developed 

specifically for this test program. 

(Fig. 11). There were three close-coupled tanks. Pneumatically driven compressors pumped low pressure gas to the cold tank. 

controlled supply for the heater tank, where the gas could be electrically heated 

as desired. A mixing valve was used to control the temperature of the gas 

delivered to the model. Gases could be delivered at 13.8 MN/m2 (2000 psia) 

and 600 K (1060°R), at flow rates up to 1.8 kg/ s (4 lb/ s) for 10 S. A small 

relief tank permitted operational flexibility, especially in preventing loss of 

expensive CF4 gas. The gas heater was used to provide heated high-pressure 

gases to models BiAi, BiA3Si, and S3F. The gases used were air (GI) and CF4 

The first was a high-pressure gas heater 

This tank was used as the 

(G2) 

23 
TABLE 5. CONFIGURATION BUILDUPS (SHOWING TEST N 

- 

~~ - 

Nozzle 

NIA 

- 

N3 

N4 

N5 

N31 

N33 

N34 

N32 

.. 

NIB 

1c N 

NID 

*1 E 

N2A 

N22 

N2 3 

N2B 

. .. 

N24 

21 N 

._ 

N 

11 

N12 

N 12 

G1 

(Air) 

lb 

la 

la, 3b 

1, 3b 

3a 

3a 

3 

la 

2b 

2b 

gb 

gb 

2b 

6 

I 

7 

1 oa 

1 oa 

- 

Gases - 

G3 

(2% Aluminum) 

2 

6 

6 

2 

6 

- 

G4 

(16% Aluminum) 

.- 

2 

6 

6 

2 

6 

~. - 

a. 

b. 

Also have nozzle calibration data - see Appendix C. 

Have only nozzle calibration data - see Appendix C. 

24 
(a) CONFIGURATION B,A1 IN MSFC 14 x 14 INCH TWT (TEST 1) 

(6) CONFIGURATION B1A7 IN AEDC-4T (TEST 6) 

(c) CONFIGURATION S3F2 IN MSFC 14 X 14 INCH TWT (TEST 10) 

Figure 10. Model installations. 

25 
TO MODEL 

62 liters (2.2 ft3) 27.6 MN/m2 (4000 psia) 

TO MODEL 

MIXER 

62 liters (2.2 ft3) 

R EG U LATO R 

COLD TANK HEATER TANK 

670 K (1200°R) 

195 liters (6.9 ft3) 

13.8 MN/d (2000 psia) 

119 liters (4.2 ft3) 

27.6 MN/m2 (4000 psia) 

PUMP # 

I - 1 FROMSUPPLY VENT 

Figure 11. Heater schematic. 

The second piece of auxiliary equipment developed was the gas generator 

used on Tests 2 and 6 to supply hot exhaust products from solid propellant combustion (Fig. 12). This device was developed for use with model BlA, [ 61 and 

was designed as an integral part of the model so that the combustion chamber 

outside wall formed the outer mold lines of the aerodynamic surface (BlA,) . Ignition was provided by a single, head-end mounted electric squib. It produced 

the exhaust products from the combustion of either a 2 percent aluminum CTPB 

formulation ( G3) or a 16 percent aluminum PBAN formulation ( G4). Details 

of these formulations and predicted specie are found in Reference 7. The model 

SRB (%) used on Test 8 with model B2A4 had been developed on an earlier test 

program described in Reference 8. For Test 8, a 16 percent aluminum PBAN 

formulation ( G5) was used instead of the 15 percent aluminum PBAN formulation of Reference 8. 

D. Description of I nstrumentation 

Static pressures on the model's external surface, base, and internal 

nozzle together with model chamber pressures were measured with remotely 

located conventional pres sure transducers. Chamber temperature for the 

26 
u 

END VIEW 

LENGTH OF PROPELLANT AS REQUIRED 

TO ACHIEVE DESIRED Pc 

ALL PROPELLANT EDGES 

INHIBITED FROM BURNING 

k1.3 cm (0.5 in.) r OUTER MOLD LINE OF MODEL BODY 

I NOMINAL 1 

DIAPHRAGM CLOSURE 

ALUMINUM PROPELLANT HOLDERS 

QUAL1 ZATION 

PROPELLANT 

Figure 12. Gas generator design for Tests 2 and 6 

(adapted from Reference 6). 

noncombustion gases was measured with a thermocouple total temperature probe 

located in the model stilling chamber. The external surface pressure orifice 

locations are presented in Table 6. 

regions or immediate vicinity. 

orifices on the cylindrical portion of the body, but not all of these were monitored on every test. 

The majority were located in the base 

Model BlAl had a considerable number of 

All of the nozzle internal surface pressure orifice locations used in 

wind-on tests are presented in Table 7. For Tests 2, 6, 8, and 10, each nozzle 

had three orifices monitored at different axial positions. However, for Tests 1, 

3, and 7, only one tap per nozzle was monitored. Some of the nozzles used with 

the classic-geometry body in Test 1 had a greater number of orifices (used during the nozzle calibration testing), but only one was monitored for wind-on runs. 

The estimated errors associated with all of the pressure instrumentation 

are presented in Table 8. 

27 
TABLE 6. BASE AND BODY PRESSURE 

INSTRUMENTATION LOCATIONS 

Base Region (S/D = 0) Body Region ( r/R = 1.0) 

x/ D 

~ 

Modi 

- 

r/ I 

Q 1 (io0 

0. 32 

0.84 

0.52 

0.8-1 

(0) 

0.52 

0.84 

Q = 150 

(0) 

0.879 

- 

0.9G9 

_- 

Class 

Classic 

and 

Orbiter 

0.931 

0.992 

0.843 

0.797 

~~ J ETa 

0.742 

0. 8x1 

~~ 

Configuration 

Class 4% =6 

0.04 

0.22 

0.40 

0. 58 

0.76 

0.94 

1.12 

1.30 

1.48 

2.20 

2.92 

__ 

hIodel 

0.04 

0.22 

0.40 

0.58 

0.76 

0.94 

1.12 

1.30 

1.48 

2.20 

2.5G 

2.92 

3.28 

0.03 

0.33 

0.67 

0.083 

0.250 

1.84 

__ 

~ 

0.583 

0.52 

0.84 

BiAi 

Classic 

Orbiter 

(0) 

0.531 

0.931 

0.992 

0 = 275'1. 

270'1 

-. __ 

-~ __ 

0.843 

o.nu 

ET I 

0.797 

0.797 B2'4.l 0.017 

0.052 

0.742 0.121 

0.742 

~ .- 

Q : 270'H 

274'1 

0.121 

0.360 

0.599 

0.759 

1.002 

1.246 

0.109 

3.190 

3.271 

3. :$tx 

3.4GG 

1.547 

- 

SRB 

a. Measured from cylinder/doinc tangent point. 

28 
TAB LE 7. NOZZLE PRESSURE INSTRUMENTATION LOCATIONS 

USED IN WIND-ON TESTS 

Nozzle A/ A, Tap 8 8 

No. (deg) x/L A/A* :z (deg) X/L 

11 

12 

3 180 0.557 3.91 2 180 0.795 6.00 1 180 0.937 7.66 

3 180 0.686 3.05 2 180 0.812 3.83 1 180 0.932 4.64 

I I Upstream Tap I Middle Tap Downstream TaD 

Classic Geometry 1 2A 

- 

7.36 

7.27 

7.33 

7.53 

7.62 

3.78 

3.91 

3.06 

5.77 

2.78 

- 

0.942 

0.943 

0.952 

0.963 

0.967 

0.942 

0.959 

0.895 

0.938 

0.806 

2 

2 

2 

2 

2 

2 

_____ 

180 

180 

180 

180 

180 

180 

0.155 

0.236 

0.181 

0.191 

0.268 

0.304 

0.569 

0.622 

0. 608 

0.612 

0.644 

0.655 

3.92 

4.04 

4.19 

4.25 

2.56 

2.67 

240 

240 

240 

SRB-Alone Class 

ET/ SRB - 

3.02 

2.99 

7.37 

7.36. 

4.32 

4.37 

6.70 

6.58 

Class i 

24B 

180 

180 

180 

180 

180 

180 

180 

180 

0.661 

0.681 

0.106 

0.114 

0.678 

0.680 

0.430 

0.436 

2.07 

2.04 

1.18 

1.19 

2.84 

2.90 

1.64 

1.64 

180 

180 

180 

180 

180 

180 

180 

180 

0.976 

0.973 

0.940 

0.943 

0.916 

0.921 

0.907 

0.902 

22 

3 2 

22 

32 

22 

32 

24 

34 

24 

34 

24 

34 

180 

180 

23 180 

33 180 

I Orbiter Class 

II 47 

48 

47 

48 

47 

48 

47 

210 

150 

210 

150 

210 

150 

2 10 

0.940 

0.941 

0.923 

0.928 

0.885 

0.879 

0.810 

~ 

4.96 

5.27 

3.68 

3.67 

6.99 

6.92 

3.09 

29 
I 11111111 I I1111 II II I I I1 I1111111111 1111 I111111 1.11 ,111 ,..,..I.,,. 11-.1. ,..,.,-- I 

TABLE 8. ESTIMATED INSTRUMENTATION ERRORS 

Pt Tunnel : 

P 

q 

bl 

hIodel base and 

surface 

Nozzles All 

g 

h 

i 

1 Ag 

lAh, 3, 5, 32, 34 

lAi, 4, 33 

Ai', 311<, 3Z1', 3311 

4j, 5, 313, 323, :A 

0.34 

0.10 

0.78b 

0. 2(ic 

130.0 

26.2 

7.58 

1.57 

Model base and 

surface 

L Chamber 

Nozzles All 

R 

h 

i 

1Ag 

lAh, 3, 5. 02, 34 

lAi, 4, 3: . , 

4j. 5, :j1J, :zJ, :::!I 

4k, 51, :Ilk, ::2k, :i:ik 

~~ 

0.050 

0.015 

0.113b 

0.0::xc ~ 

18.75 

:i. 75 

1.1:: 

0.227 

~ -. 

SI Units 

0.34 

0.10 

2.61 

110.0 

24.0 

31 10 

- Tolerances ( I kN/ in2: 

0. :"4 

0.10 

0.15 

21.0d 

1.55f 

5. 17e 

1. T,5 

0.31 

. 0.24 

0.10 

0.78b 

O.?(ic 

130-0 

2. (j 

j,, Customary Units - Tolerances ( 

0.050 

0.015 

0.37x 

l(i.0 

3.47 

0.050 

0.015 

0.022 

::. od 

0.225f 

0. 750" 

0.225 

0.046 

~~ ~ 

a. 

h. iV 2.0. 

c. M :;.5. 

d. 3.4 P 6 I:;. x ~i~/ni' (500 c P 2000 psi). 

e. 1.0 P < :!..! R.IN/II~~ (150 6 P c 500 psi). 

1. P < 1. o IN/ ni2 ( P < 150 psi). 

fi. Ilpstrcam tap. 

Tolerance depends on Mm ; masitnum valuc shown. 

c c 

c 

c 

0.050 

0.015 

0.11:ib 

0.038C 

1x. 75 

0. :175 

o.:i7a 

0.85" 

0. loa' 

0.17 

6:i. 0 

17.9 

X. 96 

2.7G 

xi) 

0.054a 

0.124a 

0.015a 

9.2 

2.59 

1.25 

0.36 

- 

0.51a 

1.2xa 

0.14" 

0. 04(ja* 

55.8 

7.7a9 m 

13.6 

1.38 

0. ($9 

~~ 

0. 074a 

0.18P 

0.020a 

0. 04Ga. 

8.1 

7.7a. n' 

2.0 

0.2 

0.1 

Anics 

1 1 -Foot 

8 

0.78 

52.0 

2.6 

0.113 

7.5 

~- 

0.375 

11. Middle tap. 

i. Downstream tap. 

i. "lli~li" P range. 

k. "I.o\v" P range. 

c 

<' 

1. "Low" P range for downstream tap. c 

111. Tolerance in I P/ P . 

30 
IV. TEST CONDITIONS 

A. Wind-On Tests 

The, equipment previously described was assembled in various combinations for a series of tests (Table 5) . Test 1 was the initial exploratory and 

feasibility investigation, using air (GI) and CF4 ( G2). Test 2 was a limited 

extension of one of the Test 1 configurations (classic geometry) into hot 

exhausts from solid propellant combustion, G3 and G4. Test 3 was another 

extension of a different Test 1 configuration (Oribter class) into small-size 

plumes (primarily via nozzles with smaller exit wall angles than on Test 1) and 

limited to transonic speeds and air (GI). Test 6 was an extension of Test 2 into 

the transonic regime. Test 7 introduced a different body geometry (ET/SRB 

class) with GI and G2. Test 8 was an extension of the Test 7 study of hot 

exhausts from solid propellant combustion. This model was considerably 

larger only to utilize existing hardware with proven capability for simultaneous 

ignition of the two rockets. The propellant formulations used in Tests 2 and 6 

were not readily available in adequate quantity; consequently, a formulation ( G5) 

was used that was very similar to G4. Test 10 was an inquiry into the applicability of the conclusions reached with the classic geometry tests to the flare 

configuration of the SRB, using GI and G,. Some of the tests using air (GI) were 

conducted at chamber pressures and temperatures which resulted in condensation within the nozzles or in the initial plume expansions. Such data were 

retained, although their utility or applicability to devising a simulation parameter may be questionable. 

Table 9 presents a quality summary of the previously mentioned tests. 

From the table it can be seen that the bulk of the data were acceptable. Table 10 

summarizes the conditions of the tests. 

chamber and tunnel freestream parameters are given in Appendix A, and the 

complete set of base, body, and nozzle pressures are given in Appendix B. 

The specific values of the model 

B. Nozzle Calibrations 

The nozzle calibration activities were incorporated to quantify the operation of each nozzle under controlled conditions. The MSFC 14 x 14 Inch TWT 

was used. Nozzles designed for use with air and CFQ were calibrated as mounted 

for the wind-on tests, using the high pressure gas heater for air supply. Nozzles 

31 
,, ,. ,.. .... . . .. . . . - ___ 

TABLE 9. TEST QUALITY SUMMARY 

Data Usability 

1 (MAlOF) Acceptable, some d-iscrepancies in nozzle wall pressures 

3 ( FAU) 

6 (FA22) 

7 (FA20) 

Acceptable, some discrepancies in nozzle wall pressures 

Low confidence in P values due to propellant contamination 

Acceptable 

~ ~~ 

~ __ __ .- ~- .. 

Subsonic and low supersonic data unacceptable due to tunnel control being 

too slow to respond to plume-induced pressure transient, before motor 

termination; quality of pressure transducers questionable for supersonic 

data 

Transonic portion acceptable; unresolved quztion concerning which 

nozzle was used on left and right SRB 

2 (MA11F 

8 ( FA23) 

1 io (FAN) Acceptable for qualitative comparisons within this data set, but tunnel 

interference precludes quantitative comparison with data from other 

sources ___ _. - - .. - J 

FABLE 10. TEST CONDITION SUMMARY 

Gas 

1 

1 

1 

~ 

2 

~- 

3,4 

3.4 

3.4 

3.4 

1 

1 

1 

1 

2 

1 

1 

2 

5 

1 

2 

1 

- 

- 

Test 

Series 

Configuration 

Class 

Mm 

0.5 1.0 1.5 2.0 3.5 

-IT .- 

Nozzls 

3 

4 

5 

1A 

a 

a 

a 

a 

Classic 

IB, 1C 

lD, 1E 

2A 

2B 

31 

32 

33 

34 

33 

23 

24 

22 

2 

6 

2 

6 

3 

3 

3 

1 

1 

7 

7 

7 

8 

10 

10 

10 

~~. 

__ 

__ 

- 

~ 

Orbiter 

ET/SRB 

21 

12 

11 SRB 

S3F2 - 

12 

32 
designed for use with solid propellant exhausts were calibrated with a special 

test section. Pressures in the chamber surrounding the specimen nozzle and 

air supplied to the nozzle chamber were controlled to levels required to achieve 

a specified value of P /P 

the basic wind-on tests. The specific values of the ambient and modei chamber 

conditions are given in Appendix C. 

Instrumentation was the same as that used for 

c amb' 

V. SUMMARY OF DATA 

A considerable amount of data was acquired during this test program. The 

bulk of the data is presented in the appendices. Appendix A gives the tunnel 

freestream and model chamber conditions, together with the one base pressure 

value for the location judged to be most representative for the respective body 

geometry type. Appendix B gives all of the base, body, and nozzle pressure 

data. Nozzle calibration data are presented in Appendix C. The test data 

reports from which all data were taken are listed in Appendix D. 

From the beginning of this test program it was envisioned that a plume 

simulation would be required to cover a spectrum of flowfields (from those 

generated by plumes small enough that base pumping existed through sizes where 

flow was separated over the vehicle afterbody). However, as the Space Shuttle 

program developed it became evident that the SSLV would not have significant 

flow separation during that portion of flight involving significant dynamic pressure. 

induce flow separation was reduced. There are some data included in this document where flow was separated over an afterbody, but the amount of flow separation and the range of variables investigated was not sufficient for a thorough 

analysis. The most important contribution to the literature is the base pressure 

results. Therefore, in summarizing the results only base pressure data will be 

considered. 

Therefore, emphasis on the region of large plume sizes which would 

A. Basic Pressure Data 

To provide an overview of the data, the basic base pressure data have been 

plotted as Pb/Pm versus P /P (Figs. 13 through 17). The data are presented 

by configuration class with data for the various nozzle/gas pairs on each plot. 

This type presentation allows a quick overview of the range of base pressure 

available and the relationship of any particular nozzle to the other nozzles in 

affecting base pressure. The data inthese plots are tabulated in Appendix A, 

together with the wind tunnel freestream and model chamber conditions. 

CQ, 

33 
8 

n 

c 

U 

K 

W 

K 

3 

v) 

v) 

W 

K 

n \ 

P 

P 

W 

1.2 

1 .o 

0.8 

100 200 300 

CHAMBER PRESSURE RATIO, Pc/P, Ib 1 M,%O.9 (c) MmX1.2 

Figure 13. Base pressure trends for classic geometry ( BIAI, BiA2). 
* . . . . . . . 0 TAP 

I 

a 

a 

w 

w 

v) 

U 

m 

15 20 40 60 200 400 200 400 600 lo00 2000 

CHAMBER PREGSURE RATIO, PJP, 

(d) Mm= 1.5 (e) b"3.5 

Figure 13. ( Concluded). 
w 

Q, @Pap 

(a) Mm*0.5 (b) M,x0.7 

1.4 

1.2 

1.0 

0.8 

0.6 

0.4 

10 20 40 60 100 200 300 10 20 40 60 100 200 300 

CHAMBER PRESSURE RATIO, P,/Pm 

(c) MmZ0.9 (d) Mm%1.2 

Figure 14. Base pressure trends for Orbiter class ( BIA1). 
CHAMBER PRESSURE RATIO, PJP, 

(e) M,Z 1.5 (f) M,%3.5 

Figure 14. (Concluded). 
w 

aJ 

CHAMBER PRESSURE RATIO, PclP, 

(a) b-13 If) 4-2.0 

Figure 15. Base pressure trends for ET tap on ET/SRB class (BiA3S~, B2A,S2). 
I 

(r) Moa 20.5 (bP M, aO.9 

h 

w 

cn 

10 20 4060 100 200 500 10 20 4060 100 

CHAMBER PRESSURE RATIO, P,/P,, 

b) Mw=l.3 (f) M,*20 

Figure 16. Base pressure trends for SRB tap on ET/SRB class ( B1A3SI, B2A4S2) . 
.... 

(a) M,X 0.5 

1.2 

1 .o 

0.8 

0 0.6 

(c) M,X1.2 

0 

(b) M,e0.9 

(d) M,z1.5 

CHAMBER PRESSURE RATIO, Pc/P, 

(e) M,-"2.0 (f) M,e3.5 

Figure 17. Base pressure trends for SRB-alone class ( S3FI, S3F2). 
B. Plume Size 

Base pressure is affected by plume flow in the base region, and the size 

of the plume is a first order parameter to be considered in performing simulation analyses. 

of relative plume size. The range of plume sizes available in the data as a 

function of M , gas type, and configuration class is shown in Figure 18. 

Furthermore, the initial plume angle (6 .) is a good indicator 

J 

Q) 

C. Nozzle Performance 

In such a plume simulation study, it is paramount that the performance 

of the nozzles be accurately known for use in data analysis. This fact was 

realized from the outset based on previous experience in testing small nozzles 

in the wind tunnel. Therefore, a concerted effort was maintained to provide 

information from which accurate nozzle performance could be determined. 

Procedures included conducting a complete mechanical inspection of the nozzle 

internal geometry, then calibrating each nozzle by flowing air at various 

levels into a quiescent evacuated chamber while measuring P , Tc, 'c/ 'amb C 

nozzle internal wall pressures, and P 

were also recorded for reference purposes and comparisons with analytical 

predictions. 

plete nozzle calibration data are included in Appendix C. An example of the 

nozzle wall pressure distributions is shown in Figure 19 for the air calibrations 

together with method of characteristics ( MOC) computed distributions. Figure 

20 shows an example of the effect of absolute P values on P /P . As can be 

seen, there are discrepancies between taps at the same station and a general 

trend with varying chamber pressure. 

for air nozzle plume computations from test run results and calibration data: 

Schlieren photos of the plumes amb' 

Individual nozzle measurements are given in Section In and comC cw 

The following procedure was developed 

P /P \ 

C -- -mP +b+A(e] 

P - P \- - 

ex 

41 
WINO TUNNEL DATA 

60 

50 

O G1 (AIR) - GZ (CFq) 

GyG5 (SOLID PROPELLANTS) 

- 

- 

101 

(a) CLASSIC GEOMETRY 

60- 

50 - 

40 - 

30 - 

REPRESENTATIVE TRAJECTORY 

0 SSME 

e SRB 

(b) ET/SRB CLASS 

-. ~. __ - - 

0.5 0.9 1.05 1.2 1.3 1.5 2.0 '35 

NOMINAL FREESTREAM MACH NUMBER, M, 

(c) ORBITER CLASS (d) SRB-ALONE CLASS 

Figure 18. Range of plume sizes. 

42 
110- 

100 

90 

80 PC 

- 

'W 70- 

60 

50 

40 

NOZZLE 4 

GAS 1 

Tc X 530 K (950°R) 

- 

- 

- 

- 

- 

-~ 

,- *-MOC ANALYSIS FOR 

8 = 35.08 deg 

e = 6.507 

Rc/R* = 3.646 

$fa.. . .'..*. EXPERIMENTAL DATA 

FOR P = 1.44 - 12.53 MN/m2 

(209-1819 psi) 

MEAN -f LIMITS 

0.7 0.8 0.9 1 .o 

X/L 

Figure 19. Example of wall pressure distribution 

from nozzle calibrations. 

NOZZLE 4, GAS 1,T, X530 K (950°R) 

D 

TAP 

NO. X/L 

0 000 U 0 44 .721 

0 0 48 .837 

46 .944 

e 

0 

8 688 8 

47 .938 

D 45 .959 

0 

I I. _1 I I I I 

2 4 6 8 10 12 14 MN/m2 

500 1000 1500 2000 psi 

I 8 I I 

pc 

Figure 20. Effect of chamber pressure on wall pressure ratio. 

4 

(de91 

330 

30 

150 

210 

330 

43 
where 

from 

experimental 

data 1 (2) 

P 

P 

C b=-atP M 0 

C 

e 

P P 

,P P P 

e1 C 

ex c 

m=-.- , gradient of - with absolute P 

C 

ex 

P 

C A (2) = increment of - from farthest downstream nozzle tap to 

pW 

the exit plane, as determined from the MOC nozzle solution 

EXIT 

V EXPERIMENTAL: 

DATA POINT -..' 

- 

FROM 

CA L I BRAT ION 

DATA 

X 

Air nozzle performance was then determined from measured 0 

pc'pex c ex 

method has been used in analysis of all air nozzle test data. However, for the 

CF4 and solid propellant data, real gas and two-phase (gas/solid) solutions 

are required. Using the equations of state of Reference 9 (which compare 

favorably with those of Reference 10) and the definition of y = a2/gPV for 

T < 444 K (800"R), theoretical nozzle solutions have produced near identical 

results to the experimental data (Fig. 21). For CF4, calculations were performed using the gas-only MOC computer code of Reference 11 with the CF, 

properties of Reference 12. 

performed using the two-phase MOC computer code of Reference 13. 

calibrated n' 

, P /Pb, and y , using ideal gas MOC plume calculations. This 

c 

For the solid propellant plumes, calculations were 

44 
lot 

70 

60 

50 

pw 40 

- 

pc 

30 

20 

10 

NOZZLE 1A 

GAS 2 

- 

- 

- 

- 

- 

- 

- 

"'..MOC ANALYSIS FOR 

8, = 14.92 deg 

E = 8.398 40 

PW *.. R,/Ri= 6.073 

P,= 6.89 MN/m2 (1000 psi 

+., T, = 533 K (960'R) 

*.EXPERIMENTAL DATA FOR 

20 

P,= 6.84 MNh2 (992 psi) 

Ti = 538 K (969'R) 

NOZZLE 16 

GAS 3 

a-..--EXPERIMENTAL DATA FOR 

P, = 2.94 MN/m2 (426 psi) 

"'TWO-PHASE MOC 

ANALYSIS FOR 

8 = 14.83 deg 

E = 7.865 

RJR, = 3.629 

P, = 2.76 MN/m2 (400 psi) 

I - -. 6 . I 

1 .o 

I 

0 0.2 0.4 0.6 0.8 

XIL 

(b) SOLID PROPELLANT EXHAUST 

Figure 21. Comparison of analysis and experiment 

for nonair cases. 

45 
D. Space Shuttle Base Pressure Simulation Procedure 

A preliminary analysis of the present data has yielded a simulation technique that has been used for Space Shuttle development wind tunnel tests. 

Although these procedures are less than perfect, an outline is presented to 

provide insight into the development of the present "plume simulation" wind 

tunnel tests. 

The simulation parameter used in the Space Shuttle development program 

is [d .y = jyjn]pROTO, where n was determined empirically from 

correlation of gases and nozzle geometry for fixed-body configurations. HowJ j MODEL 

ever, this parameter does not allow explicit determination of base pressure 

(P ) . Therefore, an implicit procedure was developed as follows. Figure 22 b 

shows a typical simulation plot. The illustrated curve of possible prototype 

base pressure as a function of simulation parameter can be computed (knowing 

prototype engine characteristics) by use of a nozzle flow analysis (i. e. , Reference 11 or 13) for a range of base pressures that might be expected. This 

curve is established for a given trajectory at a set of Ma , Pa , and engine 

thrust level values. Next, a wind tunnel test is conducted at trajectory M 

while measurements are obtained at varying P levels (P directly varies 6 

and correspondingly P ) . The experimental P levels are chosen to cause 

[ j 'j"] MODEL 

a, 

C C j 

b C 

values to fall within the prototype range of interest. In the data 

BASE 

I 

\ 

DATA 

SIMULATION PARAMETER, SUCH AS 6 y n 

(PC 1 

Figure 22. Basic simulation procedure. 

46 
r 1 

analysis stage, the model P versus is plotted on the same graph b - with the prototype possibility curve. The intersection of these two curves is 

the condition which simultaneously satisfies both prototype possibilities and 

model actualities, and thus [ 6 j,jl .y MODEL [bjyjn]PROTO for the given conditions. The previously described basic process is for a single-body configuration with either single or multiple nozzles. However, for the Space Shuttle with 

its multibody configuration, the process becomes more complicated, as the 

plumes of one body interact with the plume effect on an adjacent body. If mutual 

interaction exists between adjacent bases (e. g., between the SRB and Orbiter 

of the Space Shuttle), then tests must be conducted for a matrix of P /P for 

the two engine systems. 

curve sets that are required for the mutual interaction problem. 

successively chosen along each possibility curve until the values of simulation 

parameter "Aff and "B" are matched. 

value of P for each body is produced. 

ca 

Figure 23 illustrates the pair of "data/possibility" 

Points are 

Then, at the two match points the design 

b 

From the previous discussion it can be seen possible to produce a 

simulation process which would be difficult to apply, in terms of data analysis 

or amounts of test time required to produce a design data point. It may be that 

other approaches to the simulation process could provide a better data match 

and/or simpler application processes, but that is beyond the scope of this 

report . 

47 
TEST 

I DATA SIMULATION PARAMETER 

BASE PRESSURE 

ON BODY 1 

DESIGN 

VALUE 1.L PROTOTYPE POSSlE 

- -_ 

"A" 

SIMULATION PARAMETER ON BODY 1 

(P, OF BODY 1) 

1 TIES OF BODY 1 

ARAMETER ..-.-m. by SlMULA'i IUN t 

ON BODY 1 

(P, OF BODY 1) 

TEST 

DATA BASE PRESSURE 

ON BODY 2 

I " \ PROTOTYPE POSSIBILITIES OF BODY 2 

"B" 

SIMULATION PARAMETER ON BODY 2 

(P, OF BODY 2) 

Figure 23. Multiple body simulation procedure. 

48 
REFERENCES 

1. Lott, R. A., Baker, L. R., Sims, W. H., and McCanna, R. W.: 

Power-on Base Pressure for Space Shuttle Launch Configurations. 

LMSC-HREC D225152, lhckheed Missiles and Space Company, 1971. 

2. Goethert, B. H., and Barnes, L. T. : Some Studies of the Flow Pattern 

at the Base of Missiles with Rocket Exhaust Jets. AEDC-TR-58-12, 

Arnold Engineering Development Center, 1960. 

3. Simon, Erwin H. : The George C. Marshall Space Flight Center's 

14 x 14-Inch Trisonic Wind Tunnel Technical Handbook. 

64624, 1971. 

NASA TM X4. Pirello, C. J., Hardin, R. D., Heckart, M. V. and Brown, K. R.: 

An Inventory of Aeronautical Ground Research Facilities. Vol. I. 

Wind Tunnels. NASA CR-1874, 1971. 

5. Anon. : Test Facilities Handbook. Arnold Engineering Development 

Center, 1974. 

6. Baran, W. J. : Development of a Miniature Solid Propellant Rocket 

Motor for Use in Plume Simulation Studies. Report AA-4018-W-10, 

Calspan Corporation, 1974. 

7. Hair, Leroy M. : Test Data Report for Solid Propellant Plume Aerodynamics Test Program in MSFC 14 x 14 Inch Trisonic Wind Tunnel. 

RTR 016-1, REMTECH, Inca, 1974. 

8. Hendershot, K. C., Drzewiecki, R. F., and Lemoine, P. L.: Development of a Hot Rocket Subscale Space Shuttle Model for Base Flow Studies. 

AIAA Paper 74-1147, October 1974. 

9. Jones, Robert A., and Hunt, James L. (With Appendix A by James L. 

Hunt, Kathryn A. Smith, and Robert B. Reynolds, and Appendix B by 

James L. Hunt and Lillian R. Boney): Use of Tetrafluoromethane to 

Simulate Real-Gas Effects on the Hypersonic Aerodynamics of Blunt 

Vehicles. NASA TR R-312, 1969. 

49 

ILL .. . . . . . . . . . . 
. . 

REFERENCES (Concluded) 

10. Talcott, Noel A., Jr. : Thermodynamic Properties of Gaseous Flourocarbons and Isentropic Equilibrium Expansion of Two Binary Mixtures of 

Flourocarbons and Argon. NASA TN D-8405, 1977. 

11. Prozan, R. J. : Solution of Non-Isoenergetic Supersonic Flows by 

Method of Characteristics. LMSC-HREC D162220, Lockheed Missiles 

and Space Company, 1971. 

12. Tevepaugh, J. A., Penny, M. M., and Baker, L. R.: Input Guide for 

Computer Program to Generate Thermodynamic Data for Air and Freon 

( CF4). LMSC-HREC TM D390169, Lockheed Missiles and Space 

Company, 1974. 

13. Penny, M. M., Smith, S. D., Anderson, P. G., Sulyma, P. R., and 

Pearson, M. L. : Supersonic Flow of Chemically Reacting Gas Particle 

Mixtures. Vol. II. RAMP, A Computer Code for Analysis of Chemically 

Reacting Gas-Particle Flows. LMSC-HREC TR D496 555-II, Lockheed 

Missiles and Space Company, 1976. 

50 
APPENDIX A 

DATA OF PRIMARY INTEREST 

The specific values of model chamber conditions, tunnel freestream 

parameters, and the basic (single) base pressure data for each valid wind-on 

run of the seven selected tests are presented in this appendix. The location on 

the various models of these pressures is shown in the following sketch: 

BASE PRESSURE (TYPICAL) 

"A" 

"C" 

AV ER AG ED 

NOZZLE 

EX IT AREA 

(TYPICAL) 

FOR SRB 

CLASSIC ORBITER ETISRB SR B-ALONE 

GEOMETRY CLASS CLASS CLASS 

(ALL VIEWS LOOKING UPSTREAM) 

Exact locations of the base pressure taps are shown in Table 6 of text. For the 

Orbiter class, the three nozzles were denoted "A", "BT7, and "C". The top 

nozzle was denoted "Ar7, with "B" and trC77 proceeding clockwise as viewed looking 

upstream. For the ET/SRB class in Test 7, nozzles denoted 77Av' were mounted 

on the left-hand side and nozzles denoted "Bee on the right-hand side. In Test 8, 

the identity of which nozzle had been mounted.on which side was not resolved. 

Data are given in Tables A-1 through A-4 for the four geometry types sketched. 

Within each table, data are grouped first by test number, then by gas and nozzle 

number. 

values of A/A, and 8 ; exact values of nozzle geometry are shown in Table 3 of 

text. Beneath each subtitle the data are grouped by nominal Mach number. 

Within a Mach number group, data are presented in order of increasing P /P . 

Jet-off runs are presented first where availalbe. These tabulated data are 

plotted in Figures 13 through 17 of text. 

For each group, a subtitle is provided which includes nozzle design 

n 

cm 

The complete sets of base, body, and nozzle pressures for each run are 

presented in Appendix B. The sequence of presentation of runs in Appendix B 

is identical to that of this appendix. An example is given of obtaining these 

51 
data for a particular case: Run 356/0 of Test 1. This case is the second one 

presented in this appendix within the classic geometry type (see Table A-I) . Thus, the desired base and body data will be found at the second case in the 

classic geometry portion of the base and body section of Appendix B (Table 

B-1) . At that location the following values of Pb/Pm are found: 

TALLE 6-10 - RASE AND BODY SbRFkCE PAESSURE RATIOS (F 

.O? 

1.12 

1.30 

1.84 

2.23 

2.56 

9 RUN ?St/O 

os54 

0947 or56 

.875 .GO6 

. 349 

. 966 

0073 

.?a2 1.013 

. 992 

e332 1.019 

991 

0972 

0956 1.044 

.969 

-- 

1 

Correspondingly, the desired nozzle wall pressure data will be found in 

the classic geometry portion of the nozzle section of Appendix B (Table B-5). 

Because jet-off runs are not included in the nozzle section, the desired nozzle 

data will be found at the ith position: i = j - n , where the Appendix A case is off 

at the jth position and n is the number of jet-off runs up to position j. In this off 

example, j = 2 and n 

Tap No. 47 is found to be 26.45. 

= 1 so i = 1. At that location, the value of P /P for 

off cm 

52 
TABLE A-1. TEST DATA OF PRIMARY INTEREST - CLASSIC GEOMETRY 

.. . 

ID. F R E E.S T R f AM 

RUN/ 1 M P TT RE/L 

RERUN (PSFA)(~R)(M/FT) 

TEST 

372/0 

356/0 

323/0 

55710 

354/0 

322/0 

353/0 

358/O 

321 /O 

359/0 

352/0 

320/0 

373/0 

363/0 

316/0 

362/0 

349/0 

317/0 

350/0 

329/0 

361 /O 

32P/O 

31E/O 

351/0 

360/0 

319/0 

374/@ 

347/0 

364/0 

31 5/0 

365/0 

346/0 

314/0 

345L 0 

61 1 1 --- 

.8a9 1553 567 5.0 

0888 1553 563 5.0 

0903 152E 562 5.1 

0901 1531 564 5.0 

0306 1524 561 5.1 

0908 1520 562 5.1 

-905 1525 561 5.1 

e001 1532 562 5.1 

,910 1516 563 5.1 

0902 1530 562 5.1 

,907 1523 561 5.1 

.9C9 1517 563 5.1 

1.191 1078 562 5.4 

1.194 1C76 563 5.4 

1.208 1059 563 5.4 

1.194 1078 562 5.4 

1.206 1062 561 5.4 

1.206 1061 563 5.L 

1.203 1066 561 5.4 

1.189 1086 562 5.4 

1.211 1055 562 5.4 

1.180 1069 562 5.4 

1.207 1060 563 5.6 

1.203 1066 562 5.4 

1.208 I058 561 5.4 

1.207 1060 562 5.4 

1.459 749 564 5.2 

1.459 750 563 5.2 

1.466 741 566 5.2 

1.459 749 563 5.2 

1.479 728 561 5.2 

1.477 731 563 502 

-1!4Uz -725 540 se3 

1.484 723 566 5.2 

CHAM~ER- 

(PSIA) (OR) 

PC TC 

3 (AIR, A 

0 0 

466 358 

472 518 

837 966 

965 702 

952 510 

1217 708 

1234 9P9 

1422 510 

1501 953 

1584 712 

1740 504 

0 0 

451 950 

519 571 

354 9t?4 

e56 704 

1054 511 

1211 711 

1251 883 

1224 1004 

1502 890 

1545 507 

1616' 708 

1619 1021 

1808 506 

0 0 

461 737 

46C 971 

510 512 

847 961 

857 730 

953 510 

1202 11.7 

BASE 

PBiP PC/PB PC/P 

e846 

0841 

0933 

.939 

.967 

0994 

0995 

1.047 

1.025 

1.037 

1.087 

-913 

0709 

0741 

.a64 

0573 

.967 

0979 

0993 

0994 

1 .c57 

7.1.8 

1.074 

1.092 

1.207 

0962 

.766 

.77c 

0601 

-924 

.919 

0985 

1 *.Ill2 

51 43 

53 44 

84 79 

87 82 

93 90 

116 115 

117 116 

129 135 

137 141 

144 950 

152 166 

0 0 

85 60 

95 71 

132 114 

11'3 116 

148 143 

167 16L 

147 166 

168 167 

18€! 199 

1E4 210 

203 21P 

202 220 

204 246 

0 0 

116 59 

116 89 

122 98 

162 169 

184 17@ 

197 994 

236 23 9 

53 
TABLE A-1 . ( Continued) 

33510 

ID* 

RUN/ 

RERUN 

366/0 

313/0 

344/0 

36710 

31210 

37510 

37610 

340/0 

108/1 

37010 

341 /@ 

379/0 

33710 

?09/0 

342/0 

38010 

31 010 

343/0 

381 /G 

311/0 

37712 

3.480 175 ____ 569 lO*-l-- 

GI, 

- 

_-~~ FREESTREAM 

M P TT RE/L1.L76 732 563 5.2 

1.47e 729 560 5.3 

lmLP7 720 567 5.2 

lm47e 730 563 5.2 

3.L79 175 572 1O.C 

?.480 175 563 10.3 

3.460 175 563 10.3 

3.460 175 563 10.3 

"480 175 565 10.2 

3.460 175 563 10.3 

3e4EO 175 563 10.3 

3.480 175 569 10.1 

3.480 175 565 10.2 

3.480 175 563 10.3 

3.460 175 563 10.3 

3.480 175 564 10.2 

3.480 175 563 10.3 

3.480 175 C63 10.3 

3.480 175 56C 10.2 

3.460 175 568 10.1 

c H_AII?BER - PC TC 

__ (PSIA)(OR) 

1244 990 

1431 512 

1593 710 

1595 993 

17G2 508 

0 0 

429 943 

431 675 

513 727 

550 566 

804 686 

864 861 

990 545 

1087 502 

1134 688 

1220 859 

1443 547 

1504 700 

1544 555 

1555 lOOi 

1556 577 

0 0 

374 8C8 

360 745 

394 592 

407 677 

411 660 

747 901 

750 836 

766 1020 

753 702 

851 760 

1087 757' 

1509 a44 

!t (AIR, A 

B_A.S_E___ 

PB/P PC/PB PC/P 

I___ 

1.035 241 250 

1.131 249 262 

1eOe8 289 315 

1.104 289 319 

1.216 276 ?36 

.9e1 0 0 

.674 524 353 

e665 5?4 355 

a955 420 427 

.836 838 70C 

me63 824 711 

.&33 854 712 

.992 622 e15 

1.090 821 895 

e970 963 934 

0963 1042 1004 

1.166 1C19 118F 

1.094 1132 ?23E 

1.022 1216 124: 

1.212 1G50 1272 

1.022 1253 1280 

.940 0 C 

a776 45 35 

.775 46 36 

.767 48 37 

.76a 50 3p 

.775 50 39 

0822 95 7c 

et27 84 70 

.e20 e8 72 

.a21 87 72 

.PL2 94 79 

.le____ 114 101 

54 
 

I D. 

R U N /-- 

RERUN 

117/0 

197/0 

157/0 

19210 

198/0 

151/0 

118/0 

191/0 

15P/O 

150/0 

IFC/O 

15C/O 

’119/0 

19Q/O 

216/0 

l45/0 

164/C 

204/0 

12410 

195/0 

123/0 

203/0 

163/0 

146/0 

166/0 

162/0 

147/0 

122/0 

202/c 

137/0 

961/0 

201 /o 

149/0 

121/0 

9 6&/.0 

TABLE A-1. 

FRFESTREAM 

M P TT RE/L 

(PSFA) (OR) (MIFT) 

.PO9 1534 561 5.1 

0899 1535 562 5.1 

0387 1555 560 5.0 

a902 1530 560 5.1 

a005 1524 562 5.1 

.E99 1535 561 5.1 

.?93 1544 500 5.1 

e902 1530 561 5.1 

0894 1542 561 5.1 

a901 1525 561 5.1 

OR98 1537 560 5.1 

mP99 1535 561 5.1 

0905 1525 567 5.0 

0906 1523 562 5.1 

1.199 1070 560 5.4 

1.201 1067 560 5.4 

1.139 1071 562 5.4 

1.195 1075 502 5.4 

1.198 1071 567 5.3 

1.196 1075 560 5.4 

1.204 1063 56’ 5.3 

1.19e 1073 562 5.L 

1.300 1069 562 5.4 

1.200 1070 559 5.4 

1.203 1065 560 5.4 

1.195 1076 562 5.4 

1.205 1063 567 5.3 

1.2G6 1060 559 5.4 

1.2CO 1070 562 5.4 

1.2C7 1060 559 5.4 

1.193 1079 562 5.4 

1.201 1069 561 5.4 

1.200 1069 559 5.4 

1.204 1063 567 5.3 

1.207 1060 559 5.4 

(Continued) 

CHAMBER 

PC TC 

(PSIA) (OR) 

1123 6E6 

ll2E 1032 

1153 848 

1162 $22 

1413 1041 

1426 760 

1484 684 

1477 926 

1518 856 

1741 763 

1839 943 

1836 tic6 

1820 666 

le42 1050 

0 0 

377 737 

333 e74 

386 993 

367 672 

392 677 

762 676 

788 1022 

796 341 

80C 756 

801 905 

1113 75E 

1126 675 

1144 10‘5 

1144 918 

1430 849 

1457 1031 

1457 764 

1467 670 

1485 9c7- 

1067 aL3 

0885 119 105 

0887 119 106 

0892 120 107 

.E56 124 109 

m928 144 134 

e928 144 134 

0934 148 138 

0929 150 130 

0940 151 142 

0962 170 164 

0968 17e 172 

05171 177 177 

0931 176 172 

0973 179 174 

0744 0 c 

e558 Ql 51 

.564 91 51 

0555 92 52 

.571 91 52 

0570 92 53 

0712 145 103 

0705 150 106 

0716 150 107 

0712 151 lop 

,717 151 10n 

0787 1P5 145 

0792 191 151 

.806 le9 152 

0799 193 154 

.E05 193 155 

.e67 220 191 

.e62 228 19C 

.E64 227 196 

0682 225 159 

- ._ e876 . ~ ~ 230 202 

55 

-I I.. ... .. ~- 
TABLE A-1. ( Continued) 

ID. . 

RUN/ 

R E R U N--. 

1 2.0 / 0 

149/0 

200/0 

160/0 

189/0 

205/0 

165/0 

125/0 

206/0 

166/0 

126/0 

207/0 

167/0 

127/0 

208/0 

168/0 

128/0 

20910 

129/0 

169/0 

21R/O 

134/0 

210/0 

133/0 

211/0 

132/0 

21212 

131/3 

213/0 

214/0 

130/0 

709/0 

702/0 

712/0 

TEST 

- E E s *-.€ * M- ~ - -- 

i . i 98 ToT2-567 5 . 3 

__ __ -.. ._ - 

R P TT RE/L 

. ...- . - . ( P S F A 1 ( R- ). ( M-/F T : 

1.195 1076 559 5.4 

1.198 1073 562 5.4 

1.193 1079 562 5.4 

1.201 1067 559 5.4 

1.437 774 563 5.3 

1.462 746 562 5.2 

1.467 741 561 5.3 

1.471 737 564 5.2 

1.461 747 562 5.2 

1.470 736 561 5.3 

1.445 764 562 5.3 

1.476 732 562 5.2 

1.481 726 562 5.2 

1.455 754 563 5.2 

1.482 725 563 5.2 

1.482 725 561 5.2 

1.456 752 563 5.2 

1.488 719 562 5.2 

1.487 720 563 5.2 

3.480 175 560 10.4 

3.480 175 565 10.2 

3.480 175 561 10.3 

3.480 175 571 10.1 

3.480 175 561 10.3 

3.480 175 565 10.2 

3.480 175 562 10.3 

3.480 175 571 10.1 

3.480 175 561 10.3 

3.480 175 561 10.3 

175 565 10.2 I,_ks_P -..~~.~_____ 

L --- ---I GI 

5.480 175 570 10.1 

3.480 675 569 10.1 

3 w. 4 8 0. - 1 7 5 563 _?O& 

__~._ ~ -_- 

CHAMBER 

PC TC 

__ (PSIAI(OR1 

1814 667 

.~ -~ 

1827 770 

1832 1034 

1841 855 

1864 934 

335 991 

407 835 

458 707 

754 1016 

763 847 

820 706 

1081 1045 

1144 852 

1177 685 

1492 1047 

1553 861 

1580 696 

1863 1058 

1825 711 

1858 870 

0 0 

381 704 

430 995 

773 737 

804 1023 

1157 7C2 

1159 1050 

1479 724 

1522 1020 

1831 1019 

1851 -~ __ 730 

LLAIRLA 

435 617 

441 738 

537 253- 

__ -- 

wP52 

w933 

w937 

w940 

w948 

w 576 

0633 

w653 

0754 

w769 

w778 

w866 

we67 

0907 

0948 

0953 

0968 

0995 

1 .ooo 

.le2 

0558 

0595 

. 71 8 

0725 

w822 

.a20 

.a69 

.907 

0911 

,967 

2 56 244- 

262 245 

262 246 

261 246 

265 252 

108 62 

124 79 

136 89 

195 147 

191 147 

206 160 

249 204 

260 225 

269 233 

314 285 

326 310 

329 314 

369 35€! 

368 366 

372 372 

0 0 

562 313 

606 354 

886 036 

913 662 

1157 951 

1098 954 

1377 1254 

1560 1508 

1341 1216 

w990 1540 1525 

S=3.5, 35 DEC.) .-_ 

w939 3e2 358 

w928 392 364 

2984- 445 43e 

56 
TABLE A-1. ( Continued) 

ID. 

PUN/ 

RERUN 

710/0 

703/0 

701 /O 

704/0 

715/0 

707/0 

713/0 

714/0 

706/0 

711/0 

705/0 

708io 

TEST 

53 o 

54210 

541 /O 

519/0 

540/0 

55010 

518/0 

539/0 

53810 

552/0 

533/0 

534/0 

53510 

52010 

517/0 

549/0 

53610 

537/0 

55310 

53210 

531 /O 

51610 

-~ FREESTREAM 

c P TT RE/L 

(PSFA)(~R)(M/FT) 

3.480 175 570 10.1 

3.480 175 561 10.3 

3.480 175 568 10.1 

3.480 175 563 10.3 

7.480 175 563 10.2 

3.460 175 561 10.3 

3.480 175 570 10.1 

3.4eO 175 562 10.3 

3,480 175 563 10.3 

3.480 175 569 90.1 

3.480 175 562 10.3 

3.480 175 568 10.1 

62 9 1 --- 

,898 1537 557 5.1 

0899 1535 559 5.1 

0894 1544 559 5.1 

e904 1526 557 5.1 

0904 1526 560 5.1 

-893 1543 561 5.1 

0909 1518 558 5.1 

0906 1523 560 5.1 

0901 1530 560 5.1 

1.195, 1'076 561 5.4 

1.195 1077 560 5.4 

1.202 1066 550 5.4 

1.204 1063 559 5.4 

1.204 1063 557 5.4 

1.213 1050 559 5.4 

1.204 1064 561 5.4 

1.198 1072 560 5.4 

1.202 1065 560 5.4 

1.456 751 557 5.3 

1.444 766 561 5.3 

1,459 749 561 5.3 

1.468 739 55F 5.3 

CHAKBER 

PC TC 

(PSIA) (OR) 

728 841 

857 985 

863 734 

973 511 

1243 691 

12.48 997 

1258 854 

1373 502 

1445 523 

1558 665 

1567 989 

1587 695 

1A (CF4, A 

0 0 

481 673 

854 561 

1120 775 

1189 867 

1224 1002 

1221 695 

1569 884 

1877 886 

G 0 

510 245 

855 862 

866 865 

1134 770 

1216 693 

1242 997 

1566 6.58 

1931 890 

0 0 

496 610 

851 860 

1123 700 

__-____~ BASE 

PB/P PC/PB PC/P 

1.145 524 600 

1.363 518 706 

1.204 590 711 

1.361 589 801 

1.401 730 1023 

1.569 655 1028 

1.417 731 1036 

1.673 675 112P 

1.717 693 1189 

1.670 766 9283 

1.765 731 1291 

1.554 640 1306 

.c37 0 0 

A=8.09 15 DEC.) 

.&23 55 45 

0827 96 8C 

0857 123 106 

0867 129 112 

et87 129 114 

0864 134 116 

0913 162 148 

0944 187 177 

0753 0 0 

*568 120 68 

e667 173 115 

0471 175 117 

0722 213 154 

0725 230 167 

0772 218 16P 

e807 261 210 

0868 301 261 

0710 0 0 

0600 155 97 

0718 228 164 

e753 290 219 

57 
ID. 

RUN/ 

RERUN. 

521/0 

530/0 

548/0 

529/0 

528/0 

55410 

523/1 

52410 

52210 

515/0 

546/0 

547/0 

525/0 

526/0 

868 5229 

911 5229 

1886 5229 

1860 5229 

0 0 

0 0 

0 0 

0 0 

417 5229 

1146 5229 

1850 5229 

1226 5229 

.- 1 36 3 .. .52?-9. 

TABLE A-1. 

8 

21 

21 

FREESTREAM 

Ft P TT RE/L 

1.468 739 55%- 5.3 

(PSFA)(ORI(M/FT) 

1.467 740 561 5.2 

1.473 733 560 5.3 

1.482 725 561 5.2 

1.484 722 561 5.2 

3.480 175 561 10.3 

3.48.0 175 559 10.4 

3.480 175 559 10.4 

3.480 175 559 10.4 

3.480 175 559 10.4 

3.480 175 559 10.4 

3.480 175 562 10.3 

3.480 175 559 10.4 

3.480 175 559 10.4 

483 5229 

w898 430 555 1.4 0 

0500 426 550 

w900 430 555 1.4 484 5229 

( Continued) 

.. 

CHAMBERPC TC 

(PSIA) (OR-) 

1145 768 

1146 866 

1255 1003 

!550 877 

0 0 

418 815 

794 913 

1151 754 

1165 703 

1190 907 

1217 1026 

1239 841 

1555 844 

1850 a77 

1-817 633 

133/0 

33/0 

35/0 

34/0 

49/0 

49/1 

49/2 

50/0 

136/0 

137/0 

138/0 

?37/0 

?38/0 ~- - 

1.430 1205 549 8.4 

1.430 1209 551 8.4 

1.430 1217 548 8.5 

1.440 1201 550 8.5 

3.480 194 551 11.8 

3.L80 194 561 11.5 

3.480 194 561 11.5 

3.479 49 549 3.0 

3.480 194 548 11.9 

3.480 194 54E! 11.9 

3.480 194 548 11.9 

3.480 49 548 3.0 

3.480 49 543 . 3.0 _I 

- 

-- 632 N ?.e . --(. ?%T .A --- TEST 6 

8 .500 429 550 .7 I 0 0 

BASEPB/P PC/PB PC/P 

w769 290 223 

w788 283 223 

w629 297 246 

0869 355 30e 

w919 401 369 

w262 0 0 

0478 720 344 

w640 1022 654 

w677 1401 94E 

e661 1449 958 

e747 1313 980 

e792 1265 1003 

w728 1401 1020 

w810 1582 7281 

w651 1758 1496 

4=8.0,!5 DEC-w) 

w511 99 50 

e624 166 104 

w648 167 100 

0763 293 223 

w764 292 223 

w282 0 0 

.313 0 0 

w281 0 0 

w435 0 0 

w505 612 309 

e708 1199 849 

w812 16E5 1370 

1.536 2370 3640 

-1.626 2472 4030 

w987 0 0 

w965 168 163 

w927 0 0 

a918 177 ~- 162. 

Az8.0, 15 DEG.) 

58 
-- 

TABLE A-1. ( Continued) 

ID. FREESTREAM c HA MB E R-- 

RUN/ 1 M P TT RE/L 1 PC TC 

RERUN (PSFA) (OR) (IM/FY) (PSIA) (OR) 

TEST'6 --- G39NlE ( 2%. A 

5 I .499 863 554 1.4 I 0 0 

5 

18 

15 

1512 

15 

a500 863 554 1.4 

.E98 862 561 2.8 

e900 862 561 2.9 

1.200 357 576 4.2 

1.200 857 578 4.2 

463 5229 

0 0 

431 5229 

0 0 

442 5229 

47/0 1.460 1164 543 8.5 I 0 0 

47/1 

47/2 

72/0 

48/0 

48/1 

48/2 

161/0 

261 /O ~~ 

TEST 

11 

15 

zt/o 

2810 

29/0 

41 /2 

9 /1 

210 

3/0 

-. 

TEST 

4/2 

TEST 

24 

24 

37 

43 

43 

1.466 1153 542 8.6 

1.460 1164 541 8.6 

5.430 1217 556 8.3 

3.480 194 560 11.5 

3.480 194 559 11.5 

3.480 194 559 11.5 

3.480 194 562 51.5 

0 0 

0 0 

403 5229 

0 0 

0 0 

0 0 

407 5229 

3.479 49 547 3.0 I 421 5229 

0 0 

6 --- G3.NZB ( 2%~ A 

0500 2257 564 3.6 

m500 2259 564 3.6 

2 G4? 

1.430 1215 556 8.3 

1.420 1236 559 8.3 

1.4GO 1272 548 8.6 

3.480 194 557 11.6 

3.480 194 564 15.4 

3.480 194 561 11.5 

3.480 194 563 55.4 

3.480 194 558 ._ 11.6 

6 --_ 64. 

0500 859 550 1.4 

a500 858 550 1.4 

0500 429 554 07 

0903 576 554 1.9 

0900 576 554 1.9- 

544 5229 

16- (16% A 

397 6203 

821 6203 

1411 6203 

0 0 

349 6203 

791 6203 

1331 6203 

-_ 1849 6203 

1D (16%; A 

0 0 

363 6203 

295 6203 

0 0 

351 6203 

@ASE 

PB/P PC/PB PC/P 

0952 e1 77 

a922 0 0 

0847 85 72 

807 0 0 

0642 116 74 

0737 0 0 

0705 0 0 

.72a 0 0 

a619 77 48 

0364 0 0 

-341 0 0 

0318 0 0 

0783 385 301 

1.523 812 1237 

a976 0 0 

A=4.0, 15 DEG.) 

A=4.0, 15 DEC.) 

0949 37 35 

e515 91 47 

A=8.0, 15 DEG.) 

e609 157 96 

0696 229 160 

0201 0 0 

0597 433 259 

e824 711 586 

1.005 981 986 

1.032 1327 1370 

0979 0 0 

-- 

A=8.0, 15 DEG.) 

0945 64 61 

0967 102 99 

0919 0 0 

0557 102 8f! 

59 
TABLE A-1 . ( Concluded) 

I_- 

FREESTREAM ------CHARB:;- 

P TT RE/L 

1.201 858 577 4.2 

(PSFA) (OR) (RIFT) 

._ 

PC i pB/p PC/PB e~s~ PC/P 

(PSIA) (OR) - 

0 0 I .807 0 0 

1-1.200 858 577 4.2 I 373 6203 I .626 100 63 

TEST 6 G49N1E (16% A/A=8.O, 15 -DEG.) 

.500-574 ,551 09 I 0 0 I .983 0 0 

1 

27 0500 574 551 09 351 6203 0956 92 88 

34 .897 a59 558 2.p 0 0 0922 0 0 

34 0900 859 558 2.9 3W8 6283 e845 61 52 

62 0900 426 553 1.4 SF6 6203 0980 206 201 

50 1.200 587 561 3.0 0 0 0814 0 0 

50 1.200 5_87 561 3.0 343 6203 0680 124 84 

47/0 1.460 1164 543 8.5 0 0 0737 0 0 

47/1 1.466 1153 542 &e6 0 0 0705 0 0 

47/2 1,460 1164 541 8.6 0 0 e728 0 0 

70/0 1.410 1242 557 8.3 474 6203 0699 79 55 

7110 1.380 1301 555 8.4 855 6203 0811 117 95 

48/0 3.480 194 560 11.5 0 0 0364 0 0 

45/1 3.480 194 559 11.5 0 0 0341 0 0 

4812 3.460 194 559 11.5 0 0 0318 0 0 

62/2 3.480 194 556 ?!e6 466 6203 1.007 343 345 

163/0 3.480 194 561 11.5 878 6203 1.187 548 650 

TEST 6 - --_ G49N28 (16% A/A=4.09 IS DEG.) 

31 0498 2264 567 3.6 0 0 e976 0 0 

31 o5OC 2264 567 3.6 402 6203 .94a 27 26 

66 ,500 2254 564 3.6 470 6203 e961 31 30 

40 ,500 424 551 07 544 6203 1.024 181 185 

47 .e98 1764 574 5.7 0 0 e909 0 0 

47 0900 1764 574 5.7 425 6203 e904 30 35 

53 !.200 ?I11 589 5.3 0 0 0802 0 0 

53 1.200 1117 589 5.3 , 433 6203 0782 72 56 

TEST 2 --- G49N2A (16%9 A/A=4.0, 15 DEG.) 

60 
TABLE A-2. TEST DATA OF PRIMARY INTEREST - ORBITER CLASS 

ID. I FREESTREAM I CHAMBER 

M P 

?ERUN 

TEST 3 (EDGE TAP) -- G1 9 

220/0 

?15/0 

?10/0 

209/0 

204/0 

219/0 

216/0 

223/0 

214/0 

211/0 

20310 

205/0 

218/0 

217/0 

22410 

21311 

212/0 

222/0 

221 /o 

206/0 

195/0 

194/0 

20710 

196/0 

199/0 

198/0 

197/0 

201/0 

200/0 

203/0 

202/0 

TESl 

0500 2186 560 305 

0505 2178 560 3.6 

DL98 2188 560 305 

0500 2185 560 3.5 

0504 2182 560 3.6 

0898 1536 560 5.1 

0904 1525 560 5.1 

0898 1538 560 5.1 

,e99 1535 540 5.1 

0899 1534 560 5.1 

0895 1541 560 5.1 

0895 1541 560 5.1 

1.205 1063 560 5.4 

1.198 1072 560 5.4 

1.204 1064 560 5.4 

10201 1068 560 5.4 

1.197 1073 560 504 

10202 1066 560 504 

10201 1067 560 504 

1.690 797 560 5.8 

1.515 768 560 5.8 

1.497 788 560 5.8 

1.488 799 560 508 

1.490 796 560 508 

lo494 792 544 600 

1.692 794 560 5.8 

1.496 789 560 5.8 

1.494 792 560 506 

1.504 780 560 508 

1.499 786 560 5.8 

1.512 772 560 508 

3 (EDGE-TAP) -- G 1, 

.501 2183-3-60 3.5 

125/o 1 I-0 I .5052180 560 3.6 

51 (AIR, A 

0 0 

256 911 

480 895 

992 903 

1479 895 

0 0 

179 892 

216 912 

254 906 

992 880 

1475 894 

0 0 

125 891 

169 903 

256 904 

502 899 

991 893 

1499 696 

0 0 

88 657 

85 363 

105 836 

250 657 

257 857 

500 397 

513 667 

999 668 

987 921 

1499 917 

1495 650 

32 (AIR; / 

0 0 

248 909 

495 a97 

BASE 

PB/P PC/PR PC/P 

\=5 03 9 CONTOURED) 

0980 0 0 

0931 

0932 

0918 

0920 

e927 

0833 

.840 

0835 

0783 

0783 

0825 

0750 

0574 

0523 

041 5 

0487 

0596 

0659 

0713 

0492 

0526 

0458 

0387 

0396 

0513 

51 6 

0619 

0621 

e684 

18 17 

34 32 

71 65 

106 98 

0 0 

20 17 

24 20 

29 24 

59 46 

118 93 

167 138 

0 0 

29 17 

44 23 

83 34 

138 67 

225 134 

307 202 

0 0 

34 16 

30 16 

39 19 

117 45 

118 47 

177 91 

181 94 

293 182 

293 182 

402 275 

. -~. 0686 407 279 

0978 0 0 

A=4009 IO DEGo) 

,928 18 16 

61 
TABLE A-2. (Continued) 

ID. 

RUN/ 

RERUN 

114/0 

115/0 

120/0 

136/0 

130/0 

137/0 

131/0 

12610 

111/0 

124/0 

12210 

112/0 

11610 

119/0 

135/0 

128/1 

132/0 

127/0 

110/1 

109/2 

123/0 

113/0 

117/0 

118/0 

134/0 

129/0 

139/1 

!33/0 

150/0 

148/0 

149/0 

146/0 

145/1 

144/1 

13810 

.- 

F R E ESTR EAM. 

M P TT RE/L 

.501 2r82 560 3.5 

-- (PSFA)(~R)(M/FT) 

e499 2187 560 305 

0502 2184 560 3.5 

o500 2187 569 3.5 

0502 2184 560 3.6 

0505 2181 560 3.6 

0506 2180 575 305 

0899 1534 560 5.1 

e900 1532 560 5.1 

0399 1537 560 5.1 

0904 1528 560 5.1 

,903 1527 560 5.1 

e906 1523 560 5.1 

0906 1523 560 5.1 

0900 1535 569 5.0 

a896 1541 560 501 

.QOO 1535 575 4.9 

.900 1533 560 5.1 

1.199 1072 560 504 

1.197 1073 560 504 

1.199 1071 560 5.4 

1.202 1067 560 5.4 

1.202 1066 560 5.4 

1.198 1072 560 5.4 

1.201 1069 560 5.4 

1.190 1084 569 5.3 

1.196 1075 560 5.4 

10200 1071 560 5.4 

1.205 1062 569 5.3 

1.493 793 560 5.6 

1.498 788 560 5.8 

1.500 785 560 5.6 

1.494 792 560 5.8 

1.495 791 560 5.8 

1.493 793 560 5-06 

CHAMBER 

PC TC 

255 664 

492 653 

493 911 

1000 673 

994 909 

1449 686 

1508 908 

0 0 

153 654 

175 592 

247 596 

254 664 

496 048 

493 917 

1003 644 

1022 396 

1490 905 

1496 666 

0 0 

120 659 

125 891 

245 906 

254 664 

497 662 

496 915 

998 678 

993 909 

1503 655 

1497 915 

0 0 

84 669 

65 872 

250 663 

249 913 

- 494 91-3 

(PSIA) (OR) 

SASE 

PB/P P</PB PC/P 

-_ 

e929 

,912 

e913 

,929 

e930 

0938 

a938 

0922 

-848 

.836 

0819 

0814 

0770 

. 774 

0846 

a850 

0899 

0901 

0750 

0544 

0540 

0480 

e486 

0601 

0605 

0713 

0728 

0791 

07e4 

0709 

0471 

0450 

0507 

0509 

18 17 

36 32 

36 33 

71 66 

70 66 

102 96 

106 100 

0 0 

17 14 

20 16 

28 23 

29 24 

61 47 

60 47 

111 94 

112 96 

155 140 

156 140 

0 0 

30 16 

31 17 

69 33 

71 34 

111 67 

111 67 

1P6 133 

183 133 

256 202 

259 203 

0 0 

33 15 

35 16 

90 45 

89 45 

62 
TABLE A-2. ( Con t i nue d ) 

IDe 

RUN/ 

RERUN 

147/0 

14210 

141/0 

140/0 

143/0 

68/0 

67/0 

5610 

62/0 

61 /O 

7610 

71/0 

77/0 

82/1 

83/0 

69/0 

6610 

57/0 

60/0 

63/1 

75/0 

72/0 

81/0 

78/0 

84/0 

87/0 

70/0 

6510 

58/0 

64/0 

59/0 

74/1 

73/0 

TEST 

a810 

FREESTREAM 

m- P TT Rm 

(PSFA)(~R)(M/FT) 

1.494 792 560 5.8 

le498 788 560 5.8 

le499 786 560 5.8 

le499 786 560 5.8 

le505 780 560 5.8 

3 (EDGE TAP) -- Gll 

e503 2181 560 3.6 

e502 2182 560 3-6 

e498 2189 560 3.5 

e501 2185 560 3.5 

e499 2186 560 3.5 

e499 2186 560 3.5 

e503 2181 560 3.6 

e500 2186 560 3.5 

e501 2184 560 3.5 

e492 2197 560 3.5 

e503 2179 560 3-15 

e701 1867 560 4.5 

e702 1865 560 4.5 

e707 1857 560 4.5 

e705 1861 560 4.5 

e703 1865 560 4.5 

e703 1863 560 4.5 

e706 1859 560 4.5 

e702 1866 560 4.5 

e707 1858 560 4.5 

e698 1876 560 4.5 

e698 1873 560 4.5 

e898 1536 560 5.1 

e898 1536 560 5.1 

e910 1515 560 5.1 

e901 1531 560 5.1 

e892 1546 560 5.1 

e901 1531 560 5.1 

e898 1536 -560 -5-1 

~~ 

CHAMBER 

PC TC 

(PSIA)(oR) 

500 666 

1001 912 

1023 668 

1502 652 

1500 901 

0 0 

238 810 

257 633 

488 872 

496 637 

981 873 

997 658 

1479 851 

1505 663 

1992 657 

2001 845 

0 0 

238 826 

262 631 

496 656 

490 859 

989 874 

1025 648 

1496 643 

1493 852 

1999 655 

2000 850 

0 0 

235 833 

243 646 

489 868 

495 668 

989 848 

100.2 652- 

-~ ~~~ ~~~ 

~~ ~ 

33 (AIR, A 

.- 

BASE 

PB/P PC/PB PC/P 

-628 145 91 

e772 237 183 

e767 245 188 

e834 330 275 

e823 336 277 

e980 0 0 

A=8eO, 15 DEGe) 

e928 

e933 

e922 

-914 

e910 

e910 

e911 

e914 

e925 

e922 

e955 

e885 

e888 

e877 

e880 

e846 

e845 

e862 

e859 

e882 

e880 

e925 

e819 

e824 

e000 

e805 

e743 

17 16 

18 17 

35 32 

36 33 

71 65 

72 66 

107 97 

109 99 

141 131 

143 132 

0 0 

21 le 

23 20 

44 38 

43 38 

90 76 

94 79 

134 115 

135 116 

174 153 

175 154 

0 0 

27 22 

28 23 

58 46 

57 46 

125 93 

e747 926 94 

63 
TABLE A-2. (Continued) 

472/0 

- 

ID. FR-EESTREAM ___ 

RUN/ I bl- P TT RE/L 

.903 1528 561 501 

42310 

455/0 

454/0 

422/0 

457/0 

425/0 

453/0 

42110 

459/0 

452/0 

420/0 

473/0 

448/0 

416/0 

462/0 

417/0 

449/0 

430/0 

418/0 

450/0 

451/0 

419/0 

460/0 

474/0 

415/0 

447/0 

414/0 

467/0 

446/0 

e900 1533 562 5.1 

0899 1534 563 501 

a895 1542 563 5.0 

0904 1526 562 5.1 

0893 1543 560 5.1 

0905 1524 561 501 

OR78 1570 557 5.1 

0907 1522 562 5.1 

0900 1532 561 5.1 

.902 1529 558 5.1 

0905 1524 563 5.1 

1.199 1071 561 5.4 

1.204 1063 562 5.4 

1.201 1067 564 5.4 

1.213 1052 561 5.4 

1.201 1067 564 5.4 

10200 1069 561 504 

1.204 1063 561 504 

1.201 1067 563 504 

1.197 1073 561 5e4 

1.795 1075 561 504 

1.202 1066 563 504 

1.204 1063 561 5.4 

10466 741 563 502 

1.446 762 564 5.2 

1.449 760 560 503 

1.463 745 565 5.2 

1.466 742 561 5.3 

1.464 743 56L. -5.3. 

C H A MB E R,: 

PC TC 

(PSIA) (OR)- 

1482 663 

1484 868 

1985 815 

1996 653 

477 679 

490 815 

840 834 

910 677 

943 1001 

1023 523 

1322 815 

1322 685 

1617 1010 

1649 834 

1636 686 

0 0 

394 &@O 

490 661 

886 976 

913 676 

918 844 

1003 512 

1314 685 

1464 872 

1595 689 

1662 7003 

0 0 

470 671 

513 907 

914 693 

914 9P3 

933 891 

1326 878 

.778 a78 138 

0770 182 140 

m8OS 232 187 

.806 232 187 

e767 

0770 

0861 

.S70 

e881 

0908 

0917 

0944 

0952 

0981 

. 9?5 

0747 

0626 

0665 

0799 

e802 

.eo6 

0894 

,904 

e930 

,959 

0978 

0708 

0714 

0735 

0877 

.e87 

.a48 

58 45 

60 46 

91 78 

99 86 

100 88 

107 97 

132 121 

132 125 

155 152 

158 155 

157 155 

0 0 

85 53 

99 66 

152 121 

154 123 

153 126 

160 136 

188 177 

197 17f! 

211 196 

225 215 

230 225 

0 0 

132 97 

202 177 

200 177 

124 a9 

,686 204 181 

64 
TABLE A-2. 

468/0 

.- -~ TEST 

635/0 

(Continued) 

3.480 175 561 10.3 

1- (EDGE TAP) -- G2 9 

w906 1523 556 5.1 

ID. 

PUN/ 

?ERUN 

E37 

413/0 

445/0 

412/0 

444/0 

465/0 

475/0 

471 /O 

440/0 

408/0 

470/0 

409/0 

441/0 

438/1 

442/0 

469/0 

410/0 

411/0 

443/0 

FREESTREAM 

M P TT RE/L 

(PSFA) (OR) (#/FT) 

1.477 731 561 502 

10461 747 565 502 

10464 744 560 5.3 

10473 734 564 5.2 

1.469 739 559 5.3 

10466 742 561 5.3 

3.480 175 559 10.4 

3.480 175 561 10.3 

3.480 175 561 1003 

3.480 175 559 10.4 

3.480 175 561 10.3 

304&O 175 559 10.4 

3.480 175 561 10.3 

3.480 175 561 10.3 

3.480 175 560 10.4 

3.480 175 561 10.3 

3.480 175 559 1004 

3.480 175 560 10.4 

30480 175 560 10.4 

615/0 

616/0 

607/0 

617/0 

634/0 

618/0 

636/0 

622/0 

621/0 

620/0 

633/0 

608/0 

619-/0 ~______ 

w894 1543 577 4.9 

w901 1531 557 5.1 

w906 1524 561 507 

w9OI 1531 558 501 

w902 1528 569 5.0 

.9oi is32 558 501 

1.200 1070 557 5.5 

1.193 1079 557 5.5 

1.201 1068 558 5.4 

1.202 1067 558 504 

1.178 1078 569 5.2 

10212 1054 559 5.4 

1.210 1056 559 5.4 

CHAMBER 

PC TC 

(PSIA) (OR) 

1077 527 

1276 706 

1345 855 

1591 745 

1626 858 

1,638 987 

0 0 

390 927 

459 818 

491 696 

822 970 

896 697 

918 820 

1011 600 

1241 821 

1288 987 

1292 684 

1640 678 

1649 828 

1679 978 

33 . . (C.F 4 f_ A 

0 0 

830 839 

1145 848 

4513 754 

1558 870 

9620 1031 

1866 870 

0 0 

825 848 

1225 857 

1552 867 

'9606 1029 

1586 795 

1880 837 

BASE 

PB/P PC/PB PC/P 

0953 223 212 

0972 253 246 

0981 265 260 

1'.047 298 312 

10054 301 317 

1.053 302 318 

w436 0 0 

w882 364 321 

w936 404 378 

w940 430 404 

1.198 566 677 

10221 605 731! 

1.242 609 756 

1.354 615 833 

1.399 731 1023 

1.446 734 1061 

1.439 739 1064 

1.581 854 1350 

1.564 868 1358 

1.587 871 1383 

w913 0 0 

4=8wO9 15 DEGw) 

w773 

we14 

.a55 

we69 

w895 

w906 

0745 

w641 

0730 

0786 

w819 

w780 

0831 

100 77 

132 10F 

167 143 

169 147 

171 157 

194 175 

0 0 

172 110 

226 165 

267 210 

262 295 

278 217 

308 256 

65 

-. 
TABLE A-2. (Concluded) 

ID. 

RUN/ 

RERUN 

637/0 

623/0 

632/0 

624/0 

612/0 

609/0 

625/0 

62610 

638/0 

630/0 

629/0 

611/0 

628/0 

610/0 

631/0 

627/0 

I_.__ (PSFA) (OR) . ._ (M/FT) 

1.454 755 558 5.3 

la453 

1.461 

1.459 

1 a462 

1.457 

1.467 

1 a476 

3.480 

3.480 

3.480 

3.480 

3.480 

3.480 

3.480 

I- 3,4eO__ - 

756 558 5.3 

747 559 5.3 

750 556 5.3 

746 560 5.3 

751 558 5.3 

740 558 5.3 

731 559 5.3 

175 567 10.2 

175 567 10.2 

175 567 10.2 

175 567 10.2 

175 567 10.2 

175 566 10.2 

175 568 10.7 

175 _-___ 566 10.2 

(PSIA) (OR) - _- 

0 0 

848 851 

9118 987 

1213 840 

1210 1015 

1260 610 

1556 844 

1916 868 

0 0 

813 859 

1185 842 

1459 924 

146d 857 

1519 797 

1618 1012 

1795 855 

_____-__ 

. 707 0 0 

e712 227 162 

a799 270 216 

0800 291 233 

a826 283 234 

,792 305 242 

.864 350 303 

.922 409 377 

a185 0 0 

.E15 821 670 

1.001 974 975 

1.159 1036 1202 

1.127 1070 1206 

1.113 1124 1250 

1.251 1065 1333 

- 1.246 ?lE5_ 1477 

66 
TABLE A-3. TEST DATA OF PRIMARY INTEREST - ET/SRB CLASS 

IDe I FREESTREAM I CHAMBER I ET BASE I SRB INBOARD-BASE 

RUN/ 1 M P TT RE/L I PC TC I PB/P PC/PB PC/P I PB/P PC/PB PC/P 

RERUN 1 (PSFA)(OR)(M/FT)~(PSIA)(~R) I I I TEST 7 --- GlVN24 (AIR, A/A=8.01 35 DEGe) ' 61/1 e500 590 540 1.0 0 0 

72 /2 

61 /2 

50/2 

65 /2 

' 49/2 

73/4 

40 /2 

86/2 1 60/1 

60/2 

64/2 

51 /2 : 71/2 

48/2 , 7412 ' 41/2 

85/2 

62/1 

62 /2 

6312 

5212 

7018 

47/2 

75/2 

5914 

84/2 

56/1 

56/2 

66/2 

53/2 

69/2 

46/2 

76/2 

e499 1220 549 2.0 790 664 

e499 593 540 1.0 , 397 881 

e499 1220 545 2.0 I 823 923 

.SO0 591 540 le0 

e501 1220 546 2.0 

.498 1220 549 2.0 

e498 1220 542 2.0 ' .498 1221 545 2.0 , e900 587 545 2.0 

e907 585 545 2.0 

e899 595 543 2.1 

e898 855 546 2.9 

.899 a57 550 2.9 

e897 857 547 2.9 

-900 856 550 2.9 

e895 856 544 2.9 

e898 855 546 2.9 

1.053 596 543 2.6 

le052 59P 543 2.6 

1.051 596 544 2.6 

le049 718 546 3.1 

1.048 720 551 3.0 

le047 719 550 3.0 

1.052 719 553 3.0 

1.053 716 550 3.0 

le047 724 546 3.1 

le200 592 553 3.0 

le199 594 553 3.0 

1.201 595 551 3.1 

le200 594 550 3.1 

!.e199 598 551 3.1 

1.200 594 553 3.1 

1.198 596 553 3.1 

428 679 

1188 952 

1320 659 

1454 885 

1564 649 

0 0 

386 855 

438 683 

813 910 

831 664 

1167 936 

1260 666 

1470 893 

1523 649 

0 0 

400 860 

439 705 

814 934 

813 651 

1171 961 

1268 663 

1520 927 

1571 640 

0 0 

403 931 

439 664 

801 946 

842 674 

1152 973 

1255 671 

~~ 

' .984 

e 989 

, e984 

e 988 

e 985 

,990 

e991 

e991 

0993 

e955 

.981 

e976 

.993 

,994 

1.017 

1 e020 

1.034 

1.041 

.eo2 

-864 

.e75 

.938 

e940 

1,002 

1.018 

1,051 

1.055 

e783 

-846 

-848 

e938 

,933 

1.013 

0 0 

94 93 

98 96 

98 97 

106 104 

142 140 

157 156 

173 172 

186 184 

0 0 

97 95 

109 106 

138 137 

141 140 

193 196 

208 212 

239 247 

246 257 

0 0 

112 96 

121 106 

174 163 

173 163 

234 234 

249 254 

291 306 

296 113 

0 0 

115 98 

125 106 

207 194 

217 203 

276 279 

1.020 297 303 

.959 

e939 

e947 

e940 

e947 

e960 

a966 

e973 

e 974 

e862 

e867 

e889 

e939 

d946 

1.007 

1 e020 

le050 

1.060 

e662 

.775 

e801 

e950 

e961 

1 e043 

1 e072 

le103 

1.109 

e551 

e767 

e774 

e966 

e981 

1 e072 

0 0 

99 93 

102 96 

103 97 

110 104 

146 140 

161 156 

176 172 

189 184 

0 0 

110 95 

119 106 

146 137 

148 140 

195 196 

206 212 

236 247 

242 257 

0 0 

124 96 

132 106 

172 163, 

169 163 

225 234 

237 254 

277 306 

282 313 

0 0 

127 98 

137 106 

201 194 

207 203 

260 279 

le102 275 303 
TABLE A-3. (Continued) 

.944 227 214 

0952 233 222 

1.023 319 326 

1.035 338 349 

1.076 389 419 

.ai4 379 308 

1.082 1092 1182 

1.086 408 444 

596 0 0 

e990 639 632 

1.145 792 907 

1=5rO1 25 DEG.) 

.9a9 0 0 

.9a7 55 55 

,992 150 148 

965 0 0 

990 78 78 

1.025 143 147 

1.054 201 212 

.ai 5 0 0 

.919 103 95 

1.014 170 172 

1.052 239 251 

766 0 0 

0893 120 107 

1.022 207 211 

0755 0 0 

e893 147 131' 

1 e025 238 244 

.9a9 104 io3 

RERUK 

55 /3 

1 6712 

54/2 

68~2 

!101/3 

- TEST 

10912 

114/2 

121 /2 

109/3 

11011 

113/2 

111/2 

110/2 

122/2 

115/2 

120 /2 

122/3 

119/1 

116/2 

-119f2 

118/2 

117/2 

118/3 

FREESTREAC 

M P TT RE/L 

(PSFA) (OR)(M/FT) 

1.199 594 551 3.1 

1.197 599 556 300 

1.301 518 552 300 

1.301 519 552 3.1 

1.301 521 552 3.1 

1.299 521 553 3.1 

1.302 519 551 3.1 

~ 45/3 ~ 1.301 520 553 3.1 

I 44/2 ' 1.300 520 552 3.1 

77/3 1.299 523 554 3.0 

1.299 523 555 3.1 

2.000 184 580 2.3 

1.998 185 581 2.3 

1.996 185 580 2.3 

1.997 185 583 2.3 

__ 1.997 185 583 2.3 

? G1 

"500 1212 562 2.1 

e503 1212 546 2.0 

0501 1216 549 2.0 

-496 1218 542 2.0 

a898 851 545 2.9 

0901 850 547 2.9 

-900 854 546 2.9 

-892 865 546 2.9 

1.053 713 552 3.0 

--- 

1.048 723 548 3.1 

1.043 723 554 3.0 

1.043 722 552 3.0 

1.201 594 556 3.0 

1.200 595 548 3.1 

1.198 599 556 3.1 

1.302 518 555 3.0 

1.301 519 553 3.0 

1.300 521 555 3.0 

CHAMBER ET BASE 

1580 677 1.073 354 380 

.7ao 

373 ea4 ~ .a51 122 io3 

438 972 ! .866 140 121 

776 697 

799 964 

1178 975 

1269 698 

1514 976 

1612 702 

0 0 

395 964 

811 976 

1163 977 

1517 965 

!3 (AIR, A 

0 0 

460 0 

1256 0 

0 0 

458 0 

870 0 

1274 992 

0 0 

476 0 

864 953 

1259 945 

0 0 

442 0 

879 991 

0 0 

472 0 

881 946 

872 986 

1.122 307 344 1 

1.160 

e506 

.7 04 

.9F7 

0997 

1.105 

1.133 

1.161 

1.189 

0359 

e963 

1.015 

.ai4 

1.121 

1.127 

328 380 

0 

149 121 

217 214 j 

223 222 I 

295 326 ~ 

306 349 1 

361 419 

373 444 ' 

0 01 

320 308 

623 632 I 

809 907 

1048 1182 ; 

I 

I 

.953 0 oi -927 59 55 i 

e959 108 103 j 

.980 151 148 

848 0 01 

0884 88 78 1 

1.009 145 147 ' 

1.076 197 212 I 

0689 0 0 

.879 108 95 

1.064 162 172 

1.137 221 251 ' 

e621 0 0; 

0874 122 107 

1.079 196 211 1 

0513 0 

.901 145 1310 i 

1.081 225 244 
TABLE A-3. (Continued) 

ET BASE 

PB/P PCfPB PCfP 

l.O@5 331 360 

,612 0 0 

.97i 348 338 

1.192 551 657 

1.247 785 979 

ID. I FREESTREAM I CHAMBER 

RUN/ I M P TT REfL 1 PC TC 

SRB INBOARD BASEPBfP PCfPB PCfP 

1.159 310 360 

e350 0 0 

e861 392 338 

1.028 639 657 , 

1.188 824 979 

RERUN I (PSFA) (OR) (Mf FT) 1 (PSIA) (OR) 

123f2 I 1.297 521 554 3.0 I 1300 1023 

1.991 187 571 2.4 

1.987 187 572 2.4 

1.986 187 572 2.4 

170f 4 

17212 

171f2 

0 0 

439 955 

a55 978 

170f5 I 1.991 187 571 2.4 I 1269 992 

128f 1 ,500 597 539 1.0 ' 0 0 

TEST 7 --- G29N22 (CF49 A 

137f 2 

138f3 

148f1 

I 129f 2 

136f 2 

139f 2 

147f1 

130f 2 

135f2 

140f2 

147f2 

146f1 

131f2 

134f3 

142/2 

146f 2 

145f1 

132f2 

133f 2 

141f2 

145f2 

154f 1 

156f 4 

155f2 

154f2 

12812 

0498 1218 569 1.9 

-500 596 539 1.0 

,497 1215 554 2.0 

.a99 856 551 2.9 

.89a 599 543 2.1 

e896 557 569 2.8 

e895 855 553 2.9 

1.053 714 554 3.0 

1.049 596 544 2.5 

1.046 720 569 2.9 

1.044 721 553 3.0 

1.048 719 555 3.0 

1.203 591 558 3.0 

1.199 597 551 3.1 

1.197 596 570 2.9 

1.198 595 558 3.0 

1.198 595 558 3.0 

1.301 526 554 3.1 

le300 518 552 3.0 

1.300 519 570 2.9 

1.300 519 568 2.9 

1.298 522 556 3.0 

802 0 

405 894 

1117 0 

0 0 

820 0 

1240 0 

0 0 

385 901 

a06 0 

1241 0 

1540 964 

0 0 

384 907 

788 0 

1243 0 

1536 990 

0 0 , 380 904 

784 1005 

1531 974 

378 846 

~ 1247 0 

le991 186 582 2.3 1 95i 

1.989 188 583 2.3 793 1016 

1.989 188 5P2 2.3 

1.983 187 583 2.3 1185 1042 

.9b9 

.990 

.959 

.978 

.999 

1 e036 

,809 

.9a4 

. 869 

e956 

1.040 

1 e065 

-766 

.a35 

.944 

1 SO66 

e726 

.794 

,931 

1.055 

1.048 

1.096 

580 

.823 

1.028 

96 95 

99 98 

134 132 

0 0 

93 91 

201 209 

0 0 

107 93 

169 161 

238 248 

290 306 

0 0 

111 93 

202 190 

287 301 

349 372 

0 0 

133 106 

234 218 

328 346 

385 422 

0 0 

590 607 

138 138 

375 308 

1.090 835 911 

.954 

.954 

.969 

-846 

0865 

e954 

1 .041 

e685 

.773 

.969 

1 .OF5 

1.131 

e625 

e727 

.958 

1 e1 12 

1.160 

564 

e741 

0963 

1.115 

le162 

0336 

e642 

0849 

99 9s 

103 98 

137 132 

0 0 

105 91 

145 138 

201 209 

0 0 

120 93 

166 161 

229 248 

273 308 

0 0 

127 93 

199 190 

270 301 

320. 372 

0 0 

143 106 

226 218 

310 346 

363 422 

0 0 

430 308 

715 607 

1.088 a37 911 J 
4 

0 

ET BASE 

PBlP PCIPB PCIP 

TABLE A-3. (Concluded) 

SRB INBOARD BASE 

PBIP PCIPB PCIP 

ID. 1 FREESTREAM I CHAMBER 

iUN/ I M P TT REIL I PC TC 

-900 916 542 3.2 1 216 6330 

1 

14 

31 

20 

33 

21 

79 

0 

30 

31 

36 

42 

48 

2 

I7 

I 24 

!6 

25 

18 

' 17 

15 

, 27 ' 17 

1 28 

' 19 

\5 

;4 

10 

22 

9 

23 

11 

3 

30 

I 26 

! 32 

~ 13 

j 29 

I5 

i 12 

1.297 

e552 

e898 

e858 

a938 

1.004 

1sOg6 

tERUN I (PSFA) (OR) (RIFT) I (PSIA) (OR) 

TEST 8 --- G59N21 (16% A 

I .492 1199 541 2.0 I 0 0 

I 

A=3.1* 20 DEGs) 

a977 0 0 

s985 

1.012 

1.016 

10030 

1 e038 

1 e006 

1 e041 

1.068 

1 e093 

1 e136 

.936 

I 1.052 534 542 2.3 ' 0 0 ' 0812 

1.048 1384 556 5.7 159 6330 ' e971 

1.048 854 543 3.7 156 6330 

1.055 532 541 2.3 156 6330 

1.051 404 542 1.7 157 6330 ' 1.056 430 542 1.9 219 6330 

1.095 666 544 3.0 0 0 ' 1.098 664 548 3.0 152 6330 

1.195 587 545 3.1 0 0 

~ 1.197 1241 569 6.1 124 6330 ' 1.195 848 553 4.3 122 6330 

1.202 457 542 2.4 163 6330 

1.200 409 542 2.2 226 6330 

1.296 513 553 3.0 0 0 

1.292 645 553 3.7 134 6330 

I 1.294 772 556 4.5 165 6330 

1.291 692 551 4.0 174 6330 

1.294 494 546 2.9 145 6330 

1.297 493 547 2.9 164 6330 , 1.297 348 542 2.1 138 6330 

I 1.203 625 547 3.3 158 6330 

1.013 

1.077 

1.137 

1 e208 

a831 

1 a005 

a753 

i -908 

' 1.005 

' 1.095 

1 s131 

, e680 ' .852 

e828 

.1 -886 

, -936 

I e960 

I s998 

1 a855 

11 

17 

27 

31 

53 

0 

12 

22 

32 

40 

43 

0 

17 

26 

39 

49 

61 

0 

33 

0 

17 

23 

36 

47 

70 

0 

35 

37 

41 

45 

50 

57 

11 

17 

28 

32 

55 

0 

12 

23 

34 

e948 0 

e947 

-962 

.993 

1.002 

1 SO54 

e836 

a867 

0965 

1.064 

26 

42 

56 

73 

0 

33 

0 

14 

1.007 

1.1 59 

1 e225 

1 e284 

s630 

1 so64 

s616 

e751 

0 

12 

18 

28 

32 

52 

0 

14 

24 

32 

40 

43 

0 

19 

26 

36 

46 

57 

0 

31 

0 

19 

24 

34 

44 

61 

0 

33 

36 

39 

42 

44 

52 

11 

17 

28 

32 

55 

0 

12 

23 

34 , 

44 

0 

17 

26 

42 

56 

73 

0 

33 

0 

14 

21 

37 

51 

79 

0 

30 

31 

36 

42 

48 

57 

.4 9 , 

1 16 -' 1.297 363 541 2.2 ,, 225 6330 , 1.143 78 89 ' 1.248 71 89 
TABLE A-4. TEST DATA OF PRIMARY INTEREST - 

SRB-ALONE CLASS 

I ID0 FREESTREAM ~ CHANBER ._ BASE 

RUN/ lur P TT RE/L PC TC PB/P PC/PB PC/P 

RERUN (PSFA) (OR) (M/FT) (PSIA) (OR) 

104/0 .507-2193 549 3.7 717 a95 0921 51 47 

TEST 10 (F1) --- G21Nll (CF4r A/A=8oOt 15 DEE.) - 

71 
.- 

TABLE A-4. (Continued) 

ID. F R EfS T R-E A M CHAMBER 

RUN/ Y P TT RE/L PC TC 

RERUN 

58/0 

57/0 

50/0 

55/0 

59/6 

62/0 

61/1 

60/0 

59/0 

63/8 

63/0 

64/0 

65/0 

66/0 

40/9 

46/0 

45/0 

44/0 

(PSFA)<OR) (M/-FT) _(PSIA) (OR). 

1.199 1074 559 5.4 274 0 

1.797 1077 559 5.4 427 0 

1.198 1076 558 5.5 721 0 

10201 1072 55Fi 505 1133 0 

1.467 825 559 5.9 0 0 

10467 825 559 5.9 255 0 

10472 819 558 509 442 0 

10462 630 558 509 798 0 

1.467 825 558 509 1296 0 

10959 550 558 700 0 0 

1.961 548 549 702 225 0 

1.958 551 549 7.2 395 0 

1.958 551 549 7.2 679 0 

1.961 548 549 702 1351 0 

3.481 97 549 5.9 0 0 

30481 97 549 509 213 0 

3.481 97 549 509 513 0 

3.481 97 549 509 1048 0 

.. 

BASE 

PB/P PC/PB PC/P 

.672 55 37 

0783 73 57 

a931 104 90 

10086 140 152 

0551 0 0 

0712 62 44 

0852 91 78 

1.004 138 138 

10149 197 226 

0455 0 0 

0814 127 103 

0952 186 177 

1.156 307 355 

0283 0 0 

,761 416 316 

1.029 740 761 

1.303 1193 1555 

e673 88 59 

43/0 3.481 97 -- 549 -559 1-34? o 1.388 1442 2002 

27/9 .508 2176 549 3.7 0 0 0947 0 0 

TEST10 (F21 --- G19N1Z (-AIR, A/A=5:O, 25 DEG.) __ 

27/0 .510 2173 

28/0 .509 2175 

2910 .508 2177 

30/0 ,507 2178 

23/9 .883 1568 

20/0 0906 1526 

25/0 0908 1523 

24/1 .905 1527 

2310 0887 1561 

19/9 10212 1053 

19/0 1.201 1068 

20/0 1.197 1077 

21/0 1.203 1067 

22/0 10201 107L-_. 

549 3.7 365 

549 3.7 461 

549 307 573 

549 3.7 744 

549 5.2 0 

549 502 330 

549 503 443 

549 5.2 651 

549 502 918 

549 506 0 

549 5.6 273 

549 506 420 

549 506 709 

549 ____ 506 1098 

0 0856 

0 0894 

0 .507 

0 0920 

0 0632 

0 .a38 

0 .ma 

0 .707 

0 e888 

0 0677 

0 0608 

0 0717 

0 1.012 

0 .a02 

27 24 

34 31 

42 3F! 

53 49 

0 0 

49 31 

59 42 

76 61 

95 85 

0 0 

61 37 

78 56 

711 96 

__ 

146 147 - 

72 
II r-- 

TABLE A-4. ( Concluded) 

I 

.- 

_. ID. 

RUN/ 

__ RERUN 

15/9 

18/0 

17/0 

16/0 

15/0 

11/1 

12/0 

13/0 

14/0 

31 /8 

34/0 

31/1 

31/1 

3211 

.- 

FREESTREAM 

M P TT RE/L 

(PSFA)(~R)(M/FT) 

1.465 826 549 '6.0 

1.o462 830 549 6.0 

1.466 d25 549 6.0 

1.465 826 549 6.0 

1.461 831 559 5.9 

1.958 552 558 7.0 

1.965 545 559 7.0 

1.979 533 549 7.1 

1.960 549 559 7.0 

3.L81 97 549 5.9 

3.480 97 549 509 

3.480 97 549 5.9 

_lo480 97 549 5.9 

3.480 97 549 5.9 

-C H A ME-E R 

PC Tc 

(PSIA) (OR) 

0 0 

252 0 

439 0 

792 0 

1327 0 

220 0 

390 0 

657 0 

1297 0 

0 0 

220 0 

493 0 

1048 0 

1254 0 

PASE 

PB/P PC/PB PC/P 

0496 

0643 

e785 

09L3 

1 .lo2 

. 574 

.722 

0866 

1.072 

e315 

a756 

1.031 

1.326 

1 a407 

0 0 

68 44 

97 77 

146 13P 

209 238 

100 57 

143 103 

205 177 

317 340 

0 0 

471 326 

710 732 

1174 1556 

1324 1863 

L.. 

73 
APPENDIX B 

I Class 

COM PLETE PRESSURE DATA I 

Table 

The complete base, body, and nozzle pressure data for each valid windon run of the seven selected tests are presented in this appendix. Locations of 

the various pressure ports are shown in Tables 6 and 7 of text. Corresponding 

model chamber conditions and tunnel freestream parameters are given in 

Appendix A. Because of the significant geometry difference between the base/ 

body region and the nozzles, these two types of data are presented in separate 

tables. Base and body pressures are given in Tables B-1 through B-4 for all 

of the cases given in Appendix A, both jet-on and jet-off. Nozzle wall pressures 

are given in TablesB-5 through B-8 for only jet-on runs. The following index 

relates these tables to the four body geometry types for the two types of pressure data. In all cases, the sequence of presentation of runs is identical to that 

of Appendix A. 

Classic Geometry 

INDEX TO TABLES 

B-1 76 B-5 

Pressure Data 

Base and Body Nozzle Wall 

Orbiter Class 

ET/SRB Class 

SRB-Alone Class 

B -2 103 B -6 

B-3 127 B-7 

B -4 150 B -8 

Page 

156 

161 

16 5 

170 

An example is given of obtaining the model chamber and tunnel freestream conditions for a particular case: Run 356/0 of Test 1. This case is the 

second one presented in this appendix within the classic geometry shape (see 

Table B-1) below. Thus, the desired data will be found at the second case presented in Appendix A. At that location the following values are found: 

74 

P 
M = 0.888 W 

P = 1553psfa W 

= 563"R 

co TT 

Re = 5.0 x 106/ft 

P = 466 psia 

C 

T = 958"R. 

C 

Correspondingly, the desired nozzle wall pressure data will be found in 

the classic geometry portion of the nozzle section of this appendix (Table B-5). 

Because jet-off runs are not included in the nozzle section, the desired nozzle 

data will be found at the ith position: i = j - n , where the base and body case 

is the jth position and n is the number of jet-off runs up to position j. In this off 

example, j = 2 and n = 1 so i = 1. At that location the value of P /P for 

Tap No. 47 is found to be 26.45. 

off 

off CW 

Nozzle calibration data (wind-off) are given in Appendix C. 

75 
TABLE B-1. BASE AND BODY SURFACE PRESSURE RATIOS (P/P ) FOR CLASSIC GEOMETRY 

CQ 

0 .52 

0 e84 

a03 1.0 

X/D R/R 

0 e52 

0 e64 

.03 1.0 

e22 1.0 

e40 1.0 

e55 1.0 

e76 le0 

e94 1.0 

TEST 1, RbN 354/0 

m943 a954 

e939 e946 e951 

e959 e951 e969 

W=O =60 =180 

TEST 1, RliN 372/0 

e915 e898 

e946 .9G4 e902 

e935 .919 .935 

e946 a963 

e97b e978 

.9ac .979 

e979 e986 le015 

1.013 .999 

e59 le0 

-76 le0 

le12 1.01 e976 e992 1.022 

1.30 le0 e9b3 -989 

e991 a993 

e991 le000 le026 

(A) ElA 

y=O =60 =180 

e991 e996 

.977 a977 

.971 

,963 e951 1.042 

,954 

e963 e964 

.977 

TEST 1, RUN 356/0 

e850 e854 

.E46 e847 eE56 

e060 e949 

-968 e966 

e973 e973 

1.911 .992 

.a92 .a75 .go6 

.376 .9a2 1.01’3 

e978 e392 le019 

0966 e991 

e995 1.001 

e981 e982 

.976 

e970 e958 1.044 

e 960 

e969 e971 

e985 

le48 le0 .973 ,972 , e972 e972 1 .97@ 

2.20 IeO! .9b? e948 1.0421 e968 e956’ 1.044 

2.56 1.01 e956 , e961 

I 1.84 leu/ .966 

2.92 1.0/ .F63 .963 ’ .971 .969 

3.28 1.0, e979 e 9b0 

rEST 1, RUN 322/0 

e973 0982 

e567 e970 e981 

e980 e966 e991 

eo(i0 e993 

e996 e998 

0=0 =60 =180 

:EST 1, RUN 323/0 

e845 e849 

e841 me43 e851 

e891 eE75 e903 

e000 e948 

e966 e968 

.973 e975 

e977 e985 1,014 

le013 e997 

e976 e991 le023 

,983 e989 

e970 e970 

.907 

.963 .C49 1.043 

.955 

.964 .965 

e977 

TEST 19 “RUN 353/0 

1.000 le015 

e994 1.002 1.006 

le005 le000 le012 eooo 1.011 

1.007 le010 

e?Y4 e990 !le003 le007 

.9Y3 1.500 1.031 11.002 1.010 1.036 

- --- - -_- - --- --. ,l.UL5 1.GVf IleUJU 1.014 

1.12 1.0 .9E5 1.000 1.03C1 -904 1.002 1.0331 .992 1.006 1.036 

~1.30 1.01 e989 e996 

11.48 1.0 e977 .979 

/l.t4 leO1 .972 

i2.20 1.01 e97G -955 1.042 

12.56 1.01 .958 

j2.92 1.0 e966 .972 

13.28 1.01 .986 

0=0 =60 -180 

rEST 1, RUN 35710 

e940 e948 

e933 e936 e948 

e952 ,939 e966 eooo e979 

b987 .985 

.9a7 

. 987 

1 e019 

e 983 

e 990 

e976 

.971 

967 

e959 

e 969 

e980 

e988 

1 e993 1.027 

.999 

.998 1.026 I e 995 

e975 1 

1 

,954 1.041 

0967 

1 

1 

1 

TEST 1, RUN 359/0 

le003 le012 

0995 1.000 1.010 

le005 e996 le015 

.ooo le011 

le008 le007 

le003 1.003 

.998 1,006 1.038: 

.991 1.004 1.031 I 

1.027 1.010 

1 

e995 le000 ~ e981 e980 e 974 

.969 .955 1.043 

e959 

e969 e967 e 980 I 

t 
TABLE B-1. ( Continued) 

(A) COfiTINUED. 

X/D P/R 0=0 - - - - 0=G =6G =180 fj=O =60 =l30 0=0 =60 =1PO 

TEST 1, RUN 3211C TEST 1, RUN 35910 TEST 1, RUN 352/0 TEST 1, RUN 320/0 

0 -52 1.G5C 1.065 1.037 1.050 1.047 1.058 1.074 1.115 

0 ed4 1.047 1.048 1.059 1.329 1.035 1.041 1.037 1.044 1.047'1.087 1.096 1.075 

a03 1.0 1.048 1.036 1.059 1.034 1.028 1.043 1.043 1.039 1.049 1.082 1.085 1.092 

022 1.0 .COO 1.039 .Ob0 1.029 

040 1.0 1.C29 1.032 1.c21 1.022 1.027 1.028 1.036 1.051 1 

-5s 1.0 1.020 1e02C 1.314 1.015 1.017 1.020 1.034 1.041 

no00 1.036 e000 1.050 

.76 1.0 1.C12 1.018 l.O4? 1.008 1.014 1.C47 1.012 1.020 1.046 1.027 1.033 1.063 

e94 1.0 1.037 1.020 1.033 1.015 1.037 1.023 1.047 1.035 

1.12 1.0 0995 1.013 1.044 .974 1.008 1.036 0999 1.014 1.042 la008 1.018 1.053 

1.30 1.0 1.000 1.006 ,999 1.004 1.003 1.009 1.000 1.005 

1.4Q 1.0 0986 -986 .9a5 .~a4 .965 .?86 0990 0989 

l.c4 1.0 .975 ,976 a 978 0979 

io20 1.0 0967 e954 1.043 0368 e937 1.044 0972 mQ59 1.045 0970 0958 1.050 

2.56 1.0 0955 .Q57 961 0962 

2.52 1.0 -065 -964 -968 .966 0972 ,971 0962 a964 

3.291 1.0 09bG ,901 0985 . 979 

1.13C 

8 -52 

0 .E4 

.03 1.0 

022 1.0 

.40 1.0 

053 1.0 

076 1.0 

.F4 1.c 

1.12 1.0 

1.30 1.0 

1.45 1.0 

1.34 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

3.28 1.0 

1.914 1.027 

1.311 1.002 

-951 

e953 a924 1.140 

.Q79 

09~6 1.001 

.Qa2 

TEST 1, RUh 

.734 .734 

.913 .744 

.736 .894 

0044 .98l 

.99c .993 

1.06: 0966 

e999 e998 

1.C5C 1,033 

1.005 1.031 

1oOOi: 1.016 

1.C07 1.006 

0934 

.95e 0917 

0964 

.971 1,013 

.962 

TEST 1, RUN 316/0 

e756 0744 

0741 0733 0745 

0917 0901 0926 

a000 a986 

.9F6 .97E 

1.005 .981 

1.017 1.018 1.017 

1.042 1002P 

1.001 1.026 e996 

1oCOO 1.029 

a994 1.009 

0943 

a973 a930 1.112 

e966 

0976 0993 

.992 

TEST 1, RUN 362/0 

a864 0860 0279 

a927 a906 0934 

.ooo ,975 

,978 0977 

0972 0963 

e985 a971 1eCG2 

1.021 ,997 

1.029 1.017 

1.001 1.008 

1.027 

0965 a975 1.129 

0965 

0984 0972 

.986 

.a86 .a74 

0987 1.011 1.011 
TABLE B-1. (Continued) 

X/D R/R $=O =60 =I80 d=j =6G =180 0=0 =60 =I80 

TEST 1, RUh 749/G TEST 1, RUN 31710 TEST 1, RUN 350/0 

0 e52 *E93 .E84 .Ci6 .972 ,997 a991 

o .t4 e873 .872 ePBQ e7t7 .958 .97a .979 ,980 ,988 

083 1.0 e940 e924 e939 -974 e956 e952 a982 ,972 ,962 

022 1.0 *COG ,993 .o:o .9ae 8000 e994 

s4C 1.0 1.G33 e997 e939 e979 e997 1.000 

.SF 1.0 1e00t .9E2 h.Pb6 .975 1.007 e980 

g=o =60 =I80 

TEST 1, RUN 329/0 

1.013 1.001 

.993 .988 1.005 

.990 .974 e987 

.970 e982 

a982 a986 l a994 e980 

12.92 1.0 0977 1.OOE 

p.2e 1.0; .99c I 

0974 .997 

e952 

1 .ClP 1 a009 1 ,013 

1.053 1.034 

.996!leOO9 1.033 

1.008 1.022 

'1.005 le007 

' .936 

1.124' a968 a927 

. 973 

,980 1.008 

a991 

0 .52(l.C16 e999 

C m994 a965 1.005 

.03 a992 .977 .969 

.22 1.01 .ooo 1.000 

040 1.0'1.002 e977 

e5E le0 1.013 ,992 

076 1.O/l.C24 1.022 le022 

e94 le0 1.055 1.027 

1.12 1.01 a997 le024 le016 

11 030 1.0 11 e011 1.033 

1.4F 1.0 a996 a995 

11.34 1.0 *951 

1.025"1.001 .986 1.022 

1.044 1.015 

1.001 ,1.012 1.034 1.011' 

1 e954 1 

' e989 e999 , -985 1 

,1.015 1.037 

. 1.009 1.006 

1.127, a951 e929 1.132 

982 

32Q/0 TEST 1, RUN 

1 a067 

1.058 

1.028 

e 967 

.Ob5 

.932 

.FY9 

1.040 

1 e015 

1.318 

1.003 

a362 

946 

1.068 1 .I36 

1.053 1.059 1.138 

1.022 1.022 1.089 

e986 . 000 

a983 ' 1 moo2 . 979 1.005 

-966 1.018 1.017 

1.013 1 e042 

1.032 1.017 1.002 

1.040 1.002 

1 e007 a994 

, .939 

a926 1.140 e977 

1.145 

1 .126 

1 e079 

1 a005 

a982 

.977 

1 a015 

1 e027 

1 028 

1.021 

1.004 

a928 

31P/O TEST 1, RUN 351/0 

1.089 1.006 

1.132 1.074 1.074 1.082 

1.073 1.046 1.040 1.019 

e000 e996 

.995 .99e 

11.000 .976 

1.016 1.002 1.010 1.019, 

e996'1.005 1.027 e998 

11.051 1.029 

1.001 1.017 

i1.004 1.003 

930 

1.121 .964 .924 1.1241i 

'2.56 1.0 a974 e961 966 968 1 

e988 l.(rOO .975 e995 I .974 1.005 1 ~ 0990 J e986 1 
I 

053 1.0 0967 1.023 

076 1.0 0923 0980 1.064 

094 1.0 0937 0935 

1.12 1.0 s913 -940 1.139 

1.30 1.0 0970 0936 

1.48 1.0 0966 e910 

1.84 1.C 0946 

2.20 1.0 0949 -923 e964 

2.56 1.0 .9a2 

2.92 1.0 0935 1.001 1 3.28 1.0 0994 

TABLE B-1. (Continued) 

.Q55 1.021 .926 .984 

e945 0990 1.055, 0934 0966 1.063 

0305 0949 0940 0955 

093E 0935 1.124 a956 e927 1.140 

0340 950 0971 ,935 

0948 a909 0934 0925 

0954 0923 

0947 0934 o9b2 0955 0933 0969 

. 947 e952 

0999 1.305 0992 0966 

992 1.013 

(A) COhTINUED. 

i X/D R/R/ 0=0 =60 =la9 '1 0=C =60 =le0 I 0=0 =60 =?PO I 8=0 =60 =180 I 

TEST 1, RUN 360/C. TEST 1, RUN 319/0 TEST 1, RUN 374/0:TEST 1, RUN 347/0 

9 .52 i.iob 1.098 1.138 1.215 j 0708 0790 0783 0767 

0 ob4 1.092 1.061 1.101 1.2G7 1.194 1.197~ 0962 0914 0747 e766 ,778 0776 

022 1.0 .03c 1.010 .3d0 1.031 0976 1.014 e000 1.015 

040 1.0 loco3 0968 1.0t~7 e985 a983 1.019 1,005 1.014 

0.55 1.C 1.C12 -992 I.C;74 .979 0957 1,020 0958 1,008 

076 1.3 1oC2i 1.018 1.025 1.016 1.315 1.019 0923 e974 1.064 a940 0996 1.048 

094 1.C 1.C52 1.029 1.042 1.025 , o9OC 0946 ,908 a940 

1.12 1.0 1.001 1.022 1.015 1.01;4 1.021 0997 e922 e936 1.135 0935 0933 1.122 

1.39 1.0 lee13 1.030 1.CiG4 1.023 , 0948 0944 0941 0957 

1.48 1.0 1oCCLi 1.003 0393 1.004 ' 0953 0910 0942 0913 

l.cL 1.0 .F49 . 939 0951 0954 

2.20 1.0 .9C5 ,939 1.119 0976 0929 1.123 .941 ,933 .967 0945 .941 .964 

2.56 1.0 e976 s 966 . 979 963 

2.92 1.0 0966 1.004 0974 0997 0983 1.004 0993 1.008 

3.28. 1.0 .Y93 I 0967 e990 .9a4 

.i.3 1.0 1.G59 1.049 1.036 1.155 1.151 1.160 .?I3 0956 1.081 0960 e960 1.080 

TEST 1, RUN 346/0 

0946 e943 

0919 0924 .ti22 

.ooo 1.002 

e966 1.039 

.9ai .953 1.074 

.930 .9a5 

0922 0957 1.058 

0917 e949 

0948 0947 1.146 

0993 0937 

0935 0919 

.931 

e953 e932 0966 

0955 

,986 e970 

1.010 
00 

0 

TABLE B-1. (Continued) 

X/D 9/R I== 

3 a52 

3 .84 

e03 1eG 

I .b3 1.3 

! 022 1.c 

1 .58 1.0 

1.12 1.0 

11.30 1.0 

l.cl 1.0 

2.20 1.3 

2.56 le0 

j1.45 1.0 

e76 

.9L 

1.12 

1 e30 

1 e48 

I) .5i 

0 e64 

.ci? 1.c 

022 let 

.40 le( 

e58 le( 

.( 

e( 

e( 

e( 

e( 

led4 le( 

2.20 le( 

2-56 le( 

2-92 le( 

3-28 le( 

$=2 =to =180 

EST 1, RUN 314/0 

.c17 1.010 

e9b5 e990 e999 

e997 e968 1.061 

.COG le004 

e966 1eO43 

-94: ,993 

.tlC .961 le061 

e9OG e9&7 

e342 e953 le172 

e997 .937 

e939 .910 

-935 

-953 -929 e974 

.F65 

.99c ,971 

I .GO9 

lEST 1, RUN 344IC 

le118 1.116 

1.083 le094 le091 

1.040 1.029 1.082 

.OOO 1.003 

e904 1.03& 

.927 e979 

-920 -95t 1.05: 

.OZb -946 

-940 .941 1.15: 

e995 e936 

e932 .915 

0925 

-953 .930 .96t 

e954 

e983 e969 

1 e008 

(A) COFtTINUEDe 

O=G =60 =18O g=o =co =180 

EST 1, RUN 34510 

,346 lee40 

e012 le319 1.015 

eOjb e9b9 le979 

.oil0 1.311 

,368 1.044 

.c31 e9dF 

,QJO -363 le062 

.924 e954 

e952 e943 le145 

,984 .941 

e036 e921 

.928 

-952 e934 e972 

e958 

.991 .972 

I e013 

lEST 1, %UP4 367/C 

1.141 1.129 

IelUL le105 1elOt 

1.951 1.045 le071 

.OOO 1.037 

e976 le024 

eF24 e979 

e945 e962 1.06; 

e939 e943 

e968 e925 1e13t 

.363 e937 

.331 0917 

.924 

e954 e934 -97: e 939 

e969 e970 

1 eo20 

EST 1, RUN 366fO 

e071 le054 

e035 le027 le034 

e009 le002 le058 

e000 le042 

-976 1.928 

-928 ~87 

e949 e969 le063 

e939 ,945 

0961 e925 le131 

e958 e940 

e935 e915 

e928 

-954 -941 .974 

e941 

e962 e972 

I e023 

rEST 1, RUN 31210 

le216 1.241 le187 

le133 le154 le111 

1.199 1.268 

e000 1,006 

e969 le038 

0954 1.001 

e927 e965 1.067 

e902 e948 

e942 e949 1 e173 

e998 e939 

e948 e915 

e945 

e959 e934 -97: 

e973 

e996 e980 

1 e017 

Q=O =60 =1&O 

EST , RUN 313/0 

e158 le153 

e131 le122 1.140 

,066 le037 le094 

e000 1.000 

e964 le038 

-944 -990 

.898 .949 

-947 -947 1,168 

e997 e933 

e946 e912 

e938 

.951 -928 -972: 

-990 -971 

a919 0959 le061 

1 

1 

1 

e 961 I 

1.014 

rEST 1, RUN 375fO 

0246 e248 

e981 e288 m289 

e248 le286 e993 

e985 3.820 

e993 e993 

e965 e942 e054 

e982 ,947 

e972 e964 e911 

le002 e978 

e961 e961 

e 989 

-087 3.820 

-98s .97i .m 

-940 

e968 e966 

e983 
TABLE B-1. ( Continued) 

1.013 e9F3 

e067 e972 

1 e004 

le002 e968 e722 

e943 

e980 e994 

1 e006 

[TtST 1, QllX 77CIG~Ti~T 1, ?L\ 3~31G TEST 1, RUN 508/l TEST 1, RUN 370/0 

2 .5i .73L .?C4 .ILJ 7c .?a4 .763 .737 e925 e886 

3 e64 et74 ,672 .h3@. .F,C~ .e79 a679 -966 e703 a706 e836 me39 eE52 

-33 1.2 .Fc; .F11 1.32Ci ,776 .3i4 1.011 e696 e912 1.001 e984 e912 le017 

.;z 1.0 .clc!c .95L ,ct,: .I-jkL 1.472 0931 e000 e930 

1.2L5 .34t e994 e935 e991 e932 

.51 l.C .FtS .5:2 ..rt .Q41 e065 e930 e984 e958 

.40 1.3 .q%L .F34 

e76 1.0 -973 e53F e947 e779 -95~ e961 e970 e930 e941 -967 -936 e949 

e94 le3 .L&7 .94C .930 .9:1 e933 -940 0946 0936 

<. . 

lei? 1.0 .974 s9C9 -905 ,902 ,979 ,916 -972 -966 e903 e969 e970 e908 

1.30 le0 1.005 ,964 1oC13 e993 1e0C2 e980 1.002 e964 

, 1e4c 1eC eq71 0968 e966 0970 e965 e963 e961 e964 

1.04 1.3 .cy: 1 .oc1 ,992 . 988 

2.2; 1.0 *COS e7El e712 100C2 .98b .723 e990 e980 e7081 e984 e720~ 

2.56 le0 -547 .94 3 -940 e933 

io32 1.0 0969 .F6E ,963 e993 e969 -966 e965 

3.58 1.0 e966 1 e035 .991 e 986 

le014 0991 

e35E e968 

1 eOUl 

e956 e984 0726 

e933 

e972 0991 

e958 

C e52 

0 e04 

eGZ le0 

e22 le0 

040 1.0 

e58 1eC 

e76 le0 

e94 le0 

le12 1.0 

le30 1.0 

le&$ le0 

leL4 le0 

2.20 le0 

2.56 le0 i 2.52 1eC 

3.26 le0 

TEST 1, PLJN 337/C 

1.107 1.056 

0992 e987 1.019 

.9a6 .917 .w6 

e000 e926 

-969 e930 

e980 e926 

eC61 e938 e954 

e915 e938 

e966 e960 e908 

e999 e979 

e956 -959 

e967 

e987 e975 e712 

.931 

e965 e977 

990 

TEST I, RUN 3GQ/0 

1.194 le169 

le090 le095 l.C.90 

a991 e925 e9dl 

eC00 e928 

e988 e930 

,977 e926 

,959 0934 0337 

0918 e941 

.964 e960 .~9a 

e996 e976 

e955 e957 

e984 

e983 e975 e705 

e929 

e960 e962 

e 983 
TABLE B-1. ( Continued) 

0=0 =60 =190 j=O =60 =180 

TEST 1, RUN 310/0 TEST 1, RUN 3L7/0 

1.166 1.139 1.200 1.094 1.132 1.092 

1.002 .?32 .961 1.013 e960 1.017; 

1.316 1.236 1.198 1.190 

.O? 1.0 

.22 1.0 

.40 1.0 

.58 1.0 

e76 1.0 

a000 a926 

0=c =to =180 

.ooo a944 

TEST 1, RUN 342/O 

1.07C 1.039 

.F7G e993 e96C 

1.003 e933 1.013 

.003 .943 

1.609 0946 

0999 .942 

e977 .951 .9c2 

I 

1.12 1.0 ,982 e979 e916 

1.30 1.C 1.014 e993 

1.41 1.0 0967 e973 

1.84 1.0 1.005 

-22 1.0: .coo .944 e060 mF31 , .ooo .934 a000 0872 

040 1.0 1.006 .94P , a995 .935 ~ .994 .936 0935 m871 

*58 1.C 1oCOG .942 ~ .905 .929 .986 a933 a936 0863 

-75 1.0 .97E ,952 .98F ,166 .938 ,958 e967 ,930 ,950 ,930 .867 .932' 

(A) CONTIN 

0=G =60 =180 

TEST 17 RbN ?60/0 

1.071 1.033 

,963 .97Y ,982 

-957 a929 1.027 

.3GO .941 

1.0~3 ,942 

1.361 I .965 1.005 

2.20 1.C 1.C36 .988 0723' -998 ,985 -724' .9&3 a975 e704 1.002 .9F1 a723 

2.56 1.C. e943 ' .340 926 .945 
TABLE B-1. (Continued) 

Zl5/CITEST 1, RUN 15510 TEST 1, RUN 154/0 

I .??a .7a5 e776 e785 

e901 e776 'r783 e762 e775 e782 e781 

e921 e852 e86C e856 ea52 e859 e855 

e939 e939 e937 e939 ' e9G5 e961 e965 e962 

eQ7E e976 e977 e978 

1eC22 eOU0 .987 le014 e000 e987 le015 

1.307 le003 le007 le002 

le021 eo75 e986 le015 e974 e984 le015 

e901 e000 e961 e000 

e974 e977 ,974 m976 

.974 e974 

1.OZF e971 m963 le042 e970 e963 le040 

e966 e 964 

.3tF .3t9 e968 e968 

.978 e977 

co 

w 

TEST 1, RUN 195/0 

e771 e776 

e767 e774 e776 

e842 .a55 e852 

e935 e938 

e963 e959 

e973 e973 

e000 .983 le010 

1*000 e998 

a971 e982 le013 

e979 e000 

e970 e969 

e 966 

e965 e949 lac35 

e956 . e967 e961 

e975 

I 

I !TEST 1, RLiN 

0 e52 e910 me97 

0 e84 e940 e914 

e03 le0 e944 ,334 

e22 1eC eF66 e966 

e40 le0 -981 ,978 

e54 le0 e959 e968 

e76 1.0 .COO a395 

e94 1eC le016 1.007 

1.12 le0 e977 -988 

le30 le0 eF84 e986 

1.48 le0 e977 e978 

lebc le0 e973 

ZeLC 1eC e96Y e959 

2.56 le0 e962 

2eS2 le0 e9Cb e966 

3.26 le0, e977 

e40 le0 

e55 le0 

e76 1.0 

e94 le0 

le12 1.0 

1.32 le0 

1e4? le0 

let4 le0 

2.20 1.0 

2.56 1.0 

2.92 le0 

3.28 1.0 

e9t6 ,964 

eC79 e97P 

.CL;il e987 le315 

le007 le002 

.97i e9E6 1.G14 

eq82 a000 

e975 e977 

e973 

e570 -958 le041 

e962 

e972 e967 

e980 

TEST 1, RUN 115/0 

-774 e763 

e775 e780 e731 

as52 e861 e658 

e?39 e942 

,966 ,964 

.979 .979 

e907 e9b6 le015 

le311 1eOil3 

a974 .9&4 le016 

.?ti2 e985 

e975 e977 

.F74 

e368 e961 le682 

,903 

.CCS e966 

.976 

TEST 1, RUN 193/0 

e826 e333 

ea22 e823 e828 

e872 e883 e876 

e945 e948 

,968 e966 

e979 e980 

e000 e989 le014 

le007 le003 

e974 e988 le015 

e982 e000 

e075 e977 

.973 

e970 e961 le041 

e 964 

e975 e969 

e 979 

TEST 1, RUN 156/0 

e830 e838 

e827 e833 e834 

e874 e883 .pa0 

e947 .9a 

e980 e980 

e970 e965 

e000 e988 1.016 

le008 le003 

e977 e987 le015 

e984 e000 

,976 e978 

e975 

e972 e9bS le042 

e 966 

e972 4970 

-979 

I 
. x/D R/R O=O =60 =le0 $=C; =60 =la0 B=O =60 =I80 8=0 =60 =le0 ~ 

TEST 1t RUN 196/0 TEST 1, RUh 116/0 TEST 1, RUN 153/0 TEST 1, RUN 152/0 

9 -52 e826 e831 e824 e929 e843 eP52 e389 e903 

0 ek4 me21 -822 eF2P e?Zl e826 e828 e842 e847 e848 e889 e896 e894 

e03 le0 eE65 .e79 e875 .573 .E82 e879 e860 e890 e888 e911 e922 e922 

e948 e951 11 e947 e949 e952 e964 1 li 

e22 le0 e943 -946 

e40 le0 e967 e965 e973 e97C ! a970 e967 e980 e961 

e58 le0 e977 a979 e9b4 e983 e981 e980 e992 e992 

TEST 19 RUN 

' 9 e52 et38 e896 

0 e8L e865 e893 

eC3 le0 e910 e921 

022 le0 e958 e962 

e40 le0 a977 s976 

e58 Ieo .gat e985 

1.12 1.0 .97~ ,987 

wa 1.0 e977 ,979 

e70 le0 e990 ,994 

094 le0 1.013 le008 

1.30 le0 e984 -967 

1-84 le0 e972 

Le20 le0 e969 e959 

2.56 le0 e964 

2.92 le0 e96t m964 

,;e28 le0 e977 

e76 le0 

094 1.0 

11710 TEST It RUN 1Y7/0 TEST ?t RU'N 157/O'TEST 19 RUN 192/0 

e993 e887 e894 eP94 e892 e900 e900 e886 e895 eE99 

e917 0937 'e921 e918' e916 e925 e922 e927 e980 a920 

e958 e961 e963 e963 e966 e975 

e976 e974 , e979 e976 I e980 0980 

e903 ,986 e987 .987 e987 e966 

~ -892 eFO2 e896 e906 e889 e892 

1.019 eCb0 e991 1.023 e000 e993 1.021 e000 e994 le020 

1eOL5 le005 le010 le007 le010 le006 

1.01E e977 e9d6 le018 e980 e9.91 le019 e977 e990 le019 

I e965 eOOC , e966 e000 e984 a000 

e374 e973 I e978 e981 e976 e978 

a972 .978 e971 

1.@4G e968 .954 1.038 "974 e968 le043 e970 e956 le039 

.959 e 968 e 961 

e968 e964 1 e973 e972 e971 a968 

: e978 i .980 ! e978 

eOOi .9S6 laole e991 e993 le020 e000 e988 1.015 e000 e998 le026 

1.co2 1.002 le015 le009 le007 le004 le016 le012 
1 

e76 le0 eCO3 1.000 1.029 .COO le003 1.032 e000 le004 le033 

-94 le0 1eC15 1.013 11.017 le015 le016 le013 

1.12 1.0 e985 e994 1.023 e964 e995 le025 e985 e996 le026 

le30 1eOi e99C e000 .990 eooo e990 eooo 

le48 1.0 m982 e985 e979 e983 e981 e964 

led4 1.0 e979 .97 5 e976 

2.20 le0 e974 e967 le043 e971 e962 le039 e973 e962 le041 

2.56 le0 e968 e 964 e965 

2.92 le0 e972 e971 e968 e967 e974 e971 

3-28 le0 e979 e977 e979 

TABLE B-1. (Continued) 

e000 le006 le035 

le017 le018 

e987 e998 le027 

e992 e000 

e084 e967 

e 979 

e973 e966 le041 

e 966 

m972 e969 

e 980 
TABLE B-1. ( Continued) 

X/D R/R 

3 e52 

0 ee4 

003 1.0 

e22 1.0 

.40 1.0 

.59 1.3 

.7t 7.0 

1 .94 1.0 

'1.12 1.0 

e 936 

e984 

1 eooo 

1 e006 

1 .COa 

eo00 

1 e027 

0989 

9ai 

1.30 1eC: ,996 

IeLP 1.0 a986 

1.64 1.0 e981 

2.20 1.0 e976 

2.56 1.0 e960 

LmY2 1eG e07G 

3.28 1.0 .$8G 

(A) CONTIN 

0=u =60 =180 

e003 

e005 

oOOE 

eo11 1.039 

e019 

e000 1.032 

e998 

a986 e960 e978 

.974 

TEST 1, RUN 199/0 

e973 a979 e982 

e974 e987 m986 

.994 e999 

1.co1 .999 

1.3CO le003 

~78 .$a8 

mod0 le006 le037 

le015 le016 

e966 e992 le026 

0990 eooo 

ED e 

gi=o =60 =iao 

TEST 1, RUN 216/0 

e738 .739 

s744 e748 e769 

.901 .913 .912 

a973 m980 

e993 e988 

le012 e976 

e000 1.006 1.029 

le050 le035 

le007 le023 e983 

1.008 1.012 

le015 le017 

e956 

lb=O =60 =180 

TEST 1, RUN 145/0 

a572 .S70 

a558 a562 e567 

a901 a911 a911 

a976 e986 

e994 a988 

1.011 e979 

1.053 le034 

e000 1.008 laG3C 

le007 la026 a9881 

le011 1.015 

1.015 1.018 

e953 

-966 1.040 a970 e954 1.037 e968 e937 le133 .973 a941 la126 

, e960 - ' e985 e980 I 

e969 1 e908 e965 j e978 1.011 e979 1.011 

- ~ .Q79 , e963 a 9'85 . 

TEST 1, RUN 1t4/C TEST 1, RUh 204/O TEST 19 RUN 12410 TEST 1, RUN 185/0 

0 .52 .584 .572 e575 e565 sa0 e585 0575 

G .5t,6 .w' ~5.9 ~62 ~68 mi ,567 ,582 .570 ~72 s78 

-03 1.0 e899 ,912 a918 .8&6 s903 e903 a919 e9191 e901 e912 a913 

e40 1.9 .F95 .99e ' .980 .984 1.002 e997 e988 e992 

e59 1.0 1.G13 ,962 1.004 e975 le022 e986 le013 a981 

e76 le(! .GOO 1.012 lap33 e3dO e9Y2 1.025 e000 1.014 1.037 e000 le005 le034 

*94 1.0 1.04s 1.c42 1.035 1.029 1.057 1.043 1.047 le039 

1.12 1eC 1.013 1.020 e991 1.003 1.023 e987 le014 le025 e094 le008 1.027 a988 

1.30 le0 1.011 e000 1e0~5 e000 1.013 1.018 la012 e000 

1.48 1.0 1.023 1.021 1.015 1.006 1.020 1.025 1.020 1.022 

le84 1.0 a952 .94 9 .963 e958 

2.20 1.0 .973 e943 1.129 .362 e926 1.144 .973 .947 la145 .970 a942 1.150 

12.56 la0 e988 .9&1 e 997 e 990 

e22 le0 a977 -96.9 , -969 a977 e9091 ,979 e989 I e973 0985 

2.92 1.0 e980 1.011 e975 .?99 a982 1.018 e983 1.011 

13.28 le0 e9d5 I a975 I -989, .983 

\ 
'I 

1.046 1.039 

1.012 1.018 e991 

1.007 .ooo 

1.012 1.022 

.953 

0981 0943 1.137 

986 

e982 1.007 

a991 

TABLE B-1. (Continued) 

1.367 1.036 1.051 1.033 1.063 1.042 

1.OC9 1.032 o993'1.009 1.013 o99211.020 1.020 .999 

1.014 .ooo 1.005 1.016 1.010 1.023 

1.025 10020 1.007 1.018 1.013 1.028 

.351 0955 ,959 

e969 0945 1.132 0986 a943 1.122 e986 .948 1.131 

0969 e962 986 

-966 1.008 0979 1.002 

.F&O .991 0995 

a986 1.019 

(A) COEtTINUED. 

X/D R/R' 5=0 =60 =le0 8=0 =60 =180 0=0 =60 =180 0=0 =60 =180 

TEST 19 RUk 123/0 TEST 19 RUN 203/0 TEST 19 RUN 1O3/0 TEST 1, RUN 146/0 

9 .52 .729 .722 e726 .715 .739 0727 0729 e725 

0 .E4 a712 0712 0722 e705 0707 0717 e716 a717 e725 0712 e714 a721 

a22 1.0 e986 -956 -970 .981 a977 ,989 0972 a982 

.40 1.0 1.013 .997 .9d2 a987 .999 .997 e995 e990 

.5e 1.0 1.023 0991 1.0C5 .976 1.016 ,984 1,014 .977 

e76 1.0 e000 1.024 1.039 .COO 0999 1.025 e000 1.016 1.032 ,000 1.009 1oC29 

094 1.0 1.061 1.043 1.041 1.031 1.052 1.042 1.054 1.034 

.!I3 1.0 .910 .926 .921 .890 .9O6 .908 .902 ,917 .917 1.250 .913 0912 

1.12 1.B 1.019 1.02C 0998 1.002 1.C19 0968 1.013 1.027 ,996 1.007 1.019 e988 

1.30 1.0 1.014 1.023 1.OG6 e000 1.013 a000 1.006 1.012 

1.48 1.0 1.019 1.030 1.015 1.007 1.024 1.022 1.019 1.020 

1.34 1.0 a960 .Q44 0955 a951 

2.20 1.C a986 a948 1.135 ,762 a926 1.136 ,977 e943 2.765 .972 ,939 2.766 

2.56 1.0 .986 . 976 ,985 a 982 

2.92 1.0 .sa9 1.015 .978 1.000 0985 1.014 e976 1.008 

3.29 1.0 0997 e 976 .990 . 98 1 

3 052 

0 .t4 

.03 1.0 

022 1.0 

040 1.0 

e59 1.0 

e76 00 

.94 00 

012 00 

.30 .o 

043 .o 

1.64 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

3.28 1.0 
TABLE B-1. ( Continued) 

X/D R/R 

0 e52 

0 .b4 

003 1.0 

022 1.0 

e40 1.0 

.5P 1.0 

076 1.0 

.94 1.0 

1.12 1.0 

,1.30 1.0 

1.46 1.0 

1.64 1.0 

2.29 1.0 

82.56 1.0 

0=3 =60 =180 

TEST 1, RUN 2O2/O 

.E20 -811 

e799 ,801 o81C 

0901 -917 o9C9 

e969 -961 

.9&t e9b6 

1.003 ,979 

.OOC 1.003 1.026 

1.046 1.033 

1.002 1.017 e991 

1.004 e000 

1.010 1.006 

.942 

e968 e930 1.136 

.978 

2.92 1.0 e979 1.060 

(A) COtrtTIN 

0=0 =60 =180 

TEST 1, RUN 16710 

mQi9 e810 

.8O5 0802 .814 

.934 e931 e915 

.9E2 .994 

1.034 ,979 

1.315 .992 

e3UO 1.020 1.023 

1,342 1.037 

1.006 1.017 .995 

1.30E .ooo 

1.010 1.018 

.957 

ED. 

0=0 =60 =180 

TEST 19 RUN 161/0 

,883 .e79 

0867 e868 e875 

,924 e932 e924 

e977 a982 

e983 e990 

1.011 e982 

e000 1.002 1.032 

1.044 1.033 

1.010 1.032 a997 

1.011 .ooo 

TEST 1, RUN 2O1/O 

a883 a873 

a862 me64 as72 

.915 0928 a915 

a969 a982 

0989 0984 

1.001 0977 

o000 1.005 1.024 

1.045 1.031 

1.002 1.019 e992 

1.004 .Ob0 

1.022 1.01E ~1.013 1.010 

0956 .941 

-967 -945 1.124 a96F 0943 1.133 e966 e932 1.134 

Fb6 ’ .992 ,977 

-982 1.003 ,962 1.OOL a976 1.003 

.9Y7 .975 .978 

TEST 1, RUN 14P/O TEST 1, RUN IZI/O 

o .52 .879 .a74 ea97 e992 

0 m84 0864 e863 a872 e882 0882 *890 

003 1.0. e921 9939 a916 -930 0947 0926 

022 1.0 -974 0981 a983 -994 

040 la0 a996 e988 1.010 e992 

.5E 1.0 1.010 -978 1.017 a991 

076 100 e000 1.010 1.027 aOGO 1.024 1.035 

e94 1.0 1.046 1.032 1.056 1.040 

1.12 1.0 1.006 1.018 e989 1.016 1.022 .995 

1.30 1.0 1.005 1.011 1.010 1.022 

1.48 1.0 1.014 1.019 1.019 1.029 

lad4 1.0 a951 .959 

2.20 1.0 e975 0940 1.124 e983 .946 1.131 

2.56 1.0 a982 0961 

2.92 1.0 e977 1.005 -378 1.012 

,.3.28 1.0,, .933 . 988 

TEST 1, RUN lbE/O TEST 19 RUN 120/O 

.e96 .P84 .966 .963 

a875 a874 ob85 0952 0953 e961 

e931 .945 .920 a957 0967 a940 

0986 0994 m981 0990 

1.004 e976 a996 ,995 

1.016 0991 1.016 a984 

0000 1.020 1.025 e000 1.013 la036 

1.042 1.038 1.059 1.039 

1.009 1.019 0995 1.010 1.025 “793 

1.007 .OOO 1.013 1.017 

1.007 1.016 1.022 1.022 

0957 0952 

0987 0947 1.126 ,972 .942 1.142 

0967 984 

e984 1.004 e980 1.016 

0993 .979 
1 

040 1.0~ 0931 ,978 .903 1.024 0983 1,014 

e56 1.0 0940 -968 0989 1.036 ! 0984 1.025 

.76 1.0 .OOO -942 1.026 .030 1.013 1.065 .OOO .978 1.059 

' 094 1.0 0904 e899 0929 0943 e917 0923 

~1.30 1.0 0933 e000 0952 .ooo .954 ,944 

1.48 1.0 0933 a891 0959 0927 e965 e914, 

1.84 1.0 0919 .970 s951 

2.20 1.0 a919 -904 0932 0953 0945 a971 a948 a931 0965 

2.56 1.0 0950 .9b4 .985 

2.92 1.0 096C 0967 0994 1.02c 0992 0988 

;lo12 1.0 0883 .9G4 1.102; 8928 0943 1.133 e911 ,937 1.145 

.3.2a 1.0 .965 1 e000 .987 

TABLE B-1. ( Continued) 

0964 1.021 

-952 1.005 

.OOO .965 1.059 

me .92a 

,978 .coo 

-917 a937 1.150 

m957 0919 

. 944 

0952 m937 e966 

,992 

0994 0976 

1.002 
W 

0 

1.12 1.0 

1.30 1.0 

TABLE B-1. ( Continued) 

$=O =60 =180 

TEST 1, RUN 166/0 

a761 e787 

w769 e779 .77? 

.95a .w7 1.066 

1.021 1.027 

.991 1.021 

a976 1.032 

e000 1eOOL 1.066 

e931 e942 

a938 e940 1.129 

0946 a000 

a962 ,928 

s962 

.954 .941 .974 

:*56 1.0, e979 

!.92 l.O/l.OGG 1.014 

5.28 1.0 

9 e52 

0 .ti4 

.03 l,o 

.22 1.0 

.40 le0 

.5R 1.0 

-76 1.0 

e94 1.0 

1.12 1.0 

1.30 1.0 

1-48 1.0 

1.84 1.0 

2.20 1.0 

2.56 1.0 

2.32 1.0 

3e28 1.0 

1 .GO1 

TEST 1, RUN 127/0 

a896 m893 

.867 a877 .R75 

e963 ,969 1.042 

0993 1.013 

e975 1.042 

a949 1.000 

a000 e971 1.062 

.931 e944 

e943 a936 1.151 

e989 e934 

-939 ,926 

e938 

a962 a939 .98( 

8971 

a998 e976 

1,011 

(A) CONTIN 

0=G =60 =180 

'EST 1, RUN 

.796 .aoo 

.77a .7a9 

0362 a960 

a014 1.000 

,964 le019 

e785 1.021 

26/0 

. 784 

.047 

ED. 

B=O =60 =180 

TEST 1, RUN 207/0 

e845 0845 

e820 e830 .826 

e940 0938 1.017 

e971 a972 

e943 ,997 

e918 0971 

e000 0972 1.058, a000 a939 1.031 

0917 a922 

e918 0939 le151 

a966 e940 

,967 ~918 

.9&9 

,950 *931 m964 

*981 

a907 m991 

.3Y2 

'EST 1, RUk 20J?/o 

m9b7 a908 s914 

s944 e946 1.013 

a931 0990 

0947 a996 

.905 e955 

a000 ,939 1.025 

e911 ,907 

a935 .ooo 

e302 

a933 0919 .945 

,924 

.959 .947 

.984 

.937 .928 

.93i .a92 1.098 

,013 .89a 

e902 0905 

m902 a918 1.119 

0959 .GOO 

0918 eR98 

e317 

s932 e917 .939 

e956 

e964 *947 

0974 

lEST 1, RUN 168lC 

.97R .971 

,948 8953 e955 

e979 .907 1.052 

m991 1.027 

0980 1.050 

e946 1.002 

a000 ,978 1.065 

a938 e958 

e956 a935 1.141 

.990 a000 

e938 e934 

. 934 

e964 e942 .98' 

e969 

1.003 0981 

1 e016 

0=0 =60 =le0 

'EST 1, RUN 167/0 

.e88 .a92 

,866 .a75 ,872 

,971 .971 1.060 

,002 1.015 

,977 1.044 

,958 1.013 

a000 e978 1.067 

m930 m943 

e939 e948 1.165 

0992 e000 

a958 e927 

0 949 

,959 e945 a976 

.999 .984 

e980 ! 

I .017 1 

lEST 1, RUN 128/0! 

.9ao .973 

.953 -957 .95a 

a975 e981 1.050 

0985 1.013 

a966 1,040 

-943 8990 

1 

-000 .96a 1.059 

,928 e948 

,947 0934 1.145; 

e986 a934 

0936 m928 ! 

m927 1 

e957 e933 e976; 

.959 

.997 a970 

1.01 1 
7 

TABLE B-1. (Continued) 

TEST I, RUN 209/0 

'3 e52 ,998 e989 

0 e64 e968 e968 e973 

e03 le0 e965 e969 le008 

e22 le0 e926 e992 

e40 le0 e944 e990 

.sa 1.0 e907 .955 

e76 1.0 e000 e937 le023 

e94 le0 e916 -897 

le12 le0 e931 e889 1.089 

le30 le0 e930 e000 

1.45 1.0 e915 e892 

1.34 le0 e902 

2.20 le0 e935 e922 4.596 

2-56 le0 a919 

2.92 la0 e942 e944 

3.28 le0, e985 

3 e52 

0 e84 

e03 1.0 

e22 la0 

-40 1.0 

e58 le0 

e76 le0 

e94 le0 

le12 le0 

1.30 1.0 

1.45 1.0 

1-84 le0 

Lei0 le0 

2.56 le0 

2.92 1.0 

3.28 le0 

TEST 1, RUN 134/0 

.GOO a577 

e558 ,568 a574 

e994 e939 e994 

1.009 e000 

le012 e951 

eC0C ,957 

eCOC e959 e966 

-COO e943 

e985 e990 e926 

le016 le009 

e976 e991 

1. cu9 

le007 e997 e74C 

e96G 

e992 e985 

1 e002 

TEST 1, RUN 129/0 

le024 le015 

e995 .;9Y7 e997 

e967 1:004 le022 

e977 1.036 

m977 1.029 

.Q43 e989 

eOU0 e971 le060 

e939 e940 

e957 e924 1.134 

e964 e935 

e931 e925 

e922 

.QS5 e936 e984 

.944 

e995 e974 

1.014 

TEST 1, RUN ZIO/O 

et26 e602 

-585 ,585 e604 

,966 e926 e965 

e992 e935 

-998 e933 

1.012 e939 

eOb0 e941 e944 

-973 e924 

e974 e976 e932 

1eOG2 e000 

.FcO .979 

.9$Z 

e953 e987 e720 

e 943 

e972 e973 

e964 

ED. 

16~0 =60 =190, 0=0 =60 =180 ~ 

TEST 1, RUN 16910 TEST 1, RUN 21E/O 

le028 le023 

1eOGO le003 1,005 

e995 le007 le052 

e982 le038 

e986 1.052 

e951 le004 

e000 e960 le069 

e944 e958 

e968 e932 la146 

e979 e000 

e946 m939 

e937 

e970 e948 e986 

a958 

le004 e985 

1 e022 

TEST 1, RUN 133/0 

*COO m746 

e716 m722 e730 

e993 e941 le000 

le006 e000 

le010 m951 

e000 e958 

eOC0 e958 e969 

e000 e943 

e985 e968 e928 

le012 1.008 

e973 e990 

1 e005 

le004 e998 e743 

e957 

e987 e986 

1 e000 

,177 e180 

e182 e221 e209 

le070 e927 e961 

e993 ,938 

e997 m936 

e995 m941 

e000 e946 eo39 

e946 e927 

e976 e973 e902 

le001 e992 

e966 m979 

e 995 

a995 e990 e713 

e 948 

m976 e974 

-990 

TEST 1, RUN 211/0 

e784 e750 

,725 e726 e740 

e964 0925 mF87 

m990 e936 

e998 e933 

le021 e940 

e000 e940 e942 

e991 e926 

e977 e980 m8Y8 

1.002 e000 

e965 e984 

e 994 

,992 e989 e723 

e 947 

e973 ,975 

e 984 
TABLE B-1. (Continued) 

e967 

e995 

X/D R/R 

eo3 1.0 

I 022 1.0 

i .40 1.0 

a990 .984 a996 

e994 b943 e996 

1.002 ,000 

1.307 e948 

eo00 ,954 

d=O =60 =180 

TEST 1, RUk 132/0 

e000 0861 

e822 -823 -830 

e997 ,943 e998 

1.007 .ooo 

1.013 -952 

c) -64 

a03 le0 

m22 1.0 

a58 1.GI eOOG -958 

076 1.01 aOGO a960 "770 

~ .94 1-01 DO00 .945 

'1.12 1-GI .986 ,990 .92P 

i1.30 le0,leO1& 1.011 

1.4R 1.0 .97f, -997 

e967 ,952 

e985 .936 

e996 ,940 

.- .- .-- 

1.54 1.0 

2.20 1.0 

'2.56 1.0 

11.84 1.011.001 

'2-20 l.O1 e997 ,995 ,720 

2.56 1.0: ,945 

- . . - - . . - 1.011 

l.CO9 1.002 -741 

902 

1 .Ob6 

1.3C3 ,996 e739 1.OOe e976 .726 

.955 e961 

,983 .985 .9ai .992 

,997 1 a009 1 eo10 

(A) CONTIN 

0=0 =6G =180 

TEST 1, HUlv 212/2 

m924 e904 

-954 e924 a994 

e993 e935 

9997 e935 

1.0irO ,942 

*Ob0 m944 e940 

1.027 ,932 

S987 ,976 e888 

1.006 ,000 

ED e 

0=0 =60 =180 

TEST 1, RUN 131/0 

eooo 0949 

m907 e903 a915 

a994 e943 1.001 

1.002 .ooo 

1.008 .951 

.ooo a957 

e000 ,940 

'e000 ,956 e968 

.983 ,989 -926' 

0=0 =60 =1gO 

TEST 1, RUN 213/0 

e973 e943 

e911 e899 e909 

.979 a929 a993 

0991 e938 ! 

a998 e935 

1.027 e942 

e000 0941 a947 

e995 s923 

-974 .985 -899 

le010 1.009 ,le004 SO00 

.9a4 -991 I 0972 m992 

1 .OL2 i 1 a007 

e396 a998 ..702'1.002 a999 e743 

-971 1 e954 

a964 e986 

e995 

e991 m992 e723 

.943 

12-92 1.01 e983 .98E 1 .984 .9d0 il::;? .987 i -975 -980 

3.28 1.0 1.001 , ,969 1 -985 

I I 

TEST 1, RUN 709/0 TEST 1, RUN 702/0 

a000 a000 j ,000 eooo 

m939 -876 ,891 a928 e877 e882 

0971 093'5 1.040' e968 a933 1.012, 

,979 ,940 ' .972 .936 

e983 e949 .977 .947 

e979 .957 .974 .954 

.983 a962 3.823 e977 e960 ,984 

a955 b961 a952 e957 

.963 .986 -9231 a976 .9&1 -919' 

1.018 e994 le014 e990 

.970 .944 ~ -963 .940 1 

1.011 j 1 e006 
TABLE B-1. (Continued) 

.&3 1.3' 

.59 1.6 

.76 1.3 

.94 1.c 

'1.12 1.3 

1.30 1.3 

1-44 1.0 

leb4 1.C 

2-29 1.0 

2.54 lo@ 

2.92 1.0 

3.23 1.0 

.F7i ,941 ,976 .957 o9Zl 0956 e981 e961 

.St? .a41 0972 e946 e976 0944 0977 a951 

037; ,947 7,eEZl .976 e951 e961; 0977 0949 3.822 0980 0956 3.753 

0942 .344 .949 .94E 0961 0942 0959 0950 

1.GC5 .98C 1.014 0989 1.016 e997 1.017 0992 

0947 e922 .7cC 0938 0965 0944 0966 a942 

.Sbs ,9tF. .933 .374 .V77 .91j .978 .984 .a96 .980 .981 .919 

.9?C 1.3116 1.006 1.007 

0995 -963 o7CC 10302 0972 ,712 1.002 0977 e693 1.004 0976 0716 

.93i .948 0952 .950 

-967 e980 .97F 0967 0977 0995 0977 0994 

.FF$ 1.210 1 .oco 1 e007 
X/D R/R $=o =bo =18o 

0 052 a000 0000 

0 m64 1.673 1.615 1.655 

a03 1.0 1.227 1.202 1.033 

-22 1.0 m962 -893 

TEST 1, RUN 713/0 

I 

g=o =bo =la0 0=o =60 =is0 0=0 =60 =a80 - 

*OGO a000 .ooo .ooo .ooo .ooo 

TEST 1, RUN 714/0 TEST 1, RUN 706/0 TEST 1, RUN 711/0 

1.717 1.515 1.597 1.670 1.651 1.637 1.765 1.510 1.625 

1.321 1.511 1.059,1.241 1.223 1.111 1.324 1.197 1.118 

e971 a921 , e971 e924 1 

'I .968 m897 

e40 1.0 e975 0951 ' .978 .95a m962 s968 , a986 a956 

2.56 1.0 m935 - 

2.92 1.01 .972 .9a2 

3.28 1.01 *999 , 1 .005 

1 

.945 i s933 

e979 ,996 ; .975 .993 

1 SO07 ,I .oe2 

I . 

0 *64(1*554 1.533 1.5081 e937 e000 a907 

a03 1.013.821 1.182 1.042 e300 a933 

a22 1*0/ e972 e910 1 :;:; .964 

I sa 1.0' .976 .948 ' m9d6 e986 

e40 1.01 ,980 a968 I .9ao .979 

m823 e000 e8181 e827 moo0 m.830 

e871 *OGO a8821 e876 moo0 ,802 

e943 a942 , a940 m938 

.977 ,976 : a972 a981 

a966 s967 j a962 e962 

.708 

.973 968 975 

.967 .958 1.050 .964 .953 1.048. .970 .963 1.051 

96 1 .955 965 

e969 a967 '1 .967 .966 0961 e971 

9d4 1 .981 1; .975 
TABLE B-1. ( Continued) 

W 

cn 

(A) CONTIN 

X/D Q/R; d=O =60 =180 , 0=0 =6(r =180 

TEST 1, RUN 519/0'TEST 1, RbN 540/0 

0 .84 .857 0000 .e62 .367 0000 0874 

022 1.0 0951 e950 .955 .951 

0 052 e860 e870 0871 0876 

003 1.0 a893 e000 a904 e396 a000 0909 

040 1.0 a971 e972 8972 0972 

058 1.0 0981 0982 o95C 0981 

-76 1.0 0966 0990 1.017 0967 ,987 1.016 

094 1.0 1.001 1.000 .999 0997 

1.12 1.0 

1.30 1.0 

1.48 1.0 

1.64 1.0 

2.20 1.0 

2.56 1.0 

2.32 1.0 

3.28 1.0 

0 052 

0 084 

.d3 1.0 

022 1.0 

040 1.0 

058 1.0 

076 1.0 

094 1.0 

1.12 1.0 

1.30 1.0 

1.4E 1.0 

lad4 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

3.28 1.0 

0963 0993 1.031 0979 0931 1.029 

0585 -991 0964 0989 

0972 e972 ,970 .970 

.ooc .9tF 

.967 .955 1.04F .961' .951 1.042 

0961 .955 

0966 e968 e964 0961 

983 m980 

rEST 1, RUN 53910 

,917 0926 

e913 e000 -924 

0931 .ooo .94L 

0969 e969 

0963 -984 

0989 0989 

0992 0995 1.022 

1.006 1.004 

.FE3 ,994 1.035 

.988 .992 

0974 .973 

.97c 

e965 e952 1.042 

0957 

0966 0964 

0983 

TEST I, RU~ 53810 

.954 .ooo -968 

,947 0960 

.944 .OdO 0953 

o9GO 0982 

.990 0994 

.995 0997 

-996 1.002 1.026 

1.010 1.009 

0985 0997 1.037 

0990 0994 

0976 .97c 

0172 

-968 0955 1.045 

0959 

0967 0967 

0964 

ED. 

0=0 =60 =180 Ej=O =60 =180 

TEST I, RUN 55010 TEST I, RUN 51810 

.a92 .896 .965 .a71 

.909 .ooo .923 .a95 .ooo .go8 

0985 0983 .9a2 mi 

0887 e000 0897 0864 e000 0869 

,963 a963 0954 e951 

0979 0979 0972 ,973 

0992 e992 1.021 0986 0991 1.017 

1.002 1.001 1.003 1.000 

.980 .997 1.028 

.991 0997 

0975 0977 

. 974 

0967 0962 1.043 

m961 

e975 a969 

0985 

TEST 1, RUN 552/0 

0749 0751 

.753 .ooo -779 

0902 moo0 e921 

.975 .9a4 

0936 1.002 

1.010 -989 

1.011 1.008 1.032 

1.053 1.044 

1.011'1.041 1.011 

1.016 1.025 

1.013 1.010 

e952 

0963 0931 le150 

0976 

0983 1.008 

.987 

e982 a995 1.032 

0985 0991 

0973 0974 

. 000 

,966 e950 1.046 

.9sa 

0965 0967 

0984 

TEST 1, RUN 533/0 

.sa0 .576 

e568 a000 ,579 

.902 .OOO .917 

0976 0978 

0984 0996 

1.002 0981 

1.005 1.000 1.022 

1.049 1.036 

1.005 1.033 1.015 

1.008 1.019 

1.012 1.000 

0932 

,953 a919 1.140 

972 

,977 1.000 

.9ao 
W 

Q, 

X/D R/R 0=0 =le0 0=0 =60 =180 0=0 =60 =I80 

TEST 1, RUN 534/0 TEST 1, RUN 535/0 TEST 1, RUN 520/0 

0 .52 e687 a679 a689 .678 .741 ,732 

0 .84 ,667 .OOO .678 .671 .OOO .679 .722 .OOO .728 

-03 1.0 a902 -000 .910 0902 ,000 .910! a907 0000 ,917 

a22 1.Oi ,978 .984 ' .9EO ,987 1 .982 .990 

0=0 =60 =180 

TEST 1, RUN 517/0 

a745 .735 

a725 .OOO .730 

e919 a000 a917 

.990 .990 

a40 1.0 1.000 .989 1.004 0967 1.006 a997 

; .58 1.0 1.00; .985 1.003 e986 1.007 a988 , 

I -94 1.0.1.052 1.037 ,le050 1.036 !1.059 1.037 

1.12 1.0 1.00E 1.026 1.015/1.009 1.020 1.014;1.005 1.026 1.015 

1.052 1.040 

1.003 1.022 1.015 

1.30 1.0 1.002 1.015 11.003 1.017 11.007 1.021 .lo000 1.033 

1.48 1.01 .99& 1.001 ~ ,099 1.000 /1.005 1.CO5 I .988 .996 

1.66 1.oi .F37 0940 i e000 I .ooo 1 

2.20 1.0 924 1.l76I ,970 ,926 1.135; ,969 ,925 1.135i .982 .933 1.139, 

a58 1.0 1.013 ,998 

e76 1.0 1.025 1.027 1.033 

1.003 0981 ,la006 a994 a961 1.007 1 

1.012 1.012 1.02111.020 1.023 1.022 .959 1.005 1.061' 

2.20 1.0 .978 a936 1.136 .924 1.134 

2.56 1.0 ,980 

2.92 1.01 .980 1.013 0971 1.001 e974 1.003 

.985 992 

a941 a933 s490 

e951 

.997 1.007 

1.001 
TAB LE B-1 . ( Continued) 

0 e52 

0 e84 

e33 le0 

e22 le0 

e40 le0 

e58 le0 

-76 le0 

e94 le0 

1.12 le0 

le30 le0 

1.45 1.0 

le04 le0 

2.20 le0 

2.56 le0 

imY2 le0 

3.2P 1.0 

0 e52 

3 e64 

-03 le0 

e22 le0 

a40 1eC 

e58 le0 

e76 le0 

e94 le0 

le12 le0 

le30 le0 

le48 le0 

le64 IeC' 

2.20 le0 

2.56 le0 

2.92 le0 

3.25 le0 

-t 

TEST 1, RUN 532/0 

e613 e623 

.COG e3CO e612 

e946 e000 1.044 

.991 1.016 

1.007 1.016 

e967 1.013 

e97L 1eCOC le069 

e967 e984 

e936 e957 le128 

e938 e937 

e935 e911 

eG55 

eC50 e923 -996 

e931 

e986 1.005 

1 e033 

TEST 1, RUN 53?/0 

e816 -817 

e788 SO00 e796 

e967 e000 1.063 

le015 le008 

a957 le033 

e947 1.036 

e936 e990 1.081 

e946 e951 

e918 e952 1.148 

e963 e937 

.F57 e906 

e951 

e952 e932 e973 

.9dS 

e997 e997 

1 e009 

TEST 1, RUN 531/0 

e739 e735 

0718 e000 e730 

,954 e000 le074 

le316 le522 

e996 le030 

e369 le030 

e932 e997 le073 

e344 e943 

e912 e945 le129 

e953 e954 

-344 e310 

.945 

e940 e916 e975 

e 975 

1.000 le005 

1.01c -I 

TEST 19 RUN 516/0 TEST 1, RUN 521/0 

e783 e764 e796 e795 

e753 e000 e764 e769 e000 e778 

e963 e000 le068 e969 e000 le059 

le026 le013 le012 le003 

e972 le019 e958 le020 

e962 1.026 e956 le029 

e036 e985 le073 e937 e973 1.072 

e946 e933 e936 e932 

e911 e951 1.140 e910 e952 le151 

e957 e952 -970 e941 

e957 e903 e952 e.906 

e000 e 000 

e946 e926 e979 e945 e924 e978 

e 982 e 983 

e997 le013 , e992 le000 

1.006 ~ 1 e005 

TESl 19 RUk 548/0 

e854 -849 

ecY29 eC00 e829 

e971 e000 le066 

le006 le002 

.977 1.037 

.940 .999 

e326 -968 le077 

,942 .937 

e334 eo59 le159 

e953 e941 

.951 e914 

e337 

e956 e938 e974 

.978 

e996 e977 

1 a019 

TEST 1, RUN 529/0 

ea93 ea92 

ea69 eo00 e867 

.964 e000 le066 

-985 le025 

e982 1.054 

e926 le005 

e940 e985 le072 

e954 e964 

e953 e942 le158 

e984 e936 

'e93F! e916 

e930 

e904 e936 e982 

e956 

e996 e971 

11 e 024 

TEST 19 RUN 528/0 

e942 e941 

e920 e000 e910 

e975 e000 le065 

e980 le028 

e983 1,054 

e949 e984 le070 

e926 le002 

e957 e963 

e959 e939 le155 

e974 e939 

e938 -920 

e926 

e962 e936 e989 

e 949 

e986 e977 

1.028 
CD 

M 

0=0 =60 =180 

TEST 1, RUN 55410 

.257 .392 

a262 e000 m308 

m973 e000 e987 

,998 a952 

TAB LE B-1 . ( Continued) 

g=O =bO =180 

TEST 1, RUN 523/1 

a497 s562 

e478 .OOO e487 

.972 ,000 1.000 

a996 a951 

X/D R/R 

9 e52 

0 .b4 

.03 1.0 

022 1.0 

.40 1.0 

a58 1.0 

*76 1.0 

.94 1.0 

1.12 1.0 

1.30 1.0 

1,001 .959 ,999 .958 

a936 e962 

1.003 e972 e902 

.Fa5 .971 

.98E .987 .QZt 

1.019 e998 

0 a52 

0 eb4 

mG3 1.0 

.i2 1.0 

.4@ 1.0 

.54 1.0 

a76 1.0 

094 1.0 

1.12 1.0 

1.68 1.C 

1.64 1.c 

2.20 1.c 

1.30 1.a 

leks 1.01 .9tc .973 

1 .a4 1 .o 11.ClOt 

2.20 1.O;l.COb e586 -725 

2.56 1.0, a959 

.994 .9b9 

I a026 

lEST 1, RUh 515/C 

e700 .757 

a661 e000 0662 

.975 -000 1.000 

m999 e961 

a996 ,965 

e992 .972 

a992 e992 .93C 

1.020 1.002 

m96E e979 

.ooo 

960 

1.024 

b999 .952 

1.004 e975 ,967 

1.00b ,992 e725 

.992 ,992 

b995 

1.004 

.993 

.957 

1.020 

8967 

eo30 

I a007 

,379 

-992 

I a024 

. 964 

m972 ,978 

. 959 

m994 a925 

1 e003 

e978 

e990 3.820 

.991 

TEST 1, RUN 546/0 

.709 .%14 

0747 a000 ,745 

-972 .coo 1.007 

-998 m952 

a939 a958 

.?94 .F62 

1.005 .971 .975 

m397 ,968 

.991 e995 .915 

1.024 1.005 

e371 .979 

eOGG 

.357 

.991 .F92 

1 e024 

1.0'27 .99C e717 

.De 

0=0 =60 =180 

'EST 1, RUN 524/0 

a668 m705 

0640 e000 ,640 

.971 a000 1.009 

,997 a951 

,998 .95R 

a995 a962 

1.003 a970 a977 

a995 .969 

.991 a993 .919 

1.021 1.002 

,971 a978 

e 000 

.955 

1.023 

1.006 0990 a716 

,990 b993 

TEST 1, RUN 547/C 

.833 a870 

.792 .ooo .79c 

e996 s950 

s996 eo58 

e992 a961 

0971 . .ooo 1.021 

1.003 *970 .97E 

e994 .965 

a997 1.003 a915 

1.027 1.012 

-973 a986 

so00 

1.006 m993 a71i 

.95a 

1.028 

m995 ,990 

P=O =60 =le0 

rEST 1, RUN 52210 

0717 e756 

a975 .ooo 1.001 

0998 a951 

e997 m961 

s994 .965 

,677 .ooo .67a 

1.003 a973 ,980 

a993 .972 

a989 a993 a927 

1.020 1.003 

,966 .979 

. 000 

,956 

,990 .993 

1.007 e991 e726 

1 a023 

TEST 1, RUN 525/C 

a773 .805 

a728 a000 e734 

0974 .ooo 1.008 

a998 a950 

.99A .957 

,993 e960 

1.002 b970 e977 

.994 .965 

a989 ,992 e923 

e967 0977 1 

eo00 

e956 

a990 0992 

1.022 

1.021 1.003 

1.006 ,989 e720 
TABLE B-1. (Continued) 

X/D R/A 

0 e52 

0 e84 

eo3 1.0 

022 1.0 

e40 1ec 

058 1.0 

e76 1.0 

eY4 1.0 

1.12 1.0 

1.30 le0 

1.48 le0 

1.84 le0 

2,20 1.0 

2.56 1.0 

2.92 le0 

3.23 le0 

TEST 1, RUN 526/0 

.66? .873 

.El0 -000 .a16 

0979 eC00 1.015 

1.004 e958 

le005 0965 

le001 e966 

1.010 0977 0986 

le003 e974 

e99& e998 e925 

1.026 1.006 

.977 .9a3 

.GOO 

10C12 e994 0721 

966 

a997 0996 

1 e026 

TEST 1, RUN 52710 

e914 0926 

0851 ‘bo00 e858 

0980 .ooo 1.011 

leO(r5 e456 

1e0.05 e964 

le061 e966 

1.008 e975 a983 

1.093 e973 

e997 e998 e926 

1.027 le008 

e973 e9az 

. 000 

. $6 3 

1.011 e993 ,721 

e996 e996 

1.026 

CD 

CD 
TABLE B-1. ( Continued) 

. GO6 

.624 .7o3 

*9C6 HUN 

(R) blA2 

XID RIRI 0=0 =60 1 fl=o =co I g=O =60 

ITEST z ITEST 2 ITEST 2 

e655 

.c4a .65i 

.av3 RUN 

0 .52 .519 

0 .&&I .SI1 .517 

-03 I.Oi e904 RUN 

e33 1.0 e957 32IO 

1.030 13a/o 

boo0 

rEST 6 

0912 m926 

e918 a925 

e67 1.0 .951 

0 .52 .ooo 

c .b4 .513 .ooo 

a03 1.0' .cg& RbN 

.33 1.0 1.615 4F/l 

.67 1.0 .COG 

TEST 2 

. OCO ~ 

' 

- .coo ~ .9L1 

TEST 2 ~TEST 2 

3 -521 .GC3 .OOO 

ow3 1.011.352 RUN 

3 eC4'1.536 1.433 

e33 1.0 1.341 23710 

.uo; I .ooo 

e281 .OCC 1 a435 9481 

-969 RUN /1.111 RUN 

1.006 4912 :1.156 50/0 

067 1.0. .OOG 

:TEST 6 

0 

0' 

a03 

33 

e67 

0 

0 

.03 

033 

,521 a971 

m84, e9SU 

1.0 1.ooc 

TEST 2 

,737 ' .957 

e976 

.9S3 

KUN 

5 

.706 

RUN 

47IO 

e707 

.67 1.0/1.002 

ITEST 2 

3 

3 :::I .318 i!:i 

.33 1.0 0920 

.33 1.0 .949 48/2 

e67 1.0 -000 

eo00 .OOG 

1.626 *GOO 

1.374 RUN 

1.431 233/0 

.ooo 

fE S T 6 

e942 e945 

-952 .953 

e955 RUN 

e992 5 

1.000 

lEST 2 

,711 

e705 .72: 

0986 RUN 

1.017 4711 

1 e015 

TEST 2 

oUOG 

a783 .COG 

m695 RGN 

m969 16110 

. 000 

a000 

rtST 6 

.97a .we 

0987 6985 

e934 RUN 

.99e 8 

1 a005 

TEST b 

a912 a919 

8921 a929 

a922 RUN 

8 995 

TEST 2 

.977 ia 

.6a8 

,728 ,697 

a955 RUN 

a994 47I2 

1 e007 

TEST 2 

eo00 

1.523 1.557 

1.365 RUN 

1.237 261IO 

moo0 

g=o =tlo 

TEST 2 

.774 

.763 a762 

m.904 RUN 

a969 3510 

,906 

TEST 2 

.ooo 

m505 0000 

e958 RUN 

1.047 13610 

,000 

TEST 6 

e963 e963 

e968 a966 

.971 RUN 

m995 8 

1.004 

TEST 6 

.845 

.a69 RUN 

a969 18 

. 993 

TEST 2 

.a47 .a50 

630 

e619 e626 

mOOO RUN 

-922 7.210 

.907 

TEST 6 

. 970 

e976 a979 

a972 RUN 

.991 11 

m992 

g=O =60 

rEST 2 

,765 

e764 .7b2 

.go8 RUN 

.925 

TEST 2 

a954 34/0 

. 000 

a708 a731 

m952 RUN 

1.018 13710 

moo0 

TEST 6 

a912 e922 

.927 .937 

,920 RUN 

.98l 21 

1 .ooo 

TEST 6 

a788 0791 

a807 ,807 

*899 RUN 

a985 1512 

962 

TEST 2 

so00 

a364 a000 

-912 RUN 

,975 4810 

eo00 

TEST 6 

.957 

b94Q e955 

m954 RUN 

e989 11 

.995 

.OOb 

.2a2 .2ao 

aY65 RUN 

.054 4910 

.ooo 

'EST 2 

1 SO06 

rEST 6 

e640 0646 

e642 e650 

e804 RUN 

e992 15 

8962 

TEST 2 

.oou 

D341 .ooo 

0698 RUN 

e964 4811 

.ooo 

TEST 2 

523 

e595 .511 

.a88 RUN 

e926 2710 

e897 

, 

I 
TABLE B-1 . ( Continued) 

3 (8) COIUTINUED. 

X/D R/R 0=0 =6G , 0=0 =60 ,, 0=6 =60 " 0=0 =60 ' 0=0 =60 ' 0=0 =60 I 

TEST 2 'TEST 2 "TEST z TEST 2 TEST 2 TEST 2 

0 e52 -627 0716 .la1 e594 e821 1 a007 

003 1.0 .e67 KUh e847 RUN e638 RUN 1.007 RUN 1.025 RUh s996 RUN 

1) ob4 -609 .630 .bF6 -701 .201 .I73 .597 .528 .824 .778 1.005 .953 

.33 1.c .set mo ma 29/c, .a93 4112 .ooo 111 .ooo 210 .ooo 310 

067 1.0 *E95 ____~ e863 .9c7 __ 1 e048 1 SO96 1 e059 

TEST 2 TFST 6 TEST 6 TEST 6 TEST 6 TEST 6 

O -52 sC,OJ 1oC29 ,975 -97% -945 0954 e961 

3 sP4 1.C32 1.015 9979 .FEL e945 e961 a967 

so3 1.0 1.032 HUk e976 RUN e953 RUN e973 

.?3 1.0 .Gob 4/2 .994 24 .991 24 999 

a67 1.0 1.064 .995 0997 1.002 

3 e52 e791 a794 e626 .620 e976 e979 , -953 

3 .E4 mFO7 st07 st26 sc3U e963 e983 e956 

.G3 1.0 .e76 icuh s85F RLik .gal RUN .964 

a33 1.0 .F7? 56 e986 5t e995 27/? .992 

TEST 6 TEST 6 TEST 6 TEST 6 

a965 

s 962 

RUN 

37 

a961 

sY63 

RUN 

~~ 27 - 

a67 1.0 e959 -956 1 .ooo 1 .ooo 

TEST 6 TEST 6 TEST 6 TEST 2 

0 a52 

0 ob4 

so3 1.0 

033 1.0 

-67 1.0 

3 .5; 

0 a84 

SO? 1.0 

.33 1.0 

s67 1.0 

.717 

a699 -704 

sOOC RUN 

-882 70/0 

a907 

0000 ,000 

1.157 e300 

.972 HUN 

a972 163/0 

.ooo 

TEST 2 

.bid 

.ail .bo9 

0000 RUh 

a867 71/G 

s 899 

TEST 6 

-973 -376 

-976 e979 

.972 RUN 

a991 31 

e990 

so00 

0364 e900 

a912 RUN 

m975 48/0 

so00 

TtST C 

e949 e960 

a948 .955 

e954 RUN 

sFd9 31 

.992 

moo0 a706 

s737 a707 

a957 RUN 

.984 47/O 

1.002 

TEST 2 

. 000 

e341 so00 

0896 RUN 

e964 48/1 

.ooo 

TEST 6 

m965 e963 

e961 e967 

s965 RUN 

a992 66 

.996 - 

e908 s918 a858 a866 

a919 a929 ,857 sa61 

a913 RUN a670 RUN 

.976 43 a976 43 

s994 999 

TEST 6 'TEST 6 

e913 s920 

,922 a929 

a924 RUN 

a977 34 

.994 

TEST 2 

sOOC s711 

a705 s722 

a986 RUh 

1.017 47/1 

1 SO1 5 

TEST 2 

so00 

,318 .@OO 

s92O RUN 

e949 48/2 

so00 

TEST 6 

1.024 1.035 

1.023 1.025 

1.024 RUN 

1.031 40 

1 a030 

e845 ,845 

e845 a844 

e668 RUN 

a969 34 

,991 

1EST 2 

so00 s68b 

a728 a697 

e955 RUN 

a994 47/2 

1 SO07 

TEST 2 

1.004 

1.007 s989 

a000 RUN 

1.096 6212 

1 SO93 

rEST 6 

.901 a910 

sF09 e919 

e895 RUN 

a973 47 

e980 
TABLE B-1. (Concluded) 

X/D R/R 

0 a52 

0 e64 

a03 1.0 

.33 1.0 

a67 1.C, 

0=C =6G pI=O '60 0=0 =60 0=0 =60 $=0 =60 - =60 

TEST 6 TFST 6 TLST C 

0906 e907 *781 -786 ,779 .?87 

o9C4 e906 .do2 .dO& e732 e785 

*E95 KUN a872 RUN .aOa RUN 

.Fa6 47 a977 53 .9a7 53 

a991 0964 , a969 
TABLE B-2. BASE AND BODY SURFACE PRESSURE RATIOS (P/P ) FOR ORBITER GEOMETRY a, 

1.30 1.0' .993 .996 ' .990 1.000 00.37 0998 

1.48 1.G 0990 -9E5 ,077 0953 0976 e952 

led4 1.0 0993 . 979 0977 

2.20 1.0 0991 0992 1.016 a966 -361 1.054 0963 0958 1.041 

2.56 1.0 0992 960 a958 

2.52 1.0 0994 e000 -967 0300 0965 .000 

-3.28 1.0 0995 .Q75 0974 

a987 0997 

0974 0953 

0978 

a963 0960 1.040 

. 960 

-966 e000 

0975 
TABLE B-2. (Continued) 

.976 .997 1.028' 

. 3c3 .cuo . OOC . 000 

I 022 1.0, .COO 1,340 .ooo 1.343 

.978 .998 100251 

0=0 =60 =180 

TEST 3, RUN 208/0 

.ooo 

.ooo 

m763 .COO e000 

a000 0858 o000 

SO00 0950 

i .LO 1.6 0917 .95E 0366 e958 1 0969 ,959 

.5e l.C, .YB1 .983 .F78 .9b2 J -961 -983 I 

! .76 1.0; .984 .987 1.COL -9tS .986 1.0071 .986 .988 1.009 

0=0 =60 =le0 

TEST 39 RUN 2O5/O 

000 

.ooo 

0825 a000 o000 

a000 0873 a000 

a000 lo253 

0972 0962 

.~a3 .987 

.98a .992 1.012, 

'1.12 1.0: .974 .994 1.02S8 .976 .095 1.027 

/i.30 1.0 .9a3 .993 I .903 0995 

;lek8 1.0, e971 e950 1 0972 0952 

,7064 1.01 0976 ~ 0974 

:2.23 1.0' .961 .956 1.036 

12.56 1.01 .957 

12.92 1.0' 0963 -000 

13.28 1.0' 0972 - 

;TEST 3, RUN 218/O 

~ 0 0 .OGC 

I 3 .52/ .@OO 

I 3 .e4 

~ 003 1.0 

022 1.0 

' .kO 1.0 

.53 1.0 

076 1.0 

I .94 1.0 

1.12 1.0 

1.4? 1.0 

1.8k 1.0 

11.30 1.0 

3.28 1.0 

.coo 

1 .C13 

1.021 

1.02L 

1 0047 

1.010 

1.027 

o96Ea 

0985 

960 

.9ao 

0953 

0750 .ooo .ooc 

.GOO e906 e000 

-991 

0963 

.995 

0016 1.017 

.OD0 

0022 0955 

e916 

.959 

.952 1.15s 

.ooo 

.9d8 

.912 .958 1.034 

.957 

-964 e000 

.973 

0305 

.ooo 

0574 .900 .ooo 

.@OO 0577 .goo 

*900 1.526 

e398 0984 

1.307 1.003 

1.028 0991 1.831 

1.036 o000 

1.005 1.025 0997 

1.028 1.323 

e936 0961 

1.350 

0953 m941 1.141 

.379 

0969 0000 

TEST 39 RUN 217/0 

e984 0996 

a972 0951 

0975 

0962 0959 1.038 

0959 

0965 e000 

0974 

TEST 3, RUN 224/0 

.ooo 

523 

.ooo 

.ooo 

0998 

1.022 

1 0024 

1.040 

1.01 1 

1.026 

. 977 

,985 

966 

.985 

0954 

.coo 

.ooo .ooo 

0886 a000 

1.948 

986 

.995 

1.008 1.022 

.ooo 

1.021 1.000 

1 0019 

.966 

0950 1.131 

.ooo 

-976 :1 .983 

0986 0996 

0976 a954 

. 977 

0964 a962 1.034 

0960 

0966 a000 1 

.974 1 

TEST 3, RUN 213/11 

.ooo 

.ooo 

o000 e886 o000' 

e000 1.921 

,989 0981 

1.007 0995 

*415 .ooo .oool 

1.016 ,998 1.152 

1.037 .OOO 

1.007 1.020 0997 

1.022 1.018 

.975 .960 

0982 

0955 0943 1.1311 

0954 .ooo 

,978 

.9a2 
TABLE B-2. (Continued) 

TEST 3, RUh 195/0TEST 

00 .oco 

0 052 eooc 

0 0492 e000 e000 

003 1.01 .OOG ,970 e000 

022 1.0 e000 1.065 

~ 040 1.0 o92E 1.031 

058 1.0 0970 1.022 

094 1.0 -991 e000 

1.12 1.0 e932 e936 1.144 

1.30 led e963 -952 

1.48 1.0 0944 .e54 

1.3L 1.0 a971 

2.20 1.0 0932 ,956 e931 

2.56 1.0 o94b 

2.92 1.0 o96b a000 

3.28 lad 0936 

.7c 1.0 .96i .~62 1.031 

P 

0 

cn 

39 RUh 1F4/0TEST 39 RUN 207/0 TEST 3, RUN 19610 

.13i'o ,000 . 000 

.ooc .coo .ooo 

e526 e000 .COO\ e488 e000 a000 0387 e000 a000 

.300 e958 e000~ e000 e969 e000 e000 0977 -000 

e972 1.038 0973 1,043 

oG30 1.044 

0963 1.GJ4 

.Q54 1.007 0972 1.015 0966 1.021 

.347 .ooo 0950 .ooo ,945 eo00 

-971 0957 1.175 0955 a956 1.161 .958 ,957 1.164 

e979 a946 a991 0952 a992 0951 

095'2 0884 e960 0982 0944 0879 

0951 e956 948 

0947 -952 -976 a933 0944 ,976 0939 0945 0981 

0962 965 b957 

.959 .ooo 0958 a000 0953 .ooo 

0900 0984 .988 

' a000 2.571 ' .OOO 1.046 I 

.341 .9trz 1.076 .949 .~35 i.oai .943 .977 1.~82 
TABLE B-2. (Continued) 

OOC 

000 

I 

.coo 

396 

.ooo 

0000 

-981 

0979 

0955 

0954 

m973 

990 

0949 

0951 

.944 

0966 

960 

1.12 1.0 

1.30 1.0 

1.42 1.0 

1.34 1.0' 

2.20 1.0 

2.56 1.01 

.ooo 

,000 

0955 

1 .OC3 

1.038 

1.014 

eo00 

e958 

-951 

.884 

,948 

.ooo 

.9a& 

3.28 1.0; 0984 0986 I 

/TEST 3, RUN 2OO/C!TEST 3, RUN 2C3/0 

' 9 0 ' .ooo 

, 0 a84 0621 .OOO .OOC\ 0664 .OOO .OOO 

~ .000 

.ooo . 000 

' e03 1.0, e000 0949 -000, e000 0951 ,000 

022 1.0 .ooo 1.048 .OGO 1.048 

058 1.0 -998 1.018 0995 1.007 

~76 1.0 *98C e984 1.035 e979 .9b5 1.079 

1.01 .F63 1.031 e966 1.030 

0979 I a983 

TEST 3, RUN 202/0'TEST 3, RUN 12510 

.ooo I .981 

,000 .979 

.686 .OOO .OOO! 0978 e000 0978' 

o000 e966 .OOO/ o000 0000 e000 

e000 1.065 I .ooo .ooo 

a963 1.021 ~ .ooo .ooo 

'1.005 1.034 : .ooo .ooo 

0993 .968 1.090' a000 a000 m0OO 

.OLIO 

,000 

.513 .ooo .ooo 

.ooo 0957 .ooo 

.Oil0 1.523 

0973 1.041 

0970 1.017 

0745 0982 1.073 

a954 oOG0 

e974 ,960 1.162 

0988 0953 

-948 a8b3 

8950 

-943 .947 .967 

.9e3 

0958 .ooo 

.94 1.0 

.ooo 

.300 

~516 .OOO e000 

a000 b966 0000 

.ooo 1.947 

0959 1.040 

0967 1.005 

0946 e982 1.079 

0951 .ooo 

-973 0958 1.176 

0976 0949 

e943 0877 

. 947 

0939 0945 a990 

0951 

0956 a000 

m937 .ooo u973 moo0 0955 .ooo ! .ooo .ooo 

0=0 - - - 

rEST 3, RUN 201/O 

.ooo 

5000 

e619 a000 e000 

eo00 e974 .ooo 

e000 2.561 

0991 1.033 

1.000 1.019 

.969 .984 1.0713 

0958 e000 

s976 a959 1.170 

0987 e953 

0948 e672 

a952 

e946 a995 .986' 

963 

0960 a000 

2.56 1.0 .55C I -958 e951 

2.92 1.0; 0979 -000 ' 0970 e000 a976 o000 

1 0965 

,995 

.996 so00 

998 
TABLE B-2. (Continued) 

I. X/Q R/R 

co 

0 e52 

0 .b4 

.03 1.0 

.22 1.0 

*40 1.0 

058 1.0 

a76 1.0 

.94 1.0 

1.12 1.0 

1.30 1.0 

1.46 1.0 

1.84 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

0=0 =60 =180 

TEST 39 RUN 121/0 

.975 

e928 

e000 

.ooo 

000 

000 

eo00 

000 

.992 

a995 

*992 

8000 

.994 

994 

e 996 

.950 

.ooo .933 

.ooo .ooo 

8000 

.ooo 

.ooo 

.ooo ,000 

.ooo 

a997 1.005 

.997 

988 

m993 1.017 

eo00 

3.28 1.01 .997 

ITEST 3, RUN 136/0 

00 

0 e52 

0 -64 

.03 1.0 

.22 1.0 

.40 1.0 

058 1.0 

a76 1.0 

.94 1.0 

1.12 1.0 

1.30 1.0 

1.48 1.0 

1.84 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

3.28 1.0 

e 976 

0971 

e929 a000 e944 

.ooo .ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.GOO e000 io00 

.ooo .ooo 

e991 a997 1.005 

.994 .997 

e992 e987 

.ooo 

a993 e993 1.019 e 994 

e995 .ooo 

996 

0=0 =60 =180 

977 

TEST 3, RUN 114IO 

e929 

.ooo 

000 

.ooo 

~000 

.ooo 

.ooo 

,992 

994 

m992 

.oco 

e993 

.994 

966 

a952 

.ooo e934 

.ooo .ooo 

.ooo 

e 000 

.ooo 

.ooo .ooo 

000 

m998 1.006 

a998 

. 988 

a994 1.019 

000 

.997 

TEST 31 RUN 13O/O 

978 e 972 

.930 .ooo .945 

.ooo .ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo .ooo 

a000 .ooo 

n993 m998 1.007 

e996 m999 

e993 e990 

. 000 

0994 a994 1.019 

.995 

.997 .ooo ~ e998 

0=0 =60 =180 1 0=0 =60 =I80 

TEST 3, RUN 115/0 TEST 39 RUN 120/0 

983 

e912 

.ooo 

.ooo 

.ooo 

.ooo 

000 

.ooo 

s991 

.994 

.ooo 

992 

.993 

,995 

,990 

a952 

a000 e926 

,000 .ooo 

.ooo 

000 

.ooo 

.ooo .ooo 

000 

a996 1.004 

996 

a987 

m992 1.018 

000 

997 

e982 

TEST 39 'RUN 137/0 

.975 

a938 e000 a953 

.ooo .ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo .ooo 

.ooo .ooo 

e992 s997 1.005 

0994 e998 

e992 e988 

.ooo 

e992 s993 1.019 

.993 

.995 .ooo 

.997 

,913 

.ooo 

.ooo 

.ooo 

000 

000 

000 

992 

995 

e991 

.ooo 

994 

.995 

.991 

.956 

a000 a928 

eo00 a000 

000 

.ooo 

.ooo 

.ooo .ooo 

000 

a997 1.006 

.998 

-989. 

a994 1.019 

.ooo 

998 

TEST 39 RUN 131/0 

983 

.973 

.938 .ooo .F53 

.ooo .ooo .ooo 

.ooo .ooo 

a000 .ooo 

.ooo .ooo 

.ooo .ooo ,000 

.ooo .ooo 

a991 e996 1.004 

.994 .997 

e991 .987 

.ooo 

m992 e993 1.016 

.992 

.994 .ooo 

.995 
TABLE B-2. (Continued) 

0 -52; ms57 

o .64, .ooo .a26 

003 l.oi .ooo .ooo .ooo 

0 

0 

0 

-03 

.22 

.40 

.5P 

I my4 

11.30 

,1.4P 

'1 .t!4 

2.20 

2 m56 

2 mF2 

I .76 

11.12 

2.92 1.0 0966 -000 

3.28 1.0 a978 

0 

.52 

.64 

1.0 

1 mo 

1 mu 

1.0' 

1 .@ 

1 mo 

1 .O' 

1 .o 

1 eo' 

1.0 

1.0; 

1 mo 

1.0, 

e965 a000 

978 e977 

e925 

-922 

.coo 

coo 

.ooo 

a006 

coo 

. 000 

mF7b 

e987 

. 973 

.GOO 

m?6t 

.'/bI 

q66 

0926 

.ooo .919 

.ooo mooo 

mooo 

.ooo 

e000 

*COO a000 

.ooo 

-998 1.034 

.997 

e960 

-957 1.053 

.coo 

:3.2E 1.0' e976 

!TEST 3, RUN 112/@ 

.860 ! .872 

390 

me75 

*E68 a000 a848 ,836 e000 m840 

.ooo 

aoco 

.900 

moo0 

000 

.ooo 

.979 

e989 

976 

mooo 

e967 

m363 

969 

mooo .ooo 

000 

.ooo 

.ooo 

.ooo a000 

000 

m999 1.035 

999 

e963 

e961 1.053 

000 

ma43 

m861 

a819 o000 e829 

.ooo .ooo .ooo/ .ooo .ooo .ooo 

mooo .ooo 1 mooo .ooo 

.ooo .ooo mooo .ooo 

so00 .ooo .ooo .ooo 

mooo mooo .0001 mooo mooo mooo 

a000 .ooo ' mooo .ooo 

.973 .993 1.0271 .979 .996 1.0321 

a981 a992 ' .987 a997 

m969 a957 ' .974 e961 

a961 .954 1.040: a968 a955 1.044 

a956 962 

eo00 , mooo 

0963 moo0 I m969 .ooo 1 

a952 

TEST 3, RUN 11610 39 RUN 135/04 

m807 878' 

a813 0874 

.770 .OOO .801/ *774 e000 *812, *846 .OOO .e79 

.ooo mooo moooi .ooo mooo mooo 

mooo .ooo 1 .ooo .ooo 

mooo mooo , mooo mooo 

.060 a000 1 mooo mooo 

m76 1.0, *COG moo0 m@OO1 *OUO -000 .OOOi e000 a000 a000 

.WUU muuu 

1.12 1.0 -975 .996 1.031) .975 .995 1.032' ,978 .997 1.033 

1.30 1.0 e985 e995 , a985 a996 , *986 e998 

.ooo 

.ooo 

000 

000 

. 000 

. 000 

977 

986 

a000 .0001 

000 

.ooo 

mooo 

.ooo mooo 

.ooo 

e998 1.032 

996 
TABLE B-2. (Continued) 

i1.30 1.0 

1.46 1.0 

1.84 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.0 

3.28 1.0 

' X/D R/RI a=U =60 =lwO 0=0 =bo =I80 0=0 =60 =180 ~ Q=O =60 =160 

:TEST 3, RUN 12Q/l TEST 39 RUN 132/0 TEST 39 RUN 138/0 TEST 39 RUN 127/0 L 

1.026 1.022 ,10027 

0972 0976 ' 0974 

.ooo .oca 

0956 0941 1.149 0965 

0982 .9&7 

0961 e000 0963 

e989 ,990 

J 9 ~ .e31 .gel 0959 778 

C .521 ,376 .F22 0923 

C e84 0649 .OOC .P2L -399 o000 e924 0901 .OOO 0924 0750 

003 1.0 oCOC e000 e000 -3GO e000 a000 e000 e000 ,000 o000 

.L2 1.0' .COC' .coo .OGO .000 .ooo .ooo .ooo 

053 1.9 .000 ,000 .320 .ooo .ooo .ooo .ooo 

m76 1.0 e000 e000 e300 -3UO a000 a000 0000 .OOO a000 .OOO 

094 1.0 .ooo .coo ' .330 .ooo .ooo .ooo . 000 

1.12 1.0 s976 e996 1.030 0981 1.000 1.035 a981 1.003 1.036 le004 

11.30 1.3' .966 .997 , .9b9 10000 0992 1.000 1 0025 

'1.48 1.01 a974 e961 e977 0963 a977 0965 e969 

loC4 1.0 oG33 1 .ooo moo0 . 000 

2.20 1.0 o9t,4 -958 1.037, a906 0961 1.039 0967 0961 1.052 0957 

2.56 1.0 e560 961 e962 0984 

043 loci .COG .COG e3CG .OOO .ooo 8000 eooo 

1.024 1.025 1.020 

982 e974 0984 

.ooo 

0946 1.140 -974 0948 1.128 

.991 

0987 

.ooo .960 .OOO 

0764 

a000 e817 

.ooo .ooo 

.ooo 

eooo 

.ooo 

.ooo .ooo 

a000 

1.022 1.002 

1.024 

.976 

1.027 1.018 

e966 0978 

.ooo 

0969 0949 1.150 

e987 

0956 e000 

. 994 

.943 1.152 

'2.92 1.0 0966 e000 1 0966 .OOO .967 .oOo 0960 o000 

3.28 1.0 0977 1 0978 980 989 

TEST 3, RUN 110/1'TEST 3, RUN 109/2 TEST 39 RUN 123/@ TEST 39 RUN 113/0 
TABLE B-2. (Continued) 

-- =?BO 

118/0 

,648 

.ooo 

0=0 =60 =I80 0=0 =6i) =180 

TEST 3, RUN 134/0 TEST 39 RUN 129/0 

0775 788 

.740 .748 

,713 .OOO a743 a720 aO'OO a751 

.ooo .ooo .ooo .ooo .ooo .@OO 

.ooo .ooo .ooo .ooo 

.ooo .ooo .945 .ooo 

I a76 1.0 e000 o9CO .@CO/ e200 .90C .OUO' .OOO .OUO a000 .OOO .OOO .OOO, 

094 1.c .coo .oco .oco .uoc I .ooo .ooo .ooo .ooo 

11.12 1.0 1.007 1.022 1.00411.014 1.023 1.015/1.002 1.029 l.OC)7~1.014 1.024 1.016 

11.30 1.0 1.026 1.019 11.325 1.022 1.029 1.024 1.031 1.027 

1.4E 1.0 e976 ,976 j .375 .985 

1.64 1.6 .COO ~ eo00 

2.2C 1.0 .C5& a939 1.1481 m970 .949 1.125 

2.56 1.07 e985 I .969 

2.92 1.0, .957 .ooo ' 0963 .ooo 

*,3.28 1.01 .9a9 i .9b4 

]TEST 3, RUN 139/1iTEST 3, RUlri 13310 

I 0 0 , .887 , .9Y1 

0 e52 e81 1 I . a05 

0 064 .791 .OOO -972' .784 .OOO .a09 

003 1.0: .ooo .ooo .OOO~ .ouo .ooo .ooo 

.22 1.0 .ooo ,000 .ooo .ooo 

.40 1.0 .ooo 

.5E 1.0 .ooo 

.Y4 1.0 .coc 

1.12 1.0 1.030 

1.30 1.0, a973 

1.49 1.0 .975 

l.b4 1.01 .OOO 

2.20 1.01 a921 

2.56 1.0 a961 

'2.92 1.0 a986 

.76 1.0, .oou 

i3.28 1 .O ~ 1.006 

.ooo 

.ooo 

.ooo 

moo0 

e921 

e981 

0950 

e996 

.ooo 

. ooc , .ooo 

I .ooo 

.ooo/ .ooo 

,970 1.007 

~ 1 e012 

000 

.ooo 

.ooo .ooo . 000 

1.017 1.020 

1.018 

.97a 

0943 1.111 

000 

1 .975 a968 I .ooo .980 1 

.950 .937 i.i52( .98i .ooo 1.134: 

* 000 i .OOO 

m968 0000 ~ ,972 .OOO 

977 e987 

.977 1 .984 

TEST 3, RUN ISO/O/TEST 3, RUN 148/O 

e733 1 .619 

a756 1 *620 

a709 e000 e7921 e471 e000 *496i 

a000 0000 I eo00 .ooo 

a000 moo0 .ooo: .ooo .ooo .ooo\ 

.ooo 

. 000 

000 

.ooo 

a976 

984 

.947 

.ooo 

a941 

.956 

.961 

.9a6 

.ooo 

. 000 

000 

000 

.954 

a950 

. 882 

0946 

. 000 

1 

I eo00 

i .ooo 

.ooo/ .ooo 

\ boo0 

1.178, e978 

I 0976 

I e948 

. 000 

.987[ .947 

' .958 

! e964 

e988 

.ooo 

m000 

e000 .GOO . 000 

e951 1.187 

e950 

0891 

.948 .986; 1 

e000 1 

L 
TABLE B-2. (Continued) 

)(/D R/R 0=0 =60 =I80 0=0 =6G =I80 I 0=0 =60 ~180 

TEST 39 RUN 149/0 TEST 39 RUF( 146/0 TEST 39 RUN 145/1 

00 596 ,547 

0 052 o5Yb 0639 

C ab4 0450 a000 0451, o5U7 a000 e536 

00: 1.0 .ooo .ooo .ooo .OCO .ooo .ooo 022 1.0 .OGG .GOO .CGO ,000 

040 1.0 

.SP 1.9 

-76 1.0 

094 1.3 

1.12 1.c 

1.30 1.0 

1.413 1.0 

1.04 1.0 

2.20 1.0 

2.56 1.0 

2.32 1.0 

3.25 1.0 

03 

0 052 

0 .64 

033 1.0 

022 1.0 

040 1.0 

.55 1.0 

076 1.0 

094 1.0 

1.12 1.0 

1.30 1.0 

1.43 1.0 

1.84 le0 

2.20 1.0 

io56 1.0 

2.92 le0 

3.28 1.0 

oca0 .ooo .Ob0 .ooo 

oca0 ,000 .?LO eo00 

.coc ,000 .oco .oco .ouc .000 

.ooo ,000 0300 .090 

o90t e948 1.1115 ,971 0953 1.174 

,976 .953 .?&l 0946 

0951 .e94 , .944 ,984 

.ooi? 

0967 .9so 0977 

. 959 

0966 ,000 

095s 

e673 

TEST 39 RUN 147/0 

,722 

.625 ,003 .66? 

.OOO .ooo .ooo 

.ooo OOCO 

,000 .OGO 

.ooo eo00 

.COO e000 e000 

oCG0 o000 

0975 e955 1.173 

e961 0949 

-951 eSE7 

.OOG 

.94e ,949 0984 

0957 

.956 .OOO 

-963 

.OQO 

.F42 .941 .989 

,959 

0959 oOG0 

e962 

TEST 39 RUN 142/O 

.802 

.CdO .coo .ooo 

.000 0300 

,300 .ooo 

.3GO 0300 

,000 .3oo .ooo 

.,suo .300 

0355 ,566 1.196 

1.902 0977 

.973 .911 

oOOG 

.976 e973 0991 

0978 

0997 .ooo 

1.012 

.<bE 

,772 .OOU .7a7 

0555 

670 

.coo .ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo .ooo 

.ooo .000 

0976 e950 1.167 

,509 .eo0 e543 

.9a5 .9s2 

0950 0895 

.coo 

.947 .949 0974 

. 964 

0963 e000 

0963 

.e50 

.793 

0767 o000 -783 

.ooo .ooo .ooo 

e000 oOG0 

e000 .OGO 

.ooo .ooo 

eo00 .ooo .ooo 

.ooo ,000 

.923 .962 1.207 

0996 e971 

.969 0904 

.ooo 

e967 e967 le009 

0972 

e984 .COO 

TEST 39 RUN 141/O 

1 e003 

0=0 =60 =le0 ' 

TEST 39 RUN 144/1 

674 

,740 

0627 .OOO a666 

.ooo eooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo 

.ooo .ooo .ooo 

.ooo eooo 

e979 0957 1.168 

.986 .95a 

.951 .a92 

.ooo 

,951 e947 0972 

966 

0965 e000 

988 

TEST 39 RUN 140/0 

965 

,847 

0834 e000 OR45 

.ooo .ooo .ooo 

.ooo .ooo 

eo00 .ooo 

.ooo .ooo 

e000 e000 e000 

.ooo .ooo 

0976 0961 1.206 

0993 e971 

0964 a903 

.ooo 

0965 0966 1.008 

969 

0985 e000 

1.004 
TABLE B-2. (Continued) 

X/D R/R 

00 

0 e52 

0 .84 

e03 le0 

.22 1.0 

e40 le0 

sa 1.0 

.76 1.0 

e94 1.0 

le12 le0 

1.30 e0 

1.48 a0 

1.64 e0 

!e20 e0 

2.56 .o 

2.92 1.0 

3.28 le0 

30 

0 e52 

0 e64 

e03 1.C 

.22 1.c 

.4c 1.c 

058 1.c 

e76 I.( 

.94 I.( 

le12 la( 

il.30 1.( 

,1.48 I.( 

rl.64 1.( 

2.20 I.( 

2.56 I.( 

2.92 I.( 

3.28 I.( 

0=0 =60 =I80 

EST 3, RUN 14310 e 967 

849 

e823 e000 0830 

e000 e000 ,000 

.ooo .ooo 

.ooo .ooo 

-000 e000 

e000 e600 e000 

e000 -000 

e949 a943 le169 

e979 e953 

.942 ,873 

.ooc 

.96b 

e982 *OdO 

e975 

e953 e958 e974 

rEST 3, RUN 62/C 

a969 

m922 

953 

000 

e965 

e991 

a992 

1 e001 

e993 

e 996 

e993 

,952 

.954 e95i 

,976 

e985 

-991 

,994 .99< 

998 

.999 

.991 

*928 e921 

.99a 1e0~( 

0=C =60 =160 

lEST 3, RUN 66/0 

e 9SG 

e978 

e980 a982 a977 

e986 ,985 ,985 

e000 m992 

.995 .995 

s999 a998 

-999 e999 1.003 

1eOG7 le003 

m996 1.001 1.009 

e998 1*001 

,994 .993 e 997 

e996 e990 1.021 

e095 

e997 a000 

,999 

m956 

TEST 3, RUN 6110 

e 926 

e914 a913 e915 

e951 e944 e950 

0300 e972 

e965 .ca3 

a331 .990 

e992 e994 e997 

1.032 .997 

e992 .997 1.005 

-995 e998 

e952 -990 

g=O =60 =180 

'EST 3, RUN 67/0 

0963 

e926 

.953 

e000 

e984 

. 990 

.992 

I .001 

992 

.995 

a991 

994 

e 994 

994 

.995 

.945 

e932 a936 

e953 e961 

.975 

a984 

.990 

e994 e998 

e996 

a997 1.005 

.997 

e 989 

.994 1.020 

000 

.99e 

969 

rEST 39 RUN 7610 

.947 

a913 e914 .914 

.945 a944 .945 

e000 e988 

,981 e980 

e967 .9a7 

.989 e991 

,997 e993 

e990 e994 

.992 .995 

e992 

.9a9 .987 

.995 

e 002 

e991 a992 1.015 

e991 

.993 .ooo 

995 

Q=O =60 =180 

'EST 3, RUN 56/0 e 964 

933 

,957 

.ooo 

991 

.992 

I .001 

.992 

.995 

,992 

e 994 

.994 

.9a5 

a948 

a936 e936 

.956 .961 

e 976 

e985 

,991 

.995 ,998 

.997 

*997 1.005 

997 

e990 

e994 1.019 

.994 

e996 a000 

.946 .939 .9491 

e000 e971 1 

.982 .981 ! 

.989 .98a 

e990 0992 ,997, 

1.001 ,994 

-991 a996 1e004' 

e994 e997 1 

e991 e988 1 

e 997 
TABLE B-2. (Continued) 

X/D R/R d=O =6G =1PO 0=0 =60 =180 0=O =60 =180 

TEST 39 RUN 7710 TEST 3, RUN 62/1 TEST 39 RUN 83/0 

00 e959 .?b1 e967 

0 e52 e943 .945 e959 

0 et54 eC11 e913 -917' e914 e916 -919 e925 e928 e932 

eU? le0 e944 e942 e94E -947 e944 a951 e954 e951 e957 

e22 1.0 e000 e969 .COO e951 e000 -944 

e40 le0 e979 e980 .9~2 e9dl e983 a983 

.SP 1eC e987 -966 e969 e988 e990 e989 

e76 le0 e938 e969 e995 e990 0991 e997 e991 e992 ,997 

e94 1eC e997 -993 1.OCO e994 le001 e995 

1.12 1.0 e989 .F93 1.002 -391 e995 le004 e991 e995 le001 

1.30 le0 e992 e994 e594 e996 e994 e996 

1.48 le0 e968 -984 e999 e987 e991 e967 

1-54 1.0 eFF1 ,992 e 994 

2.20 le0 s991 e990 1.016 e353 -993 le018 e993 e993 le018 

2.56 le0 e991 e 992 e993 

2.92 le0 e992 e000 -994 e000 e995 e00'0 

3.28 1.0 e994 .397 e996 

TEST 2, RUN 69/0 TFST 39 RUN 6610 TEST 39 RUN 57/O 

00 

0 e52 

0 .64 

e03 le0 

e22 1.0 

e40 le0 

e53 le0 

-76 le0 

e94 le0 

le12 le0 

le30 le0 

1.48 1.0 

2.20 le0 

2.56 le0 

2.92 le0 

iea4 1.0 

3.23 1.0 

e954 

,956 

e955 e963 e952 

e969 ,968 .96a 

e000 ,982 

e987 e988 

.994 .994 

e994 a996 1.004 

le011 1.004 

eF88 e998 le015 

e993 ,998 

e985 e982 

.989 

e967 e967 1.039 

e986 

e98G e000 

e993 

e932 

e 903 

-365 ea90 e891 

e921 e920 e930 

e000 e956 

e971 e072 

e983 e982 

e9b4 e988 e998 

le001 e994 

e964 e992 1.011 

.9%9 e995 

.qd? e970 

Qd6 

e964 e985 le035 

e984 

e987 e000 

'.991 

e941 

e904 

e889 .89i ea93 

e922 e921 e832 

e000 -957 

e972 e971 

e984 e983 

a905 e888 e997 

le003 e995 

e982 e993 le011 

e988 e994 

e981 e977 

e 986 

e983 e984 le037 

e983 

e986 e000 

~ e991 

0=0 =60 =180 

TEST 3, RUN 88/0' 

e965 

e956 

e922 e925 a930 

e950 -948 e954 

e000 e957 

e982 e981 

m989 e989 

e990 e992 e997 

le000 e994 

,990 e995 1e003' 

e994 e996 

0990 e987 

e 992 

e992 e992 le017 

e993 

e996 

TEST 39 RUN 6010 

e 937 

e917 

ea77 ,885 e870 

e920 a919 e926 

e000 e956 

e972 e971 

e983 e983 

e986 a989 e998 

le004 e995 

e983 e993 le011 

e989 e994 

e982 e978 

e 986 

e964 -985 1-03? 

e 984 

e987 .OOO e 992 
TABLE B-2. (Continued) 

00 

0 e52 

o .84 

eG3 1.0 

.22 1.0 

o4G 1.C 

.5E 1.0 

.942 

.abc 

e920 

.O@C 

.972 

.983 

.919 

a921 

.958 

a972 

.9e4 

.969 

.996 

.995 

.995 

.979 

.ea7 e882 

.92t 

.9u9 

e846 

.951 

bd9 

*e99 a910 

.a59 ,857 

. 948 

m965 

.978 

.985 .994 

.991 

.991 1.008 

991 

.973 

e03 1.0 a907 e905 e915 *923 e921 *933 

e22 la0, SO00 1.045 *OOO 1.105 

e40 1.01 e967 .967 .973 .973 

.76 1.0 .m3 .9a5 .9958 .965 .w .997 

1.12 1.0 .sea mi 1.009, .9d3 .994 1.011~ 

.59 1.0' .9sc .979 .9b4 e964 

a94 1.0. a999 a991 '1.004 .994 

iz.20 1.0 .gab .966 1.037 .?a2 .9a3 1.031 

"2.56 1.0 -985 -981 

2.92 1.0 .~a9 .oco .96L .ooo 

a921 a921 a9321 e947 a946 *950 

a000 la114 a000 a972 

a972 s972 , ,983 .9a4 

.966 .98a .998 .996 LOOO 1.018 

.9a3 .994 1.010 .983 i.ooo 1.035. 

.984 .9a3 ,996 .995 

1.002 .994 1.019 1.009 

0=0 =60 =180 

TEST 39 RUN 72/0 

a906 

.845 

m982 

a000 

s967 

a981 

.os3 

1.002 

.9a2 

.a87 

.e54 .a58 

.a97 ,909 

a 948 

967 

.988 

a966 e996 

.993 

a991 1.009 

a 907 

. a62 

a910 

000 

969 

962 

.984 

1.002 

a903 

m873 e880 

a908 s921 

.953 

e968 

.gal 

a986 a997 

e992 

a981 a992 la009 

,988 .993 , a988 a992 

a960 e975 .979 .973 

.985 984 

.9a3 m982 

a986 e000 a985 .ooo 

.9a3 .983 1.036 .983 .9a3 1.035 
TABLE B-2. (Continued) 

'0 

3 

0 

.c)3 

.22 

e40 

e 55 

e 76 

e 94 

1 .I2 

1 e30 

1.48 

1 .c4 

2.20 

Le56 

2.92 

0 e857 .Sd8 

.52 .a51 a351 

e84 eel9 e840 sR2G e524 eP29 

1.0 e8U4 e864 sP99 e337 'r984 

1.0 so00 .945 eOOG e949 

le0 a966 a960 I .vce e909 

1.0 e985 e983 e327 e9b7 

le0 a935 e990 1.008 e990 e993 

1.0 1.009 1.000 1.016 1.003 

le0 e976 e991 1e02R e976 e995 

1.0 e985 e994 e986 e994 

1.0 e972 0965 e970 e966 

1.0 e973 .972 

1.0 e563 a964 1.045' -962 e957 

1.0 a961 e957 

le0 e968 e000 e963 a000 

e823 

me23 e800 

. 000 

e965 

e985 

le012 e964 

1 a009 

1.032 e976 

e965 

e972 

e975 

1.@47 e966 

e958 

e 965 

.9o5 .a76 

s 830 

e851 

.a28 e797 .Bo5 

a984 a892 a880 

e944 aooo 

a965 e 967 

e 983 m984 

a991 1.010 a987 

1.001 1.012 

e992 1.029 e977 

. 993 ' a985 

s963 e972 

s 976 

e959 1.039 e968 

963 

000 969 

,853' 

e826 .BO4 

a881 a894 

.944 

.967 

a903 

e991 1.007 

1.001 

s994 1.029 

.994 

a966 

s964 la052 

e000 

3.ZE 1.0 .979 e980 .9?9 . 98 1 

'TEST 3, RUFj 74/1 TEST 3, RUN 73/0 TEST 3, RUN t10/0'TEST. 3, RUN 79/0 

'10 

0 -52 

0 a4 

.03 so 

e22 e0 

e40 e0 

e58 sC 

e76 le0 

e94 1.0 

le12 1.0 

le30 1.0 

1.48 1.0 

la84 1.0 

2.20 1.0 

2.56 le0 

2-92 le0 

3.28 1.0 

.782 

,794 

e734 e764 e768 

e858 -854 e880 

.coo 0937 

e961 -961 

a981 e979 

e963 e9b8 le007 

1aOOb a998 

e973 .99e 1.027 

.VB2 .991 

e969 e960 

e972 

e962 .960 le039 

a 957 

a963 .ooo 

,975 

0 763 e805 

.796 e823 

.747 e766 e768 -778 .800 ea90 

e861 e655 e8341 e867 e866 e890 

s0OC e939 

-965 e965 

e933 .983 

e9b6 e992 le038 

1.311 e999 

-376 e993 le029 

e984 e993 

-971 0962 

.974 

e966 e961 1.048 

.959 

.PO6 a000 

e?78 

aooo so00 

e963 e961 

e983 e960 

e983 e988 1.006 

1.00: e999 

e973 e990 1.025 

e982 e991 

a969 e957 

e973 

e963 e961 1.047 

.957 

e964 so00 

976 

a 797 

a770 ,793 e805 

a864 a862 s887 

so00 e939 

s962 e963 

e980 a981 

e982 .988 IeOOi 

.814 

1.007 a997 

a974 a990 la027 

a983 a992 

e968 a956 

970 

a961 ,958 1.033 

a956 

a963 a000 

e976 
TABLE B-2. (Continued) 

X/D R/R $=O =60 =le0 0-0 =60 ~180 0=0 =60 =180 

00 .e32 .832 

0 e52 me42 ea40 

0 .ac e805 -328 e842 .806 .S28 e840 

TEST 3, RUh 8610 TEST 3, RUN 65/O 

e03 1.0 e861 e879 e905 e376 e883 .P76 

e22 1.0 e000 e948 e000 le354 

a40 1.0 m969 a986 e961 e961 

a58 1.0 e987 e986 e981 e979 

8=0 =60 =1EO 

a76 1.01 0990 0994 1.013 

e94 1.0'1eO11 1.003 

1.12 le0 .977 e998 1.030 

e9d3 a986 e907 

1.0L6 .995 

e969 e989 e997 
TAB LE B-2. ( Continued) 

e4C la0 -980 a975 a978 a976 e987 e975 

e59 le0 e989 a993 l .9~a e988 e997 la008 

e70 le0 a993 ,995 le015 -992 e994 le014 e999 le002 le021 

a94 le0 le023 1.017 le317 le043 la024 1.021 

le12 la0 e979 ,993 le035 e9aC e992 1.030 a979 e998 la037 

le30 le0 e984 ,991 e984 e990 e988 e995 

1.48 1.6 .572 ,964 e976 e961 e975 e966 

le84 la0 a969 e974 e971 

2.20 1.0 e964 .949 1.048 .968 .957 le038 .962 e949 1.048 

2.56 le0 e956 a962 e955 

2.92 la0 e967 a969 0968 e970 e969 e967 

3.23 la0 e983 e952 e 983 

' X/D RJR g=O =60 =le0 0=(j =60 =le0 ' 0=0 =OO =I80 6=0 =60 =180 + 

TEST 1, RUN 472/G TEST 1, RUN 423/0 TEST 1, RUN 45510 TEST 1, RUN 45410 

' a968 e974 

e972 e974 

e973 e977 e994 

e999 la225 

e955 e972 le009 

e961 -e968 

e949 e940 

a 944 

,939 .925 1.019 

e931 

e940 a943 

e956 

0 

0 

,o e 03 

e22 

e40 

' e58 

e76 

e94 

1 e12 

1 a30 

1 e48 

I .a4 

2 e20 

2.56 

2 e92 

0 e 907 

a52 

e64 e915 

le0 e940 

1.0 .972 

le0 0985 

1.0 e993 

le0 e996 

le0 1eG24 

le0 .F7& 

la0 e984 

le@ a974 

1.0 -971 

le0 eF6~ 

le0 e956 

1eC -967 

e 7aa 

eo00 

e010 e905 e967 

.COO e952 .e54 

.970 a945 

a982 a970 

,993 m9~2 

-998 1.016 e938 

1.018 1 e015 

,994 1.037 e974 

e991 ~ e962 

e965 ' .970 

e 909 

a950 le050 .?el 

.957 

-971 ' .769 

e792 t 000 e 000 

e786 -808' e770 e790 

e000 aR95' e865 e000 

.944 ' e947 e947 

965 a971 -967 

.983 e962 e985 

e969 1.008 .sa9 .992 

1.010 ~ le017 1.011 

e990 le030 e976 a992 

e 9&9 a984 e991 

963 a072 a962 

e972 

.959 

a950 la047 e96G e953 

.966 e970 a969 

e 900 

.ai2 e361 

e896, e903 

a 960 

e979 

e 985 

la010 e994 

1 e020 

le031 e976 

e 987 

e 974 

.97 4 

le046 a968 

e959 

e971 

e000 

e877 e889 

e000 e934 

e962 

e977 

e991 

e996 le014 

1 e012 

e994 le033 

a993 

e 965 

e957 le045 

e972 
TAB LE B-2. ( Continued) 

' X/D R/R id=C =6>:0 0=0 =hO =I30 0=0 =6O =I80 

TEST 1, RUtv 4illC TEST 19 PUN 459/0 TEST 1, RUN 452/0 TEST 1, RUN 42010 

3 3 1,025 1 .s93 1 .OS6 1.078 

:3 .52 .coo .GUC .os(! ' ,000 

3 -04 e944 -95: eQb2 eo02 1.003 .9ai .998 .99i .985 1.004 .w2 

.c13 i.o .9t: .oti3 .os7 .FG; .CJC 1.015 .99i .ooo 1.013 .~95 .ooo 1.016 

.22 l.C .95E ,959 .os5 1.635 0995 1.005 .999 1.006 

,110 1.0 .996 .9b9 lac26 lac11 1.004 1.207 1.007 1.003 

.5! 1.0 1.c;: 1.369 '1.269 1.c12 1.007 1.011 1.011 1.021 ' .7C; l.Cil.GS4 1.GGE 1.?2t,~1.211 1.012 1.034 

.94 7.0, 1.G35 1.024 '1.331 1.L758 

1.00S 1.012 ?.OZE,l0012 1.015 1.C3L: 

1.031 1.040 1.036 1.034 
TABLE B-2. (Continued) 

rl ab41 

003 1.0 

022 1.3 

.40 1.0 

e58 1.0 

, e7C 1.0 

034 1.S 

1.12 1.C 

1.30 1.C 

1.4? 1.0 

1.84 1.0 

io29 1.0 

2.56 1.0 

ieY2 1.0 

+3.~a 1.0 

0 

0 

0 

003 

022 

040 

. 5E 

.7t 

.F4 

1.12 

1.30 

1 .Le 

1 .e4 

2.20 

2.56 

2.Y2 

e004 ,915 ,921 

.944 ,000 0955 

0980 .9F2 

.F93 1,001 

1.GlC ,995 

1.617 1.013 1-92! 

1.060 1.040 

1oG06 1.634 1.913 

1.019 1.025 

1.016 .CSL 

e942 

~FCL .FZF 1.137 

-970 

-960 1.003 

.9~ 

0 . 91 2 

e52 *COO 

-64' .PO2 -809 0617 

1.0 .922 .OOO -037 

1.9 .sa2 .wo 

1.0 1.007 0996 

1.0 1.015 .999 

1.0 1.019 1.017 1.025 

1.0 1.C51) 1.C44 

1.0 1.603 1.030 l.C?OF 

1.0 1.c.05 1.021 

1.0: 1 .GO6 .995 

1.0 .F4C 

1.01 .96t .925 1.1Lt. 

1.0' .965 

1.3 0972 1.001 

.9c4 .VY1 ,987 mQ98 1 0087 0919 

.9Y7 1.GOC 1.011 ,966 1.005 1.000 

1.315 0395 1.017 1.C16 '1.014 1.017 

1.067 1.041 1.056 1.046 1.050 1.179 

1.337 1.032 1.017 1.CG7 10C21 1.012 1.@03 leC'l8 1.215 

1.563 1.019 1.002 1.019 1.006 1.020 

1.016 e991 1.003 e993 1.002 0979 

1.015 1.013 1.CL7 1.024 1.021 1.927 1.023 1.024 1.626 

.0:9 .93? 0945 

e901 e926 1.133 e969 e924 1.144 0972 e930 1.105 

.973 .969 .97 3 

0976 1.001 .976 1.co1 0972 0998 

.906 .9&9 . 988 i 
TABLE B-2. (Continued) 

eo09 

e735 e759 e750 

e957 e000 le059 

e999 1.005 

1.019 e997 

-964 1 .GO4 

-966 e923 1.046 

.919 ,928 

e929 e946 1.123 

e933 e92q 

e924 .P&l 

-9~1 

704 

e772 e715 

1.074 .QC4 

.959 

1.016 

306 

1eO5,c e372 

.9Lt 

1.14c .?Le 

.93c 

.QLt 

.?CC 

.QtS .9L1 

, .:37 ~ .965 1.902 

1.088 

*e77 

eo76 

1 e020 

e981 

.973 

e951 

a925 

,022 

e046 

e 954 

eP54 

e 000 

e740 .724 

.030 1.053 

1.011 

e 994 

1ec11 

e991 1.043 

-341 

.947 1.127 

.93& 

*&be 

e916 .OF4 

0=u =60 =le0 (J=O =60 =lEO 

TEST 1, PUN 447/01TEST 1, RUN 41410 

.eo7 

e000 

eR92 et84 

.COO le085 

1 eo10 

1.005 

1 e066 

e999 1eC61 

e967 

.C39 le126 

e945 

e895 

1 eo11 

3.23 1.3 .F83 ! 1 .$Zt ,993 ! .989 

' 1 e110 1.233 ' 1 e 337 

-c 

TEST 1, RUh &t7/Q'TtST I, r7lrt.l 4.r6/OITEST 19 QUhl 4J3/0 TEST 1, RUY 413/0 

1.169 

.ooo e \;do .ooc) eooi) 

I 3 -64 e587 ,653 .Pcli -366 eR9E e893; eo53 e955 -062' a972 -987 e972 

eo! le0 e476 .@OO 1eOE7 e973 e9OC 1.086 e995 e000 le071 e992 e000 1.078 

.22 1.01 1.025 1.001 1.923 1.913 '1.009 .CE3 ';LO18 1eOlr) 

.40 1.C .F61 1.022 .Oa2 1ec37 { e980 1.011 '1.004 le001 

e52 le3 .973 .99c ,970 le027 e965 1.11? ' .972 1.057 

.75 1.0' .95i .9a8 1.071 .F~C 1.000 1.065 .939 .97o 1.060' .958 ieOi)3 lac57 

-94 1.0' e32L 1.091 e924 esse e907 le148 e920 e917 

1.42 le0 e953 ,691 e949 e390 e935 e579 e948 .596 

2.56 1.9, e970 e 766 e 968 e956 1 

2-92 1.0 e99J 1.C09 .354 1.015 e923 e379 e991 1.010 

1.12 1.3 e919 ,941 le132 0113 e940 1.132 e926 -948 1.167: 0943 e940 le129 

le39 le0 -959 -940 .34c e937 e989 ,929 e941 e946 

led4 le3 e9Cl e956 .945 * e960 

2.20 1.0 ,942 .!I33 .952 ,937 .930 .961 .944 .923 .971j .943 .937 -970' 

82.23 1.5 1.c0c .VY5 ,999 ,, e990 
TABLE B-2. (Continued) 

,935 ,915 

,099 0990 .F39 

1.031 1.C03 

,065 0459 

1.019 

1.014 eC90 0733 

eQ63 

0992 1.0G7 

1.019 

1 X/D R/R 

0919 e910 

0994 0984 0537 

1.024 .097 

0977 .953 

1.012 

1.009 .OB4 0731 

.954 

.987 1.OCO 

1.019 

3c 

9 -52 

0 .L4 

033 1.0 

.2; 1.0 

.4i) 1.0 

.5? 1.5 

.76 1.C 

094 1.0 

1.12 1.0 

1.3G 1.C 

lokg 1.9 

1.~4 1.0 

2.20 1.0 

2.56 1.0 

2.92 1.c 

1.C27 e999 

,977 .9:4 

1 eC13 

1eCCC1 a985 ,731 

.95b 

.FY3 .99t 

1.02c 

1 oL31 1.610 1 e671 1.692 

,000 000 .000 000 

m961 0996 ,095 1.047 1.064 1.007 1.054 1.060 1.056 1.053 1.092 1.1356 

.C9b o000 1.065 1.032 e000 1.095 1,023 a300 1.104 1,032 moo0 1.102 

1.017 1.306 1.022 2.124 1.023 1.016 1.023 1*006 

eCC6 IeCb4 ,965 1.323 0969 1.022 .961 1.017 

,967 1.022 ,901 1.043 e971 e068 .968 -973 

.93% -964 1.951 2.1~6 e975 2.141 e936 a949 1.364 0941 e896 1.071 

.92C 1.16P 0325 .900 .912 .933 .931 1,015 

0957 ,?E2 ' e350 a830 ' .os9 .230 .959 .881 

.F5G .7>2 * 947 0955 

-931 e924 eo63 ,344 e925 e973 ,933 a917 0949 0941 e326 0937 

.9 72 356 ' ,926 .962 

.91i .939 1.1~ .m .553 1.155 .ws .94a 1.149 .9i2 .943 1.132 

.Q44 ,938 , .'id9 -950 ,954 .943 0959 0943 

.$92 1.005 leCb0 1.305 1.000 .c57 -996 1.011 

1.026 .39F 

,324 .FS4 

1 .PI5 

1.012 0987 e731 

.se5 

.3Yti 1.003 

1. CJ.16 

>!! 

3 .s2 

2 .ti 

*u3 1.c. 

.22 1.0 

.4c 1.0 

, 1.9 

.ic. 1.e 

1.12 1.G 

1.30 1.0 

I.&% 1.3 

1.L4 1.c' 

2.20 1.3 

2.55 1.0 

2.92 1.0 

3.2E 1.c 
CL 

N 

N 

0 0 3.319 

0 052 .@OO 

0 064 1.19c 1.201 

ow5 1.0 1.0:: .oco 1 022 1.0 l.OOC! .958 

TABLE B-2. (Continued) 

1.17F 

1.036 

3.575 3 0698 

3oP22 

1.221 1.244 1.201 1.242 

1.031 3.522 1.004 1.033 

1.021 e965 1.020 

1.014 0959 1.017 

.coo 

1.258 1.221 

e000 1.021 

0959 

4.118 

.009 

1.354 1.360 1.524 

1.103 o000 o08l 

'1.076 0973 

.9,'C .9F2 .9&4 a935 0996 

1.024 0997 1 A25 
I 

1.014 

1.029 

1.044 

TABLE B-2. (Continued) 

e986 -991 1-01: 

le015 1eOC6 

-977 .CGO le030 

.90\i ,189 

.97C e970 

.ooo 

-965 e952 le042 

e957 

e964 e967 

e976 

.CJi 

7 .C75 

'le GOC 

,965 

.:'? c 1 

e 397 

.967 

.915 

1.300 

l.!,ciE 

e Cbl 

. s9E 

le911 

1.SCS e913 

1eC701 e941 

I ,966 

.000 

e9J5 

1.224 .987 

1 .ai0 

.329 .977 

-982 

,970 

0 000 

.?il .?6O 

' .954 

' .963 

e3c3 

e905 e902 

e931 e943 

e965 

e976 

e 987 

-991 1.015 

1 ec09 

-000 le030 

.989 

.969 

-949 1.046 

. c63 

e 799 

e773 

e P,67 

.939 

eOO@ 

-073 

e 981 

le013 

e 974 

e 977 

e 966 

e 000 

e 964 

e957 

e 964 

-913 

e799 .go8 

e864 e386 

e939 

e953 

e978 

.935 leO0R 

1 e003 

e000 1.026 

.9a5 

4966 

e953 1ec44 

.966 

1.2b 1 .GI 1.01F 1.223 , ,977 976 

3 9 1 .E37 .3t!7 .FCC e923 

'TLST 1, PUId 616lC;TtSl 1, Ru~ 6t,7/&TEST 1, QUUP! 517/G TEST IT RUN f34/0 

e909 

eF95 e909 ,519 

,927 e929 eS52 

e966 e969 

eo00 a984 

e992 e995 

e994 e999 1.026 

le015 le014 

e984 e000 1eC30 

.a07 -992 

e900 *97? 

.ooo 

e968 m9tl 1.039 

e 961 

e966 e969 

e984 
TABLE B-2. (Continued) 

1,020 

.F46 

.?dZ 0963 

0300 -968 

1.3~9 e978 

1 .ai)!! 1.3uo 

1.057 1.036 

. 906 

0938 

sL2 1.0 -971 

, -40 1.0 .GOG 

I .5? 1.c .98c 

.75 1.0 .991 

.9L 1.0 1.015 

1.12 1.0 0979 

1.39 1,Ci .9&4 

'1.45 1.9' -472 

,1054 1.0 .c30 

0980 

.cog 

.913 

0918 

.F36 

.971 

-980 

.991 

.F93 

1.010 

*COO 

e951 

.972 

-54 1.0 

11-12 1.0 

'1.30 1.0 

'1.075 1.040 

, 1.004 1.026 

1.CtP 1.040 1.3c1 1.c41 

l.C,27 e000 1.C)CZ 1.3G7 -000 loco6 1.00611.044 a000 loco2 

1.GGl 1.C15 1.016 1.CZ3 11.003 1.027 

I *671 e470 

e666 

0903 

0978 

.987 

984 

.Q89 

1.034 

oOG0 

1 oC13 

0993 

0675 

.935 

$=O =60 =l*EO 

TEST 19 RUN 621/0 

0777 

. 745 

0730 0748 0760 

0916 m913 a934 

.989 ,987 

.OOO -992 

1.012 0986 

0023 1.017 1,006 1.028 

11.063 1.037 

.998~1.017 .OOO 1.007 

1.004 1.015 1 

81.006 1.000 

1 .ooo 

Le23 1.0 eF61 e954 1.043 -958 oF21 1.144 e945 0923 1.141 0961 0924 1.140 

'2.56 1.C .955 e 947 1 .961 0965 

2.92 1.3 .9c5 .963 .FhE 0399 1 .96? .9F3 ; .973 1.002 

i '5.2F 1.0 .T75 ."cl , .97L , 0982 

TELT 1, RbPd 6;C/C TEZT 1, RUh 63?/0iTEST 1, RUPr 6U8/O'TtST 1, RUN 413/0 
TABLE B-2. ( Continued) 

,965 0931 I 

0951 e000 1.139 

.9C6 -935 

,962 

.ooo 

0939 e927 e969 

e960 

.Q91 

.sa4 -999 

iTEST 1, RUN 637/0 TEST 1, RUN 6L3/0 TEST 1, RUN 632/0 TEST 1, RUN 624/0 

X/D P/R e=o =60 =18d ' d=O =60 =le0 8=0 =60 =le0 0=0 

e975 0928 

1.003 a000 1.146 

.Fa6 .941 

.948 .903 

e 000 

0943 e929 0573 

0935 

1 e005 

.9a9 .96i 

oc .?I5 ,74 e .a59 e 868 

0 052: .708 . 944 .820 

.li3 1.0: .97~ ,978 1.07~: .ot5 .977 ieo67,, .96s .9a3 i.c)sa -964 

-22 leO.1.CO1 1.015 ;l.oGc 1.009 '1.013 le515 1 eo10 

046 1.0 .COO 1.007 ! .3bC 1.001 .ooo 1.012 e 000 

.51 1.3 .97C 1.007 j .973 1ecoo e974 1.C16 .97? 

e94 1.3' -943 -964 .947 -558 .943 .918 0953 

1.30 1.C e93h ,934 I ,341 ,941 ' .950 .9L5 0938 

,1.45 1.0: .9ic .F07 , 0736 .9G& 1 -949 0909 .943 

1 e04 1.0' eo36 .3OG i .!IO3 .900 

2.55 1.0, e939 ; ,938 .965 .953 

2.92 1.0. .990 1.OOt' 1.20L 10,311 e099 1.015 1.001 

0 .707 .715 .759 -712 .756 .732 .799 .E25 .SI9 .EO0 

e76 1.C' .956 .994 l.05C; ,367 e388 1.054 a947 e094 leob0 e962 

1.12 1.0 .9LZ ,000 1.133, ,949 .QUO 1.134 .937 -000 1.130 -961 

!Lei5 1.0' eCL3 e924 -131 e$+'; ,922 .?dS, e935 0033 0971. -938 

ee15 

0823 eE18 

0981 1.078 

1 e016 

1 e005 

1 .GI0 

-996 1.059 

.948 

a000 le129 

e 944 

e91 3 

1 e007 1 
TABLE B-2. (Concluded) 

0=0 =6G =180 

TEST 1, RUN 629/0 

1.985 

1.011 8961 8985 

a964 e939 1.005 

8992 0943 

a000 8946 

a961 

2.521 

1.357 

1.113 1.356 1.096 

e"Y4 8947 1 e004 

.Q9& 8944 

.CGC 8947 

.?$4 0351 

.957 .Q51 .9E3 

,765 .945 

8913 .?a2 .30G .922 

/1.311 .9d7 

I .?e; 8964 

1 .3GC 

.713! ,595 .'.do .718 

~ .s:7 

, .9YQ 

.c73 .~a4 

-__ 

0=0 =60 =190 

TEST 1, RUN 611/0 

2.537 

1'.101 

1.159 1.092 1.131 

1.010 ,973 1.c12 

.992 8943 

.ooo 8945 

. 943 0962 8936 

so00 -911 0985 .OOO .910 

8983 ,1.011 .987 

.97~ .7ii; .997 .sa0 .71i 

. 964 1 .Q6Q ,968 

, .ooo 

946 

a963 ' "976 -986 

. 996 , 0.998 

TEST 1, RUN 631/C)!TEST 1, RUN 627/0, 

2.820 2.952 

1 .lb2 1 a180 

1 0251 1.184 1.216,l e246 1.188 1.216 

1.035 .394 1.017'1.333 1.006 1.C11 

.991 8943 1 8993 .944 

.e30 .943 .coo .94* 

.F96 .950 .994 .Q51 

098% 8947 .577, 8987 ,950 s'i82 

a968 ~926 ' .965 .942 

e982 .@OO e905 0984 .OOO 8913 

1.c19 .985 

.964 -967 ,967 .967 

I 

1.012 .989 

.ooo .@GO 

a996 8981 1.840 8995 0939 8713 

8942 1 .943 

.975 ,984 { .974 .9s5 

1 .ooo ,I 8997 
TABLE B-3. BASE AND BODY SURFACE PRESSURE RATIOS (P/P ) FOR ET/SRB CLASS W 

e 987 

e985 e984 e979 

e000 

,963 ,971 ,000 

,989 

,989 

e994 a 

SRB-R ,954 e958 ,947 

,958 SRB-L ,946 ,958 

X/D R/R 8=0 =15 =45 =90 ~270 j 6=0 =15 =45 =90 =270 

TEST 7, RUN 61/1 ~ TEST 7, RUN 72/2 

0 0 e986 ' e989 

'0' e531 e984 ,963 ,980 e989 e986 e984 

10' .a79 e 968 a992 

'0' e969 , 000 a000 

'0' ,992 ,960 e963 e000 e945 e949 ,000 

e033 1.0 e989 ,978 

e583 le0 ,992 ' e991 a 

'0' e931 e983 e983 e978 e 990 ,986 e984 

e250 1.0 ,988 e985 

0 e742 SRR-R e956a ,963 e958 SRB-R e951 e954 e939 

o ,742, e958 SRB-L ,960 ,963 e954 SRB-L e939 e952 

TEST 79 RUN 61/2 TEST 7, RUN 50/2 

992 

,969 eYa9 e981 

e000 

e945 e958 e000 

e979 

,985 

e990 a 

SRB-H e970 e970 e960 

e970 SRB-L e960 e970 

0 0 

'0' ,531 

'0' e679 

'0' ,931 

'0' e569 

'0' .992 

e083 1.0 

e250 le0 

,583 le0 

0 ,742 

0 e742 

0 G 

'C' ,531 

'0' eS79 

'0' e931 

'0' ,969 

'0' e992 

,083 1 e0 

e250 1.0 

e563 le0 

0 e742 

0 e742 

,535 e 987 

.9b4 e984 e961 e 988 e987 ,984 

e9bO m960 e976 ,988 ,987 e979 

9b5 e991 

000 ,000 

e961 ,971 .GOO e942 e953 ,000 

e985 ,979 

e968 ,935 

.991 a e992 a 

SRR-R e948 e959 e948 . SRB-R a952 0955 e940 

,957 SRR-L e946 ,959 e955 SRB-L ,940 ,953 

TEST 79 RUN 6512 TEST 79 RUh 4912 
TABLE B-3. (Continued) 

0 G a992 a959 

'0' a531 ~ a953 .991 ,988 ~ .955 a946 m939 

'0' .679 .995 a959 

~'0' a931 a992 e990 a983 a957 a946 a917 

1'0' -969, a000 a000 

X/D R/R 

0 0 

'0' a531 

'0' a879 

'0' a931 

'0' a969 

'0' a992 

a033 1.0 

0'50 1.0 

.5s3 1.0 , 

I 0 a742, 

0=0 =I5 =45 =90 =279 

TEST 79 RUN ?3/4 

.990 

a991 .989 a986 

a993 

a000 

a991 a989 e978 

a948 a954 a000 

a992 

a991 a990 a987 

a 996 

a000 

a991 a993 a984 

a950 a959 a000 

1 0 .742, .976 SRB-L a966 a975, a981 SRB-L a972 a981 

TEST 79 HUN 86/2 I TEST 79 RUN 6011 
TABLE B-3. (Continued) 

X/D R/RI 0=O =15 =45 =9G =270 ' 8=O =15 =45 =90 =270 

TEST 7, RUN 5112 ' TEST 71 RUN 7112 

0 0 0993 

'0' e531 a993 0985 -976 

'o' .a79 0997 

'0' a531 0996 -988 0963 

'0' 0969, e 000 

'0' 0992 0904 086: e000 

,083 1.0 0964 

,250 1.0 0971 

0563 1.0 ,979 n 

. 994 

0994 0984 0976 

0997 

.ooo 

0996 0986 e000 

0904 0849 .ooo 

.965 

0973 

0982 n 

0 a742 ~ SRB-R .960- -971 0942 SRB-R .960- .977 .949 

0 .742 .965 SRB-L ,963 0935 0970 SRB-L 0968 0942 

TEST 71 RUN 4812 TEST 71 RUN 74/2 

0 0 

'0' 0531 

'0' 0879 

'0' .931 

'9' -969 

'0' 0992' 

0053 1.3 

.?50 1.0 

0583 1.0 

0 0742 

0 0742 

9 0 

'0' 0531 

'0' ob79 

'0' a931 

'0' e969 

'0' 0'992 

0083 1.0 

.25c 1.0 

-583 1.0 

0 0742 

0 0742 

1 oC14 1 .OW 

1.017 1.c10 .959 1.020 1.012 1.002 

1 0319 1.011 e992 1 e026 1.016 0998 

1 0020 1.024 

.030 .ooo 

.937 ,903 .os0 .944 0691 e000 

oSh2 0989 

.385 0990 

-990 a 0993 a 

SRB-R 1.020 l.OZfi 1.010 SRB-R 1.033 1.042 1.023 

1.024 SRB-L 1.003 1.024 1.035 SRB-L 1.016 1.030 

TEST 79 RUN 4112 TEST 71 RUk 85/2 

1.031 

1.634 1,027 1.C17 

1 0034 

.coo 

1.031 1.027 1.013 

e962 0921 .ooo 

1 .ooo 

0994 

0994 a 

SRB-R 1.060 1.067 1.053 

lac59 SR6-L . 1.046 1.062 

1.037 

1 e041 1.032 1.022 

1 e044 

.ooo 

1.044 1.036 1.023 

.961 0919 a000 

1.004 

1 e004 

1.002 a 

SRB-R 1.072 1.076 1.062 

1.071 SRE-L 1.058 1.072 
TABLE B-3. (Continued) 

0 0 

'0' a531 

'0' .879 

'0' m931 

'0' .F69 

'0' e992 

.083 1.0 

.250 1.0 

e583 1.0 

X/D R/RI 0=0 =45 =90 =270 I 0=0 =I5 =45 =90 =270 

I TEST 7' RUN 62/1 I TEST 7, RUN 62/2 

,804 a866 

0802 .803 b793 *864 .ti62 e658 

.811 .871 

a000 .ooo 

.BO1 e802 a761 .a64 a862 a842 

e684 e639 aOG0 a761 a707 .ooo 

e924 I a921 

e939 a .935 a 

, e901 , a901 

loi83 L:2i .938 SRB-R e969 m972 a 0974 

,742'j .979 SRB-L 0949 a981 

~ .250 1.0 .926 

, .583 1.0 s938 a 

0 .742 SRB-R e820 e836 

a936 a 

SUB-R 1.047 1.055 1.0461 

1.055 SRB-L 1.039 1.0601 

' e926 

I .935 a 

.SI1 1 I SUB-R ,961 e965 e961 I 0 .742, .837 SRB-L e791 a8331 e970 SRB-L a940 e972 

I TEST 79 RUN 70/E ~ TEST 7, RUN 47/2 

10 0 

1'0' 0531 

~ '0' a879 

'0' e931 

'0' e969 

'0' ,992 

:a083 1.0 

I.250 1.0 

.93a 

m940 .93a .9~9 

a950 

boo0 

e 946 .93F a910 

.a36 e769 e000 

e921 

m931 

1 .992 

! 1.010 

i 1.007 1.004 e986 

1 e002 1.004 a994 

I b000 i a932 a862 e000 

.953 

~ .941 
TABLE B-3. (Continued) 

X/D R/R' 0=0 =15 =45 =90 ~270 ~ 8=0 =15 =45 =90 =270 , 

I TEST 79 RUN 7512 TEST 79 RUN 59f4 

0 0 1.010 1 a043 

'0' 8531 1.018 1.018 1.008 18051 18045 18036 

'0' .&79 1 e028 18054 

'0' ,931' 1.026 1.019 .OF8 18052 1.044 1.033 

'0' .969 

'0' e992 

.250 1.0 

a583 1.0 

.083 1.0 

0 8742 

0 e742 

0 0 

'0' e531 

'0' .e79 

'0' e931 

'0' .969 

'0' 8992 

8250 1.0 

.0d3 1.0 

sa3 1.0 

0 e742 

0 a742 

0 0 

'0' ,531 

'0' 8879 

'0' ,931 

'0' 8969 

'3' e992 

.083 180 

.250 1.0 

v583 1.0 

0 a742 

3 a742 

8000 8000 

.955 a970 8000 , ,995 e906 .OOO 

e967 .957 

8951 ' ,964 

8942 a , 8941 a 

SRB-R 1,073 1.090 1.072' SRB-R 1.100 1.130 1.704 

1.080 SRB-L 1.071 1,090 1.102 SRB-L 18103 1.121 

18047 ' .791 

TEST 7, RUN S4/2 TEST 79 RUN 56f1 

18055 18049 1.037 

1 e058 

.ooo 

1 e057 1.051 1.035 

.575 a926 -000 

8Fb9 

.965 

8945 a 

SRE-R 1.113 1.133 1.115 

1.115 SRB-L 18103 18129 

TEST 7, RUN 56f2 

8854 

.a46 8837 e841 

e848 

eo00 

.a46 8839 8832 

,740 e664 e000 

8925 

.941 

8953 a 

m795 SRB-L .755 .798 

SRB-R a774 a794 a779 

.783 8771 a777 

.779 8'772 8760 

786 

.oo.o 

-668 0642 8000 

a 924 

8939 

8956 

SRB-R 8565 8540 e557 

0557 SRB-L 0545 8543 

TEST 79 RUN 66f2 

a 

.as8 

. e48 ,839 .a45 

.a44 .a41 .a36 

.a51 

a000 

0733 ,663 a000 

.924 

e939 

b959 a 

SRB-R a795 8797 a782 

e806 SRB-L a765 0801 
TABLE B-3. (Continued) 

e982 

X/D R/R 

0 0 

'0' 0531 

'0' 0679 

'0' e931 

'0' e969 

'0' a992 

a083 1.0 

.250 1.0 

a583 1.0 

0 a742 

a997 SRB-L a972 m9941 

TEST 7, RUN 7612 1 , 1 e017 

1.020 1.016 1.013 1 

1 1 e029 

l 1.029 1,020 1.009 

$=O =15 =45 =90 =270 

TEST 79 RUN 5312 

0942 

e938 .932 m934 

,935 e934 a920 

e841 .734 .ouo 

a938 

.94& 

e960 a 

a941 

a 000 

SRB-R .9a4 .976 .974 

1 .OS6 1.055 1.043 

1.064 

eo00 

1 .os 1.051 1.040 

1 .GO3 a863 e000 

-991 

-961 

s958 a 

SRB-R 1.122 1.145 1.120 

1.132 SRB-L 1.123 1.142 

0 .742 -984 SR6-L 0958 

0 G 1 .OGP 

TEST ?+ RUN 4612 

'0' e531 1.013 1.009 1.006 

'0' .679/ 1.016 

'0' .969 .ooo 

'0' ,992 ,939 ,830 .Olio 

1'0' e931 1.013 1.008 -996 

'.083 1.0 -967 

,.250 1.0 I ,954 

1.583 1.0 e962 a 

I c .7d SRB-R 1.077 1.002 

1.073 1.070 1.065 

1 e078 

.ooo 1 1.079 1.070 1.063 

1 e030 .a95 .ooo 

1.009 

e973 

a961 a 

SRB-R 1.156 1.185 Ia156( 

la166 SRB-L 1.161 1.179; 

0=0 =15 =45 =90 =270 

TEST '79 RUN 69/2 

946 

a933 .931 m936 

0937 

.ooo 

.935 a935 a927 

.a33 a727 .ooo 

m939 

0946 

0958 a 

1 

SRB-R e996 0990 .991! 

0 .742/ 1.079 SRD-L 1.067 l.OSl/ 1.109 SRB-L 1.105 1.106i 

TEST 7, RUh 43/3 I TEST 79 RUN 79/3 

Io 0 1.046 I 1.063 1 

'0' a531 

'0' ,679 

'0' a931 

'0' ,969 

'0' e992 

0063 1.0 

,250 1.0 

sa3 LO 

0 ,742 

0 e742 
.- 

~ 

TABLE B-3. (Continued) 

e974 1.005 

SRB-R aF29 a822 .d14 SREi-R 1.002 a99d 

1.055 .E42 1.004 SRB-L 

TEST 7, RUN 4513 

.640 SRB-L 

TEST 71 RUh 5412 

i X/D RIR 0=0 =I5 =45 =90 ~270 fj=o =I5 =45 =90 ~270 , 

TEST 79 RUN 5512 TEST 79 RUN 5513 

I) 0 a 787 ,853 

'0' m531. m750 .77a .769 85 1 .a49 .838 

'0' a879 786 a857 

'0' e931 0777 0772 -734 ,850 .a48 e812 

'0' a969 e000 .ooo 

'0' .992 ,675 e651 e000 .757 ,673 .OOO 

a083 1.0 a933 e932 

.250 1.0 .555 , a953 

.5a3 1.0 ,965 a a965 a 1 0 ,742 SRB-R a517 w4Y7 e512 SRB-R ,763 a801 a773 

0 a742 a506 SRB-L 

TEST 79 RUN 

0 G a668 

'0' e531 e806 

'0' ,879 a872 

'0' a931 ,866 

'0' a969, ,000 

'0' 0992' -772 

,083 1 .o .939 

.250 1.c 0959 

a583 1.0 ~ ,969 

e459 .5O6 .806 SRB-L m756 a815 

671 2 TEST 7, RU~ 68/2 

.E60 .e51 

e862 a823 

-679 e000 

0 0 

'0' a531 

'0' e879 

'0' a531 

'0' 0969 

'0' 0992 

.003 1.0 

0250 1.0 

1 0 a742 

1 0 ,742 

.sa3 1.0 

.939 

.944 e940 ,926 

e953 

eo00 

a948 e944 .900 

.a62 .737 a000 

.953 

e962 

~ .972 a 

,948 

e552 ,950 e954 

e957 e953 0916 

.a75 e753 .ooo 

.Y45 

0953 

.963 a 

*96? 

a000 

SRB-R 1.013 1.012 1.008 

1.014 SRB-L a966 1.008 

1.009 

1.023 1.027 la007 

1.036 

a000 

1.028 1.006 

.969 .842 .ooo 

.976 

a964 

. 968 a 

1.032 

SRB-R 1.103 la117 la105 

1.110 SRB-L 1.101 1.121 
TABLE B-3. (Continued) 

0=0 =15 =45 =90 =270 

TEST 79 RUN 77/3 

1.013 

1 .035 1.036 1.017 

1.04L 1.039 1.015 

.9&8 0850 8000 

e966 

1.047 

.ooo 

a971 

X/D R/R 0=0 =15 =45 =90 =270 

TEST 79 RUN 44/2 

1.048 

1 .076 1.068 1.046 

1.082 1.068 1.041 

1.037 .889 .ooo 

1 e005 

1 a087 

.ooo 

b973 

0 0 

'0' .531 

'0' e879 

'0' m931 

'0' e969 

'0' e992 

.oa3 1.0 

e250 1.0 

sa3 1.0 

0 a742 

0 ,742 

0 0 1 a055 a61 5 I 

"C' ,531 1.086 1.083 1.056 a596 sa8 .6i2 

'0' .879 1 a096 .580 

' .sa9 a601 e619 

I m578 

'0' ,931, 1.0'99 1.083 1.059 

'0' e963 eo03 . '0' ,992 1.061 e903 e000 I .617 ,630 a619 

I e033 1.0 , 1.023 , 0966 

.250 1.0 e985 .9a5 

.583 1.0 .973 a 1.042 a 

0 a742 SRB-R 1.180 1.215 1,183 SRB-R a358 e362 .370 

0 e742 1.2'21 SRB-L 1.134 1.216 a345 SRE-L .349 0345 

TEST 79 RUN 164/4 TEST 7, RUh 16312 

3 i, . E37 1 e036 

'0' a531 e614 -815 m836 ,990 e997 1.026 

a 679 e806 m994 '0' 

'0' .931{ .do3 m808 e840 

'0' e969 -801 . 967 

.995 e997 1.036 

I '0' aF92, od3P 0690 e791 a 921 m850 a954 

i .OB3 1.0 .956 .961 

-250 1.0 .Y74 ,974 ' e583 1.0 ' 1.044 a 1 a056 a 

0 .742, SkB-R a961 e943 a970 SRE-R 1.011 1.085 1.018 

l, 0 .742' .955 SRB-L e956 ,957 1.031 SRB-L 1.011 1.103 
BE@=-- 

'0' ,531 1.145 1.135 1.135 1 a032 1.085 1.079 

'0' .879 1 e145 1 .I10 

'0' m931 1.149 1.131 1.129 1.130 1.086 1.089 

'0' .969 1 e137 1 a096 

'0' .992 1.071 .962 1.071 1.055 ,917 1.012 

0083 1.0 .979 a 984 

e250 1.0 ,978 ,988 

.563 1.0 1.046 a 1 e056 a 

0 e742 SRB-R 1.122 1.249 1.125 SRB-R le155 1.338 1.161 

0 ,742 1.164 SRB-L 1.117 1.271 i.isa SRB-L 1.094 1.258 

0 C .$e9 ,987 

TEST 79 RUN 10912 TEST 7, RUN 11412 

"0' ,531 .969 a933 .9E1 ,987 .983 .9ao 

'0' .k79 e989 .9a6 

'0' .969~ e976 .975 

'0' ,931 e987 .wo .972 e996 a979 e971 

'0' ,992 e941 .F44 -962 e942 a944 .963 

.083 1.0 .F77 e975 

,250 1.c .9&5 .984 

a533 1.0 .ooo a a000 a 

0 .797 SRB-R ,956 m955 ,953 SRB-R .941 .94a .924 

o ,797 .95a SRB-L a953 .952 ,948 SRB-L a930 a947 

TEST 79 RUN 12112 TEST 7, RUN 10913 

0 0 .990 .992 

'0' 0531 e989 ,984 ,963 a 992 e988 a985 

'01 .a79 a990 e993 

'0' a931 e990 e963 e977 e992 m986 a978 

'0' a969 e978 .gal 

'0' -992 aG47 a949 e967 .950 a953 ,971 

.083 1.0 e977 .979 

.250 1.0 .965 m986 

a583 1.0 .ooo a .ooo a 

0 .797 SRB-R .971 e973 e958 SRB-R .9a9 .993 .9~3 

0 e797 a972 SRB-L a961 .972 ,991 SRB-L a977 e991- 

TABLE B-3. (Continued) 
TABLE B-3. (Continued) 

- 

X/D R/R 0=0 =15 145 =90 =270 0=0 =15 =45 =90 =270 

TEST 79 RUN 11O/I TEST 79 RUN 113/2 

0 0 e967 .909 

'0' a531 a965 .955 .947 990 ,980 e972 

'0' a679 a 967 .994 

'0' a931 .967 m956 .927 .991 .981 .959 

'0' a969 e951 .97Y 

1'0' e992 e860 ,847 .891 

' .083 1.0 .Y37 

0 .797' l.02P SRP-L 1.030 1,007; 1.057 SRB-L 1.072 1.087 

TEST 7, RUN 122/2 1 TEST 79 RUN 115/2 

' e893 -880 m927 

0952 

0 0 -620 I a920 

'0' ,531 0815 *e04 ,809 1 a919 e909 a905 

"0' a879 0811 

!'O' .931 -816 e803 .7&2 I ,917 e907 e892 

1'0' .969 .794 a907 

*o' .wz i$%i .660a .735 1 .a08 a779 n854 

091 6 I 

I 

I , .ob3 1.0 .a86 

'0250 la0 , e904 e 908 

j 0 .797 SRB-R a700 e703 .690 SRE-R 0893 e914 0886 

0 ,797 .698 SRB-L e669 a698 e894 SRE-L a872 e900 

l 

a583 la0 1 .ooo a 

e250 1.0 !I a956 

.563 1.0 moo0 

e968 

.ooo a 
TABLE B-3. (Continued) 

' X/D R/R: 8=0 =15 =45 =90 =270 , 0=0 =15 =45 =90 -270 

TEST 7, RUh 120/2 TEST 79 RUN 12213 

0 0 1 e003 1 e053 

'0' e531 le014 e995 e9&l 1 e052 le044 le037 

'0' e679 1 e020 1 e053 

'0' e931 le021 le004 e986 1 e055 le044 le031 

'0' e969 1 eo14 1 e047 

'0' e992 e939 -892 e965 e984 a937 le007 

e083 le0 e937 e982 

e250 le0 e928 e965 

e583 1.0 eooo a e000 a 

0 e737 SRB-R 1.069 1.079 le074 SRB-R le137 le178 le137 

0 e797 le059 SR6-L 1.054 1.068 1.132 SRB-L le172 le164 

TEST 79 RUN 115/1 TEST 79 RUN 116/2 

0 0 e777 e894 

'0' e531 e766 ,753 .762 .a93 

'0' eb79. e756 e888 

'0' e931 e768 e747 e718 e890 ma79 e867 

'0' e969 e 734 e675 

'0' 0992 e664 .641 .71F ,792 e712 e893 

e083 le0 .5G7 ,917 

e250 le0 e93! .93b 

e583 le0 eooo a eooo a 

e881 e884 

0 e7971 SRB-R ,622 e614 e620 SRG-R e895 e905 e891 

0 e7971 e614 SRB-L e612 e610 e879 SRB-L e857 -890 

1 TEST 7, RUN 119/2 TEST 79 RUN 118/2 

0 0 

'0' ,531 

'0' e879 

'0' e931 

'0' e569 

'0' e992 

e063 1 e0 

e250 la0 

e533 1.0 

0 e797 

0 e797 

1 eo04 

1 e022 le002 e960 

1 e029 

1 eC31 le011 e989 

1 e022 

e947 e854 e306 

e959 

e955 

e 000 a 

SRB-R leG83 lelb3 le090 

1.068 SRB-L . le067 le092 

e755 

e 735 e721 e727 

,722 

e734 e712 e684 

e709 

e651 e646 e709 

-923 

e955 

eooo a 

SRB-R e538 e520 e549 

e539 SUB-L e538 e531 
TABLE B-3. (Continued) 

, X/D R/R 0=0 =15 =45 =90 =270 0=0 =15 =45 =90 =270 

TEST 7, RUN 117/2 TEST 79 RUN 118/3 

9 0 0897 1.002 

'0' e531 e893 .880 .877 1.025 1.009 e977 

'0' m879 e 887 1.029 

'0' .931 .E92 0876 e856 1 a030 1.016 0989 

'0' .969 ,877 1.025 

'0' -992 ,811 0727 e832 , m957 0855 0964 

0085 1.0 ' 0926 ' a963 

e250 1.0 0953 / a961 

0583 1.0 e 000 a moo0 a 

0 

"'0' 

'0' 

"0' 

'0' 

'0' 

. Ob3 

e250 

. 563 

0 

0 1 eo71 

0531 1.065 1.067 1.044 

0879 : 1 a090 

e931 leOe9 le070 1.044 

e969 1 eCd6 

0992 le032 m910 1.012 

le0 1.009 

1.0 0932 

1.0 ' .000 U 

0797 SRB-R 1.169 le232 ~~ ~ 

0 e797 1.174 SRB-L le157 

TEST 79 RUN 172/2 

' .632 ! .612 0606 a627 

,605 0611 a642 

e600 

e61 1 

! e605 e616 e629 

-923 

,956 I 

1 0038 a 

1 m161 i SRB-R e35b e337 a352 

1.211 e356 SRB-L 0349 0348 

' TEST 79 RUN 17112 

0 0 lee10 , 1.129 

'0' e531 m971 e979 0997 1.192 1.171 1.119 

'0' 0879 e971 1 0199 

'0' e931 0963 e965 1.001 1.187 1.170 1.118 

'0' 0969 960 1 0190 

'0' e9P2 0921 e849 0947 1.118 m985 1.120 

e250 le0 0964 0963 

;e083 le0 ,941 .gab 

,0553 le0 I 1.033 a 1 e034 U 

0 07971 SRB-R e865 0914 e880 SRB-R 1.040 1.187 1.026 

O 07971 ,832 SRB-L 0842 ,934 1.041 SRB-L 0987 1.206, 
&&&- 

0 e797' 

0 e797 

0 0 

'0' e531 

'0' e679 

'0' e931 

'0' e969 

'0' e992 

e083 le0 

,250 le0 

,563 le0 

0 e843 

0 e843 

0 0 

'0' e531 

'0' e079 

'0' e931 

'0' e969 

'0' e992 

,083 le0 

,250 le0 

,583 le0 

0 e643 

0 e813 

TABLE B-3. (Continued) 

CI 

w 

W 

X/D R/R!j 8=0 =15 =45 =9cr =270 

TEST 7, RUN 170/5 

3 G 1 e2G4 

'0' e531 le247 le189 le152 

'0' e679 1 e246 

'0' e931 le262 le194 le137 

'0' e969 1 e239 

'0' e992 le213 e993 1.122 

1 e025 

m95s 

1.022 a 

SRB-R 1.208 le412 le196 

le299 SRB-L le180 le425 

TEST 79 RUh I26/1 

e985 

e902 .963 e9bl 

e9bl e981 e97L 

e960 e965 e976 

.979 

e987 

e991 a 

,084 

e979 

SRB-R e952 e968 e962 

a954 SRfi-L e961 e966 

TEST 7, RUN 126/2 

e967 

e954 e985 .983 

e983 e964 e979 

e986 

e981 

e 963 eS70 e9bI 

e981 

e 967 

e991 a 

SRB-R e959 e956 e953 

e955 SRB-L e955 e954 

TEST 7, RUN 137/2 

.991 

e989 e909 e986 

.9a9 e988 e.976 

.949 e954 e973 

e977 

e986 

e991 

e993 , 

e983 

a 

SRB-R e959 e958 e953 

e956 SRB-L e954 e956 

TEST 7, RUN 13E/3 

e 991 

e990 e992 e983 

e993 

e984 

e 990 e989 e977 

e950 e956 e975 

e976 

e984 

e990 a 

SRB-R e973 e974 e969 

e968 SRB-L e970 e972 
TABLE B-3. (Continued) 

0 0 

'0' .531 

'0' ,679 

'0' ,931 

'0' .969 

'0' a992 

.oa3 1.0 

, a250 1.0 

' xfD R/RI g=o =15 =45 =90 =270 I 0=0 =15 =45 =90 =270 I TEST 79 RUN 14811 I TEST 7, RUN 12912 

e 963 

e959 ,955 a942 

.963 a959 a911 

-842 .aao 

.967 

a955 

-858 

e928 

! 

'0' .931 1.000 1.001 e968 

)'!I' -969' .996 

'0' -992 m913 e915 .943 

.oa3 1.0 .959 

a250 l.@ 974 

.5a3 1.0 1 .9a3 a 

0 0843' SRB-R a963 a972 .956 

a982 

.978 e978 e965 

a984 

,979 a978 e945 

a971 

m898 a900 ,926 

a951 

m969 

e981 a 

SRB-R -873 -697 a868 

1 e039 1.036 1.009 

1 a033 

0961 m961 a983 

. 989 

.997 

.999 a 

SRB-R 1.044 1.044 1.044 

I 

o .e43 .a59 SRB-L ~843 m862; ~884 SRB-L .862 .a91 

TEST 77 RUN 136f2 TEST 7, RUN 139/2 

O ,6431 -963 SRB-L .951 .967, 

I TEST 79 RUN 147/1 

10042 SRB-L 1.038 1.046 

TEST 7, RUN 130/2 

e925 a 

SRB-R .689 .69a .689 1 ~~~~, .692 SRB-L -6bl s6Y7 

e927 a 

SRB-R .765 a788 a791 

a778 SRB-L 0755 0786, 
TABLE B-3. (Continued) 

X/D R/R 0=o =15 =45 =9C =270 ' 0=0 =15 =45 =90 =270 

TEST 7, RUN 135/2 TEST 79 RUN 140/2 

0 0 

'0' .531 

'0' a879 

'0' e931 

'0' e969 

'0' ,992 

e083 1.0 

.250 1.0 

,583 le0 

0 a843 

0 .843 

0 

'0' 

'0' 

'0' 

'0' 

'0' 

.083 

e253 

. 583 

,955 

e956 

e958 

a561 

sb98 

,963 

e955 

.919 

e92L 

SRB-R 

e959 SRB-L 

TEST 79 RUN 

' 1.034 

.957 .951 1 .Ob0 

.959 e940 1 a044 

.836 ,887 e981 

' ,960 

.943 

a a927 

e957 a970 ,990 

.947 .974 1.093 

147/2 TEST 

0 1 .ob2 

0531 1.065 1.055 le047 

e879 1.070 

-931 le067 1.060 1.042 

e969 1 .Ob5 

e992 le010 .970 ,998 

1 .o .991 

1 .o e 968 

1 .o ,935 a I 

.843 SRB-R 1.140 1.178 1.1401 

.843 ~ 1 .I49 SRB-L le122 1.152 

1 TEST 7, HUN 131/2 

0 c 

'0' a531 

'0' e879 

'0' e931 

'0' e969 

'0' e992 

e083 1.0 

a250 1.0 

,583 1.0 

0 a643 

0 a843 

e866 

.a35 e828 .827 

e838 

e830 e829 e810 

.a20 

,729 e670 a825 

e911 

.967 

e956 a 

SRB-R e738 a751 e743 

e729 SRB-L e712 e752 

1.035 1.023 

1 a045 

1.040 

1.039 le019 

e942 .973 

a 

SRB-R 1.081 1.106 1,089 

SRB-L 1.081 1.102 

7, RUN 146/1 

e784 

766 ,765 a759 

m772 

.7'5 4 

e762 .765 .73a 

e671 e643 a792 

903 

.938 

e856 a 

SRB-R e632 e623 e631 

*622 SRB-L e619 e623 

TEST 7, RUN 134/3 

e944 

.944 e942 e937 

.944 -e945 e928 

e949 

8939 

. a47 e771 e896 

a971 

e946 

e949 a 

SRB-R m952 a963 e980 

.935 SRB-L e937 a957 
TABLE B-3. (Continued) 

. 

X/D R/R 

'0' a531 0726 0719 0731 . 794 0791 a809 

IO' 

'0' .931' .711 0710 0711 ~ .?a9 0792 08-05 

"'0' 0992' 0650 0649 0796 0708 0666 e828 

.879 ' 0724 . 799 

'0' 0969' a710 .7ao .. 

0083 1.0 0922 I 0921 

0250 1.0 I ,957 0962 

0583 1.0 I .965 a I 0966 a 

0 0843' SRB-R .566 -534 .559' SRB-R 0745 e749 0758 

0 0 

'0' 0531 

'0' 0879 

'0' 0931 

'0' 0969 

'0' 0992 

0063 1.0 

0250 1.0 

e563 1.0 

e531 ! IO' 

! '0' 0879 

1 IO' 0931 

'0' 0969 

'0' 0992 

..Od3 1.0 

,250 1.0 

0=0 =15 =45 =9G =270 I 8=0 =I5 =45 =90 =270 

TEST 79 RUN 142/2 I TEST 79 RUN 146/2 

0931 0937 0939 1.055 1.044 1.026 

a932 0941 0929 '' 1.062 1.048 1.024 

0840 -767 .a97 r 0997 0881 a957 

0932 

0961 

0943 I 1.065 

0927 I 1.061 

.976 

1.040 

1.048 1.034 1.019 

1.054 

1 0053 1.037 1.013 

1.050 

-568 0876 0956 

e972 

0963 

0556 a 

1.068 

1.066 1.058 1.049 

1 0071 

1 a077 1.061 1.037 

1 0069 

1.021 0906 e983 ~ 0998 

. 973 

1 0957 a 
EL@- 

TABLE B-3. (Continued) 

CI 

P 

w 

X/D R/RI 0=0 =15 ,=45 990 =270 1 0=0 =15 =45 =90 ~270 

' TEST 7, RUN 14512 1 TEST 7, RUN 154/1 

0 0 1 e087 a601 

'0' a531 1.096 1.080 1,062 580 a566 e584 

'0' 0879 1.101 e569 

'0' ,931 1.102 1.083 1.054 .570 a561 .587 

'0' e969 1.102 w570 

'9' e992 lac55 a921 e986 m636 a634 a668 

a083 1.C 1.011 e921 

a250 1.0 e981 5968 

a583 1.0 a969 a 1 a047 a 

SRB-R 1.162 1.229 1.159 SRB-R ~319 8323 a323 

1.199 SRB-L 1.165 1.204 0317 SRB-L e349 e332 

TEST 79 RUN 156/4 TEST 7, RUN 155/2 

0 0 

'0' a531 

'0' e679 

'0' 0931 

'0' e969 

'0' ,992 

e083 1.0 

a250 1.0 

,563 1.0 

0 .643 

0 .el43 

0 0 

'0' a531 

'0' a879 

'0' 0931 

'0' .969 

'0' a992 

.983 1.0 

,250 1.0 

"583 1.0 

0 0643 

- r) .a43 

0842 

e823 e823 eb41 

e812 

a819 a808 a860 

e809 

0754 .687 ,791 

m917 

e968 

1 e047 a 

SRB-R m681 a646 a650 

e615 SRB-L ,635 .672 

TEST 7, RUh 154/2 

1.1 00 

1.090 1.097 1.090 . 

1.130 

1 e146 1.105 1.087 

1 m063 .947 1.020 

1.137 

e954 

e976 

1 a047 a 

SRB-R 1.090 1.201 1.082 

1.146 SRB-L 1.093 1.241 

1 e060 

1.028 1.027 1.059 

1 .O4O 1.045 1.085 

1 a039 

1.029 

e902 1.002 

a , 1.034 

SRB-R e682 e967 ,848 

a672 SRB-L .a50 .966 
TABLE B-3. (Continued) 

'0' a969 

1'0' e992 

a121 1.0 

'e017 1.0 

e052 1.0 

0 ,833 

o .a33 

X/D R/R 

0 0 

'0' ,531 

'0' a879 

'0' a931 

'0' e969 

'0' .992 

.017 1.0 

no52 la0 

.121 1.0 

1.008 

e983 .9a5 .959 

m993 

1.006 

la006 a 

SRB-R 1.021 1.013 1.003 

1.01~ SRB-L 1.002 1.017 

0=0 =15 =45 -90 =270 

TEST 8, RUN 1 

980 

.977 .9a4 ,985 

' a990 

0958 

,988 a985 ,968 

e925 .922 ,968 

e952 

a965 I 

1.002 

.985 e995 a996 

a 996 ,993 .994 

.931 -935 m972 

.995 

a956 

8959 

a973 

1 0 .E331 SRB-R -951 ,958 eF5O' SRB-R .954 .978 .945i 

,972 a ~ .933 a 

i 0 .633 

0 0 

1'0' a531 

'0' .879 

'0' ,931 

!'9' .F69 

1.017 1.0 

'e052 1.0 

0121 1.0 

'0' ,992 

a945 SRB-L ,945 a951 

TEST 69 RUN 31 

1 .GO7 

1.012 1,010 1.005 

1 e013 

e 987 

1.016 la005 .997 

e960 e957 m9bO 

a982 

m990 

.994 a 

.976 SRB-L a949 0973, 

TEST 89 RUN 20 1 

1 a019 

1 e016 1.014 1.018 

1.015 , 

1.01 5 1.010 1.016 1 

a980 

,955 e967 s980 

e986 

,994 

.99a a 

SRB-R 1,013 1.017 .99U 

1.015 SRB-L .997 1.014 

1 .041 

1.038 1.037 1.045 

TEST 8, RUN 21 

1,040 

1 e019 

1 e043 1.023 1.039 

.996 a999 .980 

1.015 

1 e023 

I .020 a 1 

SR8-R 1.061 1.061 la056 

le059 SRB-L 1.052 1.059; 
TABLE B-3. (Continued) 

1 0 ,833 

'C 

,847 SRB-L e839 0853 e943 SRB-L 

TEST 01 RUh 24 TEST 89 RUN 6 

X/D R/R 

0 0 

'0' .531 

'0' ,879 

'0' .931 

'0' a969 

'0' e992 

.017 1.0 

,052 1.0 

0121 1.0 

0 a833 

$=O =15 =45 =90 =270 0=0 =15 =45 =90 =270 

TEST a, RUN 2 TEST 8, RUN 7 

.928 a985 

.936 e932 e927 1 e006 1.009 ,962 

0957 0946 e879 1 a013 1,015 .940 

-790 .690 e849 e866 a866 ,896 

e844 a901 

.a36 a936 

a918 a a 966 

.957 1.012 

a 936 996 

U 

SRE-R a835 -849 e832 SRB-R .946 ,937 .875 

0 0 

'0' .531 

'0' 0879 

'0' .931 

'0' e969 

'0' ,992 

.017 1.0 

.os2 1.0 

.121 1.0 

0 ,833 

0 .ti33 

0 0 

'0' "331 

'0' e879 

'0' 0931 

'0' a969 

'0' a992 

a017 1.0 

.os2 1.0 

,121 1.0 

0 a833 

C a833 

1.012 

1.041 1.026 1.0C9 

1 e039 

1.022 

1 .Ob4 1.047 .9Y1 

e913 ,886 e868 

a940 

964 

a980 a 

SRB-R 1.026 1.010 -974 

1 e045 

1 a068 1.049 1.030 

1 e068 

1 e070 1.064 1.038 

1 e043 

a950 a924 a850 

a970 

e991 

1 a003 a 

SRB-R 1.108 1.092 1.073 

1.C2O SRB-L .955 1.0151 1.099 SRB-L 1.055 1.001 

TEST b, RUN 25 1 TEST 8, RUh 8 

1 e074 

1 SOY3 1.078 1.074 

1 -090 

1 e097 1.102 1.055 

1 e072 

m990 a992 e849 

1.009 

1.026 

1 e026 

SRB-R 1.142'1.127 1.113 

1.135 SRB-L 1.106 1.131 

1.087 

1 .136 

1.111 

e995 

1.013 

1.030 

1 a037 

1 e156 

1.100 1.089 

1.115 1.104 

1.015 ,883 

I .loo 

1 a085 

a 

SRB-R 1.166 1.157 1.137 

SRB-L 1.130 1.150 (0 

. 
TABLE B-3. (Continued) 

X/D R/R 

0 0 

'0' ,531 

'0' ,879 

'0' e931 

'0' e969 

'0' .992i 

.017 1.0 

.os2 1.0 

,121 1.0 

0 .E33 

0=0 =15 =45 =90 =270 0=0 =1S =45 =90 =270 

TEST 8, RUN 17 TEST 8, RUN 15 

.779 w927 

,612 .791 .7b? .9?l a967 e934 

-809 e981 

,822 a839 0756 m980 .989 .938 

a765 e971 

.604 .570 .?ti9 667 a766 e757 

.a37 a 863 1 

a88C a902 , 

1 

.893 a I .92s a 

SRB-R .733 .755 .7281 SRB-R ,943 .938 .891' 

0 .8331 .720 SRB-L a 71 2 

I TEST c, RUN 27 

,017 1.0 

.052 1.0 

.121 1.0 

0 a633 

.735[ .926 SRB-L m8S3 .924! 

1 TEST be RUN 17 1 

.Sa3 

a907 

e919 a 

SRB-R 1.039 1.G35 1.003 

1.047 e766 

a 

SRB-R 1.239 1.255 1.233 

a833 1.238 SRB-L 1.217 1.231 

1.079 

1 a077 1.096 1.125 

1 a088 

1.094 1.132 1.114 

1 

1 

1 e091 

1.025 '1.010 .801 

,997 1 

e996 1 

,975 a 

SRB-R 1.163 1.172 1.162: 

1 .177 1.148 .625 

1.192 I 1 a179 

l 1 .143 a 

1.325 SRB-L 1.295 1.312; 

SRB-R 1.283 1.306 1.273; 

0 .S33( 1.033 SRB-L 1.012 1.0221 1.171 SRB-L 1.157 1.17'J 

I TEST &I~ GUN 26 I TEST 8, RUN 19 

0 0 1.144 

'0' ,531 1 1.137 1.125 la129 

'0' .879l 1.133 

'0' -931 1 1.156 

'0' e969 1 .I38 

la172 1.124 

1.200 

1 a208 1.194 1.224 

I 

1 a196 

1.204 

1.209 1.225 1.205 I 
0 0 

'0' e531 

'0' -879 

'0' m931 

'9' .F69 

'0' e992 

eo17 1.0 

e052 1.0 

a 1 

SRB-R -834 -634 -7701 

a 

SRC-R e634 e653 e620 

TEST 29 RUN 4 TEST 8, RUN IO 

e757 e866 

-753 m764 e769 e855 ma73 e850 

e791 e774 e747 e856 e870 m827 

e 790 e 868 

692 e779 

m5Y2 e630 e730 e598 e619 e720 

e672 e907 

mFZ1 ~ -950 1 

9 0 

'3' e531 

'0' e875 

'0' e931 

'3' m969 

'0' e992 

eo17 le0 

eo52 1.0 

e121 1.0 

0 e833 

0 e833 

e 898 

.YO8 .e98 e897 

m9G9 -930 e875 

e918 

m824 

e634 m638 e740 

e918 

-968 

U e 997 

SRB-R m923 m8F9 e855 

m8Y4 SRB-L e846 e892 

m992 

1 eo04 le019 e985 

1 e029 

1 e025 le032 e961 

-990 

e795 m693 e727 

m937 

e987 

1 mol7 a 

SRB-R le080 1.080 1.087 

le068 SRB-L le046 le080 
TABLE B-3. (Continued) 

- 

I 

X/D R/R 

0 0 

'3' e531 

'0' ,879 

'0' .931 

'0' e969 

'0' .992 

.017 1.0 

.052 1.0 

.121 1.0 

0 ,833 

0 .633 

0 (i 

'0' .531 

'0' .E79 

'0' .931 

'0' a969 

'0' e992 

.017 1.0 

.052 1.0 

0121 1.0 

0 ,631 

0 ,631 

0 G 

'3' e531 

'0' .875 

'0' .93i 

'0' e965 

'0' .99; 

.017 1.0 

.os2 1.0 

.121 1.0 

0 .83: ~ 0 083: 

0872 

,873 .YO5 e838 

,787 

a624 0641 e675 

.927 

e987 a 

.970 

SRB-R e977 e962 0955, 

.952 SRB-L .921 09471 

fl=O =15 =45 =90 =270 

TEST 6, RUN 23 

1 0057 

1.095 1.076 1,062 

1.096 

1 .I05 1.114 1.044 

1 e092 

.994 e832 a739 

.998 

1.018 

1 .GZ5 a 

SRB-R 1.170 1.137 1.171 

1.173 SRB-L 1.156 1.196 

TEST 8, RUN 3 

.712 

0683 a709 e762 

,662 a712 0717 

.599 -627 a657 

,942 

. 974 a 

o71R 

-615 

.a92 

SRB-R e564 .a574 a545 

-557 SRB-L m555 a565 

TEST 09 RUN 30 

.a44 

-628 me20 e844 

a827 

0828 .e37 .a08 

e614 ,638 ma 

-716 

e915 

0959 

.983 a 

SRB-R ,899 ,886 .84! 

a913 SRB-L s872 091( 

0=0 =I5 =45 =90 ~270 

TEST 8, RUN 11 

1 a182 

1.131 1.185 1.173 

1-0210 1.196 1.127 

1.202 

1 e203 

1.172 . a965 0715 

1 .lkl 

1 0142 

1 a109 a 

SRB-R 1.296 1.348 1.293 

1.355 SRB-L 1.301 1.383 

TEST 89 RUN 12 

e850 

m852 

a834 

e622 

e91 3 

0964 

e984 

a935 

TEST 

a839 0869 

e854 

a848 a825 

-765 

.640 .616 

a 

SRE-R a907 a908 0877 

SRE-L s919 0925 

8, RUN 26 
TABLE B-3. (Concluded) 

'0' -969: ~ 1rJ' 0992' 

0317 1.0 

0352 1.0 

0121 1.0 

I) .a33 

3 0833 

XID R/R $=o =15 =45 =90 =270 jJ 0=0 =15 =45 =90 ~270 

TEST t, RUN 32 TEST 8, RUN 13 

e971 

a792 

.91R 

.F74 

a991 

SRB-R 

1.126 SRB-L 

0 0 0941 a951 

'0' a531 nF36 0925 0951 e960 ,929 .9a5 

'0' 0879, .92a a963 

'0' e931 0933 0972 m923 .957 0929 1.007 

'0' .969 0867 e923 

'0' .992, m690 e660 0687 0707 a660 a649 

e017 1.0 ' e926 e921 

0052 1.0 .970 . 973 

.121 1.0 0987 a .994 a 

0 0833' SR6-R 1.036 1.016 1sOU6 SRB-R 1.094 1.081 1.091 

0 e833 1.007 SRB-L 1.001 1.007 1.072 SRB-L 1.080 10060 

~ TEST 6s RUN 29 ' TEST 8s RUN IO 

1.133 

,984 leOoe ' 1.143 1.163 1.245 

1.156 

0990 .995 ' 1.173 1.190 1.221 

1.165 

1.112 e916 0690 

1 m074 

1.042 

1.112 1.128 lol(i3 SRB-R 1.244 1.327 1.220 

1.276 1.376 

a 

8= -4 5 
TABLE 3-4. 

0=0 =9u =270 

TESTlC, RUN IO4/O 

e921 e922 e922 

a970 

1.001 

1 e026 

1 eCi4 

*GOO 

BASE AND BODY SURFACE PRESSURE RATIOS (P/ P ) FOR SRB-ALONE CLASS a) 

0=0 =90 =270 0=0 =90 =270 

TESTlG, RbN 105/0 TEST109 RUN 106/0 

a933 e933 e933 e945 .945 a945 

e975 981 

1 e004 1 e007 

1 e027 1 e029 

1 ,025 1 e026 

, e000 e 000 

X/D R/R 

0 .81 

e121 1.0 

e360 1 e0 

0599 le0 

e759 le0 

le002 1.G 

0=0 =90 =270 

TEST109 .RUN 107/0 

a953 a953 a953 

.964 

1 e009 

1 e030 

1 e027 

e000 

1 e007 

TEST109 RUN 100/01 

1.020 

1 e086 

1 e142 

1e135 

e956 e956 .957! 

000 

,le246 1.U 1.039 i 1 .040 1 e044 1 eo34 

'TESTlu, RUN 96/0 TEST109 RUN 97/O TEST109 RUN 98/O TESTl(1, RUN 99/1' 

0 .01' e645 e632 e642, e757 e745 e757 e860 e844 e861 le009 e995 IeOI? 

e121 1.0 leltS I1 el62 1.162 1e170 

e363 1.G ,le267 ' 1 e263 1 e262 1 e262 

e59Y le0 le313 1 e31 1 1 e 300 1.299 

.759 1.0 1.269 1 e272 1 e262 1 e256 

1.602 1.0 .COO .oeo ' a000 e 000 

1.246 le0 1eOb6 1.016 1 e007 1e009 

TEST169 RUN 92/0 TEST109 RUV 94/1 TEST109 RUN 95/0 TEST109 RUN 8812 

0 e61 .671 e641 e656 -924 e9G3 e915 le045 1.027 1.034 e759 e718 a748 

e1?1 1.0 le291 1 e2F6 1 e291 1 e419 

.360 1.0 1.34P 1.334 ' 1 e 336 1 e416 

e599 1.3 le366 1 e351 1.354 1.439 

'1.002 1.C eOGO .ooo ; eOOO e 000 

:le246 le0 4;1e017 ! e997 1' e977 ,' e964 

0759 1.0 1.219 ~ 1.232 1.224 .gal I 
TABLE B-4. (Continued) 

e121 1.0 

e360 1.0 

0599 1.0 

a759 1.0 

1.002 1.0 

1.246 1.C 

1; 031 

0121 1.G 

0363 1.0 

e599 1.0 

0759 1.0 

1.302 1.0 

1.246 1.0 

,TESTIG, RUN 89/1 TEST109 RUN 11119 TEST109 RUN 108/1 TESTIG, RUN 109/0 

0 .ai .906 .865 .goo .422 .372 .350 .599 .571 .581 .a04 .777 .817 

0121 1.6 1.419 i .a31 1 e835 1 .a35 

a360 1.0 1.412 1.770 1.777 1.781 

0599 1.0 1.432 1 0629 1 0623 1.608 

.759 1.c 0384 1.141 1 e129 1.110 

1.002 1.0 .oco .000 . 000 .ooo 

1.246 1.0 e960 1.121 1.110 1 0091 

TEST109 RUN 113/O TEST10, RUN 1II/O TEST109 RUN 4719 TESTIO, RUN SO/O 

0 061 1.004 1.C48 1.096 1.365 1.355 1.403 0954 0952 e953 0913 0912 e913 

e121 1.0 1.651 1.680 .9a7 965 

e360 1.G 1.7S2 1.817 1.006 . 999 

.59F 1.0 1.64'3 1.65E 1.027 1.023 

0759 1.0 1.224 1.333 1.02: 1.023 

lob32 1.0 .GOO OUG .ooo .ooo 

1.246 1.0 1.191 1.296 1.005 1 .004 

TESTIb, fiJN 49/0 TESTlC, RUY 43/3 T€STIO, RUY 47/1 TEST109 RUN 51/9 

0 .el 0921 0920 SF21 ,932 0931 -931 0943 e942 0942 0962 -850 0850 

0968 

l.GO0 

1.323 

1.223 

eo30 

1.094 

TEST109 RUN 51/0 

0745 0739 0739 

0953 

loG50 

1.117 

1.109 

.ooo 

1.031 

1 eOC5 1 e006 

TESTlfj, RUN 52/0 TEST109 RUN 53/0 

.8e3 .798 .79a .8ai .377 .a77 

-961 0983 

1.121 1.126 

1.112 1.117 

e 030 . 000 

1 e032 1.038 

1 .OS3 1.064 

1 0036 

TEST109 RUN 54/0 

1.013 

1.134 

1.123 

. 000 

1.044 

.945 .942 .942 

1 078 
TABLE B-4. (Continued) 

3 .cl 

e121 1eG 

0563 1.C 

-599 1.0 

*759 1.0 

TESTIi,, HUN 55/9 TtSTlOs RUY 5810 TESTI0, QUN 57/0 

e723 0707 -706 e672 et59 e660 e783 e769 0774 

1.17R 1.173 1.171 

1.2~0 1.273 1.270 

1e32P 11.312 1 e308 

1.2t9 j I .25e 1 e254 

TEST10, RUN 56/0 

m931 0915 e922 

le176 

1 e269 

1.303 

1.269 

e030 

e938 

1.c02 1.6 eLL9 .ooc 

I !TFSTIi,, RUN 55/0 TEST169 RUN 59/6 TEST10, RUN 62/0~TESTlO, RUN 61/1 

;q *zi 1.~1~6 le973 1.Gb5 .551 .527 -514 .712 -663 .676' ea52 e825 .a29 

.I21 leu 1.197 1.317 ll.311 7 1.312 

.3bL 1.0 ; 1.274 1.37c i 1.361 1 e253 

,599 1.3 1.3~~ ,10367 ~ 1.373 1.365 

.759 lac, 11.C48 ' 1.297 ' 1 e 220 

,000 . 000 

' 1.908 e 984 

1.092 1.0 .LGO 2% 

~__- 1.246 1.3 l.LU3 ,--__-. -- ___. 

' Tk5T1 kbh 6IjIC.j TiSTIL, Rbh 59/0'TESTlO, RUN t3/P' TESTlG, RUN 63/0 

'J e61 l.bC4 -979 .C2S11.14~ 1.128 1.134 ,455 e161 -419 e67? e636 -637 

.1:1 1.: 1.ZLC '1.313 1.450 1.455 

.-!6LJ 1.0 ,1.34" 1.351 ' 1.446 1.445 

, 0594 1.0 '1,356 1.359 1,465 , 1 e454 

.755 1.6 1.21: 1.216 ,947 e 969 

:l.b32 1.0 .G3@ e ~uG eo00 eOG0 

1 .i4b 1 .;__L.Livs ~_~________ 1 .OLY ,927 e925 

TESTIC, RciY tL/0 TCSTIO, RbY O5/0 TESTlil, RUN 6CIO TEST10, RbI\; 46/9 

'C .ti, .CI~ .7to ,763 .952 .FI~ .920 1.156 1.114 1.125 .2~3 e272 .23a 

,121 1,s 1.455 1.456 1 .168 ' 1 .PO4 

.36C 1.G 1.L41 1 ,441 1.469 le793 

,593 1.0 1.44F 11.443 1 ,445 1 e601 

;1.c02 1.c I .oca ' .OCO .ooo . e000 

,L1 ai66 1 i e'j3.l I .Q31 , 0937 e 969 

, a759 1.C , e97F 1 .Ft7 .996 0955 

000 
X/D R/R 

I) e31 1.303 1.246 1.283 1.388 1.326 1.368 

0121 1.0 

e36b le0 

e599 1.0 

e759 1.G 

1.002 1.C 

1.246 1.0 

TABLE B-4. (Continued) 

(A) CONCLUDED. 

I =90 =270 1 =9L =270 0=ir =90 =270 , 0=0 =90 =270 , 8=0 

1 edC.4 1.811 

1.7b9 

1.561 1 .5t3 

1 eo17 1.054 

.GOC 

I .a24 1 . a54 

1 .so4 1.820 

1 .5ai 1.65@ 

1 e075 1.183 

1 

.ooo 

e045 

1 

1.130 

,000 ' 
TABLE B-4. (Continued) 

X/D H/R 

0 .a1 

e109 1.0 

0196 1.0 

m271 1.0 

0385 1.0 

8=0 =90 =270 

TEST139 RUN 27/9 

0947 .945 .945 

1.013 

1.033 

1.050 

11.049 

TEST10, RUN 27/0 

.e86 .865 0886 

.9Y4 

1.020 

1.042 

1.042 

1 e031 

TEST109 RUN 28/0 TEST109 RUN 29/0 

a894 ,893 a894 a907 m906 m906 

0995 1 .ooo 

1.021 1.024 

1.042 1 .045 

' 1 a032 1 SO34 

1 a042 1 1.044 

1 

.1OY 1.0 11.005 

-190 1.0 ,1.027 

e271 1.0 11.046 

03.55 1.0 'lac46 

1 346 

1.310 I 

-466 1.0 

e547 1.0 

1.342 

1 e307 

0 e 81 

e109 1.0 

e130 1.C 

0271 1.0 

~ e385 1.G 

: -466 1.0 

.547 1.0 I 

I 

0 e81 

I e109 1.6 

' .134 1.0 

0271 1.0 

.355 1.0 

1 e036 

1.02s 

TESTlU9 RUN 2411 

*DO8 a600 -812 

1.399 

1.159 

1.201 

1.1Y2 

1 0166 

1.140 

TESTlCI, RUN 2010 

0717 .705 0717 

1.367 

1.403 

1 a414 

1.374 

1.346 

1.310 

1 e079 ,l 087 I 1.091 

1.137 1 e152 ' 1.154 

1.186 1.199 i 1.201 

1.lbO 1 0190 ' 1 a191 

1.15C '1.162 

1.124 1.135 i 1.137 

'1.164 I 

I I 1 

TEST16, RUN 

.8b8 .833 

1.099 

1.152 

l.lY4 

1.184 

1,158 

1,133 

23/g,TEST10, I RUY 19/91TEST109 RUN 19/01 

08891 0677 0664 0671 e596 a605 

' 1.392 

1.439 1.418 

1.448 ~ 1.425 

1.406 1.385 

1.376 1.357 

, 1 0336 ,10319 

1 

TEST109 RUN 15/91 

e496 a472 e489; 

1. 594 

1 s622 

1 0601 

1.533 

1 0482 

1 392 1 
TABLE B-4. (Concluded) 

.271 1.0 

0365 1.0 

0466 1.0 

i 0547 1.0 

0 081 

0105 1.0 

019.0 1.0 

0271 1.0 

0385 1.0 

0466 1.0 

0547 1.0 

0 081 

a105 1.0 

o1FG 1.0 

0271 1.0 

0385 1.0 

0466 1.0 

0547 1.0 P 

en 

en 

'1.796 1 .ec5 1.808 1.759 

1.563 1 e572 1.565 1,551 

1.339 1.354 1 e321 1.379 

os70 .9b3 e983 . 1.026 

TESTIu, RbN 31/8 TEST101 RbN 34/0 TtSTlOc RUN 33/1 TESTlG9 RUN 3.1/1 

0315 0260 0264 -756 e697 0725 1.031 0949 1.011'1.326 1.241 1.313 

3.104 3.262 3 238 3.109 

2.751 2.691 2 670 2.683 

2.451 , 2.346 ~ 2.314 2.306 

1.239 i 1.294 1 e317 1 0328 

0930 e932 .936 942 

0931 a952 1.013 1.042 

TEST109 RbN 32/1 

1.4G7 1.322 1.398 

3.316 

2.706 

2.323 

1.324 

1.040 

0942 
TAP PC/P 

rEST 1 

tUN 356/0 

~3pG1 

C7 26.45 

rEST 1 

?UN 359/0 

\i3pG1 

$7 27.40 

rEST 1 

2UN 350/0 

\3,G1 

IAP PC/P TAP PC/P 

rEST 1 TEST 1 

RUN 35810 RUN 321/0 

U3,GI N39G1 

L7 27.21 47 27.14' 

TEST 1 TEST 1 

TABLE B-5. NOZZLE WALL PRESSURES FOR CLASSIC GEOMETRY 

RUN 34910 

N3pG1 

47 26.69 

TEST 1 

TAP PC/P 

TEST 1 

RUN 32310 

N3(G1 

47 26.15 

TEST 1 

RUN 352/0 

N3pG1 

47 27.52 

TEST 1 

RUN 32910 

N3pG1 

RUN 31710 

N3pG11 

47 26.77/ 

TEST 1 I 

47 27.30147 27.17 

TEST 1 

N3pG1 

47 26.25 

TEST 1 

RUN 313/0 

tV39G1 

47 27.14 

TEST 1 

RUN 341/0 

N3pG1 

47 27.02 

TEST 1 

RUN 381/0 

N39G1 

47 27.54 

N39G1 

47 26.38 

TEST 1 

RUhi 344/C 

hi3pG1 

47 27.45 

TEST 1 

RUN 379/E 

N3pG1 

47 27.05 

TEST 1 

RUN 311/( 

N3,Gl 

47 27.4( 

TAP PC/P 

lEST 1 

3UN 35710 

43pG1 

C7 26.92 

rEST 1 

?UN 320/0 

V3pG1 

L7 27.40 

TEST 1 

RUN 361/0 

N3,Gl 

47 27.20 

TEST 1 

RUN 315/0 

N3pGl 

47 26.18 

TEST 1 . 

RUN 367/0 

N3pG1 

47 27.40 

TEST 1 

RUN 337/0 

N3pG1 

47 26.92 

TEST 1 

RUN 377/2 

N3,Gl 

47 27.50 

TAP PC/P 

TEST 1 

RUN 35410 

N3tG1 

47 26.82 

TEST 1 

RUN 36310 

N3pG1 

47 26.38 

TEST 1 

RUN 328/0 

Fu3pG1 

47 27.36 

TEST 1 

RUN 36510 

N39G1 

47 26.55 

TEST 1 

RUN 312/0 

h3'(G1 

47 27.17 

TEST 1 

HUN 309/0 

N3,GI 

47 26.91 

TEST 1 

RUK 336/0 

rU39G1 

47 27.54 

TAP PC/P 

rEST 1 

IUN 322/0 

U3pG1 

L7 26e75 

TEST 1 

RUN 316/0 

Y3jG1 

47 26.26 

TEST 1 

RUN 31810 

N39G1 

47 27.20 

TEST 1 

RUN 346/0 

N3pG1 

47 26.64 

TEST 1 

RUN 376/0 

N3pG1 

47 26.38 

TEST 1 

RUN 34210 

N3pGI 

47 27.14 

TEST 1 

RUN 155/0 

N4pG1 

47 94.34 

TAP PC/P 

rEST 1 

PUN 353/0 

U39Gl 

(t7 27.30 

TEST 1 

RUN 362/0 

N3pGI 

47 26.91 

TEST 1 

RUN 351/0 

N3pG1 

47 27.70 

TEST 1 

RUN 314/0 

N39G1 

47 26.70 

TEST 1 

RUN 34010 

N3pG1 

47 26.51 

TEST 1 

RUN 380/0 

47 . 27.17 

TEST 1 

RUN 154/0 

N4pG1 

47 93.46 

N39G1 

TEST 1 'TEST 1 

RUN 308/1,RUN 370/0 

N39G11N39G1 

47 26.55,47 26.89 

TEST i !TEST 1 

RUN 310/0'RUhr 34310 

N3pG1 N3,GI 

47 27.43,47 27.42, 

I TEST 1 ITEST 1 I 

RUN 195/01RUN 194/0, 

N4pGI ~N4pGI 

47 92.59147 93.46: 
TABLE B-5. (Continued) 

TAP PCIP r~~~ PCIP TAP PCIP TAP PCIP ,TAP PCIP TAP PCIP TAP Pcip !TAP pcipTEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUN 11510 RUN 19310 RUN 15610 RUN 19610 RUN 11610 RUN 15310 RUN 15210 RUN 11710 

N49GI N4iGI N4,GI N49GI N49G1 N49GI N49G1 N49G1 

47 51.74 47 92.45 47 92.31 47 92.86 47 92.02 47 92.74 47 93.17 47 93.60 

TEST 1 TEST 1 TEST 1 TEST 1 i TEST 1 TEST 1 TEST 1 TEST 1 

RUN 19710 RUN 15710 RUN 19210 RUN 19810'RUN 15110 RUN 11610 RUN 19110 RUN 15810 

N4vGI N49GI N49GI N4,GI N49G1 N4vG1 N4VG1 N4,GI 

47 93.17 47 93.75 47 93.60 47 93.90 47 94.94 47 94.94 47 94.94 47 95.39 

TEST 1 

RUN 15010 

'N 4 9 G1 

47 96.46 

TEST 1 

RUN 12410 

N4vGI 

47 90.91 

TEST 1 

RUN 14710 

N4(G1 

47 93.90 

TEST 1 

RUN iauo 

"tpG1 

47 94.79 

TEST 1 

RUN 12510 

N49G1 

47 89.29 

TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUN 19010 RUN 1591C RUN 11910 RUN 19910 RUN 14510 RUN 16410 RUN 20410 

N4,GI~N4tG1 N4vGl N49G1 N4pG1 N4pGl N49GI 

47 95.69,47 97.09 47 96.15 47 96.15 47 93.31 47 94.34 47 94.34 

TEST 1 TEST 1 

N4,Gl hi4,Gl 

RUN 18510 RUN 12310 

47 54.04 47 91.05 

TEST 1 

RUN 12210 

N 4 ~i 

47 93.02 

TEST 1 

RUN 12010 

N4,Gl 

47 95.24 

TEST 1 

RUN 20610 

N4VG1 

47 92.74 

TEST 1 

RUN 20210 

47 93.31 

TEST 1 

RUN 14910 

N4,GI 

N49G1 

47 97.09 

TEST 1 

RUN 16610 

1u49G1 

47 91.32 

TEST 1 TEST 1 TEST 1 

RUN 20310 RUN 16310 

Fc4,Gl N4pGI 

-- 47 93.02 47 92.59 

TEST 1 

RUN 18710 

h49GI 

47 93.46 

TEST 1 

RUN 20010 

N4 v G1 

47 95.24 

TEST 1 

RUN 12610 

N4 pG1 

47 91.19 

TEST 1 

RUN 16110 

N4pG1 

47 94.64 

TEST 1 

RUN 16010 

N49G1 

47 95.15 

TEST 1 

RUN 20710 

N4VG1 

47 92.59 

RUN 14610 

N49G1 

47 92.59 

TEST 1 

RUN 20110 

47 94.19 

TEST 1 

RUN 18910 

N4,Gl 

N49GI 

47 96.000 

TEST 1 

RUN 16710 

N4tGI 

47 .92.24 

TEST 1 

RUN 18610 

N49GI 

47 92.59 

TEST 1 

RUN 14810 

N49GI 

47 95.24 

TEST 1 

RUEl 20510 

N49G1 

47 92.59 

TEST 1 

RUN 127/0 

N49GI 

47 92.59 

TEST 1 

RUN 16210 

N4 9 GI 

47 93.60 

TEST 1 

RUN 12110 

N49G1 

47 95.39 

TEST 1 

RUk 16510 

N49G1 

47 90.91 

TEST 1 

RUN 20810 

N4tGI 

47 94.04 
TABLE B-5. (Continued) 

TAP PC/P 

TEST 1 

RUN 210/0 

N4VC1, 

47 94.94 

TEST 1 

RUN 130fO 

N49G1 

47 96.46,47 

TAP PC/p 

TEST 1 

RUN 133/0 

N4pG1 

47 90.77 

TEST 1 

RUN 709/0 

N5pG1 

30.83 

TAP PC/P 

TEST 1 

RUN 169/0 

N4,GI 

47 96.15 

TEST 1 

RUN 213fO 

Nk(G1 

TAP PCfP TAP PCfP 

TEST 1 TEST 1 

RUN 16810 RUN 12~0 

NGtGI N4,Gl 

47 94.19 47 94.64 

TEST 1 TEST 1 

RUN 211f0 RUN 132fO 

N4,GI N4,Gl 

TAP PC/P 

TEST 1 

RUN 134fO 

N49G1 

47 91.88 

TEST 1 

RUN 214/0 

N4rG1 

TAP PC/P TAP PCfP 

TEST 1 TEST 1 

RUN 20910 RUN 12910 

N4gG1 N4rGI 

47 95.24 47 96.15 

TEST 1 TEST 1 

RUN 212f2 RUIv 131fO 

N4,Gl N4qG1 - 47 92 59147 92.74)47 92.171,47 93.60 47 94.04 47 95.39 

RUFI 707fO 

1% 5 t GI 

,47 59.64 

RUN 713f3 RUh 7141~ RUN 706/0 RUN 711fO RUN 705fO RUN- 542/0 RUN 541/0 

N 5 t GI N 5 t GI N 5 9 GI 'N 5 9 GI N 5 9 GI N !A, C2 N 1A, C2 

47 62.83 47 65.72 47 66.15147 66.30 47 66.90 47 52.08 47 48.6; 

TEST 1 TEST 1 TEST 1 

RUN 519fO RUN 540fO RUN 550fil 

N IA, GZ N IA, G2 N ?A, G2 

47 49.71 47 48.70 47 47.47 

TEST 1 TEST 1 TEST 1 

RUN 535fG RUh 520fO RUN 517fO 

k IA, G2 N 1AV G2 N 1P, G2 

TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUN 51df0 RUN 53910 RUN 530/0 RUN 533/0 RUN 534/G 

N ?A, G2 N IA, G2 N IAp G2 N 1AV G2 N lA, C2 

47 50.68 47 48.70 47 48.31 47 48.74 47 48.58 

TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUN 54910 RUN 536/0 RUN 537/0 RUN 532/0 RUN 531/0 

N 1Av G2 N IAc G2 N 1Ac G2 Ec 1Ap G2 N 1Ag G2 

TEST 1 

RUN 516fO 

N IA, G2 

,47 50.93 

TEST 1 TEST 1 ITEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUN 521fG RUN 530fO HUN 54810 RUN 529/0iRUN 52810 RUN 523/1 RUN 524/0 

N IA, G2 N IA, G2 N IAp G2 IN 1Ap G2 ;N IA, G2 N 1Ap C2 N 1Aq G2 

47 49.97'47 48.27 47 47.58 47 48.35147 48.66,,47 49.46,47 47.85, 
TABLE B-5. (Continued) 

TAP PC/P 'TAP PC/P 'TAP PC/P TAP PC/P TAP PC/P 'TAP PC/P 'TAP PC/P 

TEST 2 

RUN 237/0 

N IC, G3 

2 6.80 

3 25.88 

4 72.05 

TEST 1 TEST 1 TEST 1 TEST 1 'TEST I 

RUN 522/0 RUN 515/0 RUN 546/0 FtUN 547/U RUN 525/0 

k IA, G2 N IA, G2 N 1Ap G2 tu 1A, G2 'N IA, G2 

47 49075,47 5Oo8G 47 48043 47 49o3G 47 48.90 

TEST 2 

RUN 238/0 

N IC? 63 

2 6094 

3 27020 

4 74.35 

TEST 2 TEST 2 

TEST 2 

RUN 161/0 

N ZA, G3 

2 5026 

3 12.23 

4 23058 

TEST 2 

RUN 3/0 

N 18, G4 

2 4.92 

3 20021 

4 59.10 

TEST 2 

RUN 261/C 

N 2Ap G3 

2 5.17 

3 12069 

L 24.35 

TEST 2 

RUh 412 

Tu le, G4 

2 5.31 

3 23089 

4 62.66 

TEST 2 

RUN 3310 

N IC, 63 

2 7.24 

3 28.05 

4 77.52 

TEST 6 

RUk 8 

N ID, G3 

2 5.63 

3 27.46 

4 81.30 

TEST 6 

RUN 11 

k 269 G3 

2 

3 12e5b 

4 25.64 

TEST 6 

RUN 24 

N ID, G4 

2 5.71 

3 26.53 

4 80.65 

TEST 2 TEST 2 

RUN 35/0 RUN 3410 

Tu lC, 63 N IC? G3 

2 7.32 2 7055 

3 28027 3 28.78 

4 75.70 

TEST 6 

RUN 21 

N ID, G3 

2 5018 

3 27.086 

4 7e.12 

TEST 2 

RUh 2710 

k 16, G4 

2 5025 

3 24.55 

4 64.60 

TEST 6 

RUN 37 

k ID, G4 

2 4049 

3 20075 

4 62089 

4 76.69 

TEST 6 

RUN 5 

N IE, 63 

2 5.46 

3 25.97 

4 71.94 

TEST 2 

RUN 2810 

2 5.17 

3 22.41 

4 62011 

N IR, G4 

TEST 6 

RUN 43 

N ID, G4 

2 5.69 

3 23.81 

L 

TEST 1 TEST 1 

RUN 526/0 RUN 52710 

N 1AV G2 N 1Ap G2 

47 48.74, 47 49014 

TEST 2 

RUN 13610 

N 1Cp 63 

2 6.99 

3 28.13 

4 73056 

TEST 6 

RUN 18 

N IEp 63 

2 5.91 

3 26074 

4 70042 

TEST 2 

RUN 29/0 

N 18, 64 

2 5036 

3 24060 

4 60.31 

TEST 6 

RUN 56 

N ID, 64 

2 5.73 

3 26.68 

4 74.07 

TEST 2 

RUN 137/0 

N 1C, 63 

2 7.12 

3 27029 

4 77.52 

TEST 6 

RUN 15 

N 1Ep GZ 

2 5.77 

3 26.95 

4 79037 

TEST 2 

RUN 1/1 

N 1R, 64 

2 4089 

3 22082 

4 57.74 

TEST 6 

RUB 27 

N IE, G4 

2 6007 

3 28.01 

4 72066 

TAP PC/P 

TEST 2 

RUN 138/0 

2 7.25 

3 28023 

4 76090 

N IC, 63 

TEST 2 

RUN 7210 

N ZAP 63 

2 5.20 

3 11.98 

4 23.75 

TEST 2 

RUN 2/0 

t 5.10 

3 21023 

4 58.00 

N IBp 64 

TEST 6 

RUN 34 

N IE, C4 

2 5.51 

3 24.51 

4 66067 
TABLE B-5. (Concluded) 

TAP PC/P 

TEST 6 

RUN 62 

N lE, G4 

2 5.87 

3 25.13 

4 65.36 

TEST 6 

RUN 40 

N 2R9 G4 

2 

3 13.87 

4 

TAP PC/P 

TEST 6 

RUIv 50 

tJ IE, C4 

2 5.85 

3 25.97 

4 

TEST 6 

RUN 47 

bi 2Bt G4 

2 

3 11.55 

4 

TAP PC/P 

TEST 2 

RUN 7010 

N 2Ap G4 

2 5.36 

3 11.44 

4 19.12 

TEST 6 

RUN 53 

N 28, G4 

2 

3 12.80 

4 25.45 

TAP PC/P 

TEST 2 

RUN 71/0 

N ZA, G4 

2 

3 11.39 

4 23.67 

TAP PC/P 

TEST 2 

RUN 62/2 

N 2Ac 64 

2 5.30 

3 11.41 

4 

TAP PC/P 

TEST 2 

RUN 163/0 

2 5.24 

3 11.55 

4 21.22 

N 2A, G4 

TAP PC/P 

TEST 6 

RUN 31 

N 28, 64 

2 

3 13.2E 

4 

TAP PC/P 

TEST 6 

RUN 66 

N 269 64 

2 

3 12.97 

4 24.27 
TAP PC/P 

TEST 3 

RUN 215/0 

h31 G1 

47 39.85 

48 36.62 

TEST 3 

RUN 208/c 

N31 9 G1 

47 42.47 

48 36.80 

TEST 3 

RUN 195/0 

h31 , ti1 

47 39.96 

43 38.01 

TEST 3 

RUN 200/0 

iu31 p GI 

47 42.10 

43 36.71 

TEST 3 

RUh 13C/O 

N32 , b1 

47 30.02 

43 30.79 

TEST 3 

RUh 119/0 

N32 GI 

47 29.05 

46 29.80 

TABLE B-6. NOZZLE WALL PRESSURES FOR ORBITER GEOMETRY 

TAP F'C/P TAP PC/P [TAP PC/P TAP PC/P TAP PC/P 'TAP PCIP iTAP PC/P 

TEST 3 TEST 3 TEST 3 TEST 3 TEST 3 ,TEST 3 'TEST 7 

RUN i10/0 RUN 209/0 RUN 20410 RUN 216/0 RUN 223/0'RUN 214/(i RUN 21110 

h31 9 GI N31 GI N31 9 GI h31 9 GI N31 , GI N31 GI N31 GI 

47 41.00 47 42.41 47 42.81 47 24.61 47 42.43 47 42.00 47 41.80 

48 36.47 48 36.82 48 37.12 48 36.52,4~ 36.67'48 36.60 48 36.46 

TEST 3 TEST 3 TEST 3 TEST 3 TEST 3 TEST 3 TEST 3 

RUN 105/0 RUN 21710 RUh 22410 RUN 213/1'RUN 212/0 RUN 222/0 RUN 221/0 

1431 9 GI N31 9 GI N31 1 GI N31 9 GI N31 G1 N31 9 GI N31 GI 

47 43.07 47 32-22 47 43.84 47 42.10 47 41.7b 47 42.37 47 43.07 

46 37.0514~ 36.12 LE 36.81,43 36.68 &E 35.47 48 36.74 48 37.09 

I 

TEST 3 TEST 3 .TEST 3 

RUN 194/3 HUN 207/t RUN 19010 

N31 , GI i~31 , G1 'h31 GI 

48 55.05 48 36.77:4f? 36.00 

TEST 3 TEST 3 iTEST Z 

Huh L03/(i RUN 2OZ/ir~RUN 121/Ci 

47 54-82 47 45.26 47 42.02 

Pi31 , GI N?l , GI 

47 42.76 47 42.130 

43 37.05 43 36.73 

TEST 3 TEST 3 

RLN 137/oi RUN 1311~1 

N32 , GI 

47 30.25 

48 :1*2e, 

TEST 3 

RUN 135/0 

Fi32 , GI 

47 29.92 

46 50.87 

N32 GI 

47 30.26 

LB 31.26 

TEST 3 

RUh 120/l 

h32 9 GI 

47 30.03 

4E 30.94 

h32 9 G1 

47 28.9G 

4e 29-58 

TEST 3 

RUN 111/0 

h32 GI 

47 ZE.82 

4E 29.04 

TEST 3 

RUh 132/0 

h32 , 61 

47 30.20 

4E 31.16 

TEST 3 TEST 3 TEST 3 TEST 5 

RUN 195/0 RUN 196/0 RUN 197/0 RUN 2C110 

h31 G1 lu3I G1 N31 GI 

47 42.03 

48 36.3 

TEST 3 

RUN 114/0 

N32 G1 

47 28.56 

48 29.52 

TEST 3 

RUN 124/0 

47 21.86 

48 26.01 

TEST 3 

RUN 138/0 

ti32 GI 

N32 , GI 

47 30.31 

45 31.35 

47 41.68 47 41.99 

46 

~- 36.25 48 36.30 

TEST 3 

RUN 115/0 

N32 9 GI 

47 29.23 

4s 30.07 

TEST 3 

RUN 122/0 

Fi32 GI 

47 28.88 

4E 29.57 

TEST 3 

RUN 110/1 

N32 , G1 

47 20.47 

4e 29.43 

TEST 3 

RUN 120/(, 

k32 G1 

47 29.02 

48 29.73 

TEST 3 

RUN 11210 

N32 9 GI 

47 28.95 

48 29.54 

TEST 3 

RUN 109/2 

N32 , G1 

47 28.72 

48 29.79 

N31 , G1 

47 42.32 

&a 36.72 

TEST 7 

RUN 1?6/0 

h32 , G1 

47 29.96 

48 30.89 

TEST 3 

RUN 116/0 

N32 9 GI 

47 29.28 

48 30.14 

TEST 3 

RUh 12310 

h32 9 G1 

47 2P.91 

4R 29.64 
TABLE B-6. (Continued) 

TEST 3 

RUN 85/0 

k33 9 G1 

47 75.23 

48 75.57 

TAP PC1P TAP PC/P 

TEST 3 T€ST 3 

RUN 11310 RUh 117/0 

29.52 48 30.0Y 

TEST 3 !TEST 3 

RUN 149/01RUh 1461U 

~32 9 GI jh32 G1 

47 29.50'47 28.92 

I 

1 

48 31.0Y 

TAP PC/P 

TEST 3 

RUN lla/o 

N32 GI 

47 29-89 

4P. 29.82 

TEST 3 

RUN 145/1 

N32 9 GI 

47 29.14 

TEST 3 TEST 3 'TEST 3 

RUN 143/0 RUh 67/3'RUtu 56/1; 

h32 GI ,N?3 9 61 1N33 GI 

47 30.28,47 18.27147 15.96 

TEST 3 

47 74-14/47 74.96,47 75.0i 

48 74.59i48 75e39,4P 75.34 

I 

TEST 3 'TEST 3 /TEST 3 

RUN 72/0 

h33 , G1 

47 73.10 

49 73.72 

TEST 3 

RUN 5910 

N33 , G1 

47 72-44 

48 72.69 

RUN 81/0 

N33 , G1 

47 74.12 

4b 74.47 

TEST 3 

RUN 74/1 

N33 , GI 

47 73.56 

46 73-89 

RUN 7d/( 

47 74.4i 

48 74.7t 

TEST 3 

RUN 73/( 

h33 , G1 

47 73.2' 

48 73.6; 

N33 GI 

-~ 

TAP PC1P 

IEST 3 

7UN 134/0 

432 , G1 

r7 30.03 

tE 30-93 

TEST 3 

IUN 144/1 

~32 9 GI 

47 29-16 

48 29.75 

TEST 3 

FtUk 62/0 

433 9 GI 

47 72.89 

49 72-86 

TEST 3 

RUN 66/0 

N33 , 61 

47 24.25 

4E 25-47 

TEST 3 

RUN 84/0 

1133 , GI 

47 75.00 

48 75.45 

TEST 3 

HUN ao1c 

N33 9 GI 

47 74.1c 

48 74.4: 

IAP PC1P 

lEST 3 

IUN 129/0 

132 9 G1 

C7 29.96 

C3 30-77 

TEST 3 

?UN 14710 

U32 , G1 

47 29.33 

48 29.93 

TEST 3 

RUN 6110 

N33 9 G1 

47 71.96 

48 72-15 

TEST 3 

RUN 5710 

N33 GI 

47 33.75 

43 30.3: -___ 

TEST 3 

RUN e7/0 

N33 9 GI 

47 75.11 

48 75.37 

TEST 3 

RUN 79/C 

N33 9 GI 

47 74.36 

48 74.71 

'AP PC/P 

'EST 3 

IUN 139/1 

432 , G1 

h7 30.28 

b8 31-31 

rEST 3 

IUN 142/0 

432 , til 

e7 29.77 

t8 30.62 

rEST 3 

2UN 7b/J 

TAP PC/P ITAP PC/P 

TEST 3 'TEST 3 ; 

RUN 141/0'RUN 140/0/ 

N32 , GI :N32 61 I 

47 29.91 47 30.281 

48 30eR3,4R 31.311 

TEST 3 ITEST 3 

HUN 'IIIOIRUN 7710' 

73-85 

TEST 3 

PUN 60/Q 

47 72.30 

V33 G1 

48 72.53 

TEST 3 

RUF; 6510 

N33 9 GI 

47 34.65 

48 68.19 

TEST 3 

RUN 8610 

47 75.24 

N33 9 61 

48 75.51 

48 73-43 

TEST 3 

RUN 6311 

N33 G1 

47 72.93 

48 74.70 

TEST 

3 ~ RUN 7510, 

N33 , GI 

47 74-00 

48 73-03 48 73.89, I I 

TEST 3 :TEST 3 

RUh 5810 RUN 6410 

N33 9 G1 "33 9 G1 

47 72.93 47 73.15 

48 71.21;48 73-20, 
TABLE B-6. (Continued) 

TAP PC/P TAP PC/P TAP PC/P ;TAP PC/P TAP PC/P 

TEST 1 TEST 1 

RUN 423/0 RUN 455/0 

47 30.23 47 30.77 

TEST 1 TEST 1 

RUN 459/0 RUN 452/0 

N34E9 GI N3489 GI 

N3489 lil N34P9 GI 

47 56.71 47 >7.14 

TEST 1 TEST 1 

RUN 430/0 RUN 416/0 

Fi3489 GI N348, GI 

47 45.87'47 52.27 

____i 

TEST 1 

RUN 414/0 

N348, GI 

47 4z.89 

TEST 1 

RUN 465/0 

Fv343, GI 

47 56-82 

TEST 1 

RUN 442/0 

Fv3459 G1 

47 50.76 

TEST 1 

RUN 607/b 

47 43.01 

h?3R9 G2 

TEST 1 

RUN 467/0 

N346, G1 

47 43.54 

TEST 1 

RUN 471/d 

l\t34B9 G1 

47 26.1G 

TtST 1 

RUFv 469/0 

N346, GI 

47 51.50 

TEST 1 

RUh 617/0 

N330, G2 

47 42.05 

TEST 1 TEST 1 TEST 1 

RUN 45410 RUN 42210 RUN 457/0 

47 41.90 47 s3.64 47 44.58 

TEST 1 TEST 1 TEST 1 

RUN 420/0 HUN 4td/O RUN 416/0 

~34a, i;i ~34a, GI ~348, GI 

N3489 21 .N34t39 GI N34B9 GI 

47 57.03 47 26.67 47 30.61 

TEST 1 TEST 1 TEST 1 

RUh 453/0 RUN 451/0 HUN 419/0 

N34E9 GI iu3489 61 N34B9 GI 

47 52.26.47 54.35 47 56.72 

TFST 1 

RUN 44b/O 

FJT4E9 GI 

47 44.05 

TEST 1 

RUN 440/0 

N3LB, G1 

47 29.31 

TEST 1 

RUhr, 41d/O 

N34t3, G1 

47 51.61 

TEST 1 

RUN 634/0 

47 40.79 

h33P9 G2 

TEST 1 

HUFi 433/0 

h34a9 Gl 

47 47.39 

TEST 1 

RUFI 40a/u 

h34U9 GI 

47 30.57 

TEST 1 

RUFv 411/0 

tv?4E9 G1 

47 57.14 

TEST 1 

RUN 618/0 

tv33Et GZ 

47 42.19 

TEST 1 

RUN 413/0 

h34B9 GI 

47 51.02 

TEST 1 

RUV 470/0 

N3489 GI 

47 41.41 

TEST 1 

RUN 443/0 

N34R9 G1 

47 56.87 

TEST 1 

RUN 622/0 

N3389 G2 

47 42.11 

TAP PCIP 'TAP PC/P TAP PC/P 

TEST 1 

RUN 42510 RUN 45310 RUN 421/0 

TEST 1 TEST 1 

N34B9 GI N34B9 GI N34Bi GI 

47 46.51 47 52.13 47 52.16 

TEST 1 

RUN 462/0 

N34B9 GI 

47 43.16 

TEST 1 

RUN 460/0 

N348, Lil 

47 56.71 

TEST 1 

RUN 445/0 

N34B9 GI 

47 52.17 

TEST 1 

RUh 409/0 

h3LB9 GI 

47 43.36 

TEST 1 

RUN 466/0 

47 56.93 

TEST 1 

RUN 621/0 

N3389 G2 

47 42.1Y 

N34B9 GI 

TEST 1 TEST 1 

RUN 417/0 RUN 449/0 

N34B9 GI N34B9 G1 

47 44.05 47 43.73 

TEST 1 TEST 1 

RUN 41S/O RUN 447/0 

N3489 GI N34B9 GI 

47 29.84 47 31.75 

TEST 1 

RUN 412/0 

N3489 GI 

47 56.50 

TEST 1 

RUN 441/0 

N3469 GI 

47 44.31 

TEST 1 

RUFv 61S/O 

N33B9 G2 

47 42.16 

TEST 1 

RUN 620/0 

47 42.16 

N3389 G2 

TEST 1 

RUN 4&4/0 

N34R, 61 

47 56.82 

TEST 1 

RUN 43&/1 

N340, GI 

47 46.12 

TEST 1 

RUN 616/0 

N33B9 G2 

47 42.16 

TEST 1 

RUN 63310 

N3389 G2 

47 40.76 
TABLE B-6. (Concluded) 

TAP PC/P 

TEST 1 

RUN 606/C 

N33R9 G2 

- 47 42.55 

TEST 1 

RUN 626/C 

TAP PC/P /TAP PC/P ITAP PC/P TAP PC/P TAP PC/P TAP PC/P 

TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RLih 61910 RUN 62310 RUN 63210 RUN 624/0 RUN 612/0 RUN 60910 

N33B7 G2 Ir33Bp G2 N33Bt G2 N33R9 G2 N338, G2 N3389 G2 

47 42.40 47 41.81 47 40.87 47 42.31 47 40.90 47 44.61 

TEST 1 TEST 1 TEST 1 TEST 1 TEST 1 

RUh 63010 RUN 629/0 RUN 6ll/ci RUh 62810 RUN 610/0 

TEST 1 

RUN 625/0 

N33B, G2 

TEST 1 

RUN 627/0 
L-' 

I 

RUN 63/2 

Llu 24AfG1 

22 25.90 

23 85.24 

24 138.06 

RN 248961 

32 27.59 

33 77.11 

34 130.48 

TABLE B-7. NOZZLE WALL PRESSURES FOR ET/SRB CLASS 

RUN 52/2 

LN 24AtGl 

22 27.06 

23 83.65 

24 137.49 

RN 24BpG1 

32 29.08 

33 78.41 

34 136.24 

*TAP PC/P "TAPPC/P-TAP PC/P I TAP PC/P -TAP PCIP /TAP PC/P 

I 

TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 

RUN 7212 RUN 6ll21RUN 50/2iRUN 65/2 RUN 49/2 RUN 73/4 RUN 4012 RUN 86/2 

LN 24A9G1 LN 24A9GliLN 24APG1 LN 24A9G1 LN 24ApG1 LN 24AgG1 LN 24AtG1 LN 24AtG1 

22 27.55 22 27.39 22 27.70 22 26.89 22 28.19 22 28.29 22 e00 22 28.50 

23 80.44 23 89.17 23 81.30 23 83.29 23 82.57 23 a2.14'23 e00 23 82.36 

24 129.59 24 132.40 24 129.53 24 132.03 24 132.43 24 130.07 24 e00 24 128.75 

RN 24BvG1 RN 2489Gl:RN 24B9G1 RN 24BPG1 RN 248961 RN 24BtG1 RN 248961 RN 24BtG1 

32 30.42 32 29.60 32 30.41 32 29.57 32 31.05 32 31.02 32 e00 32 31.07 

33 76.29 33 76.95 33 77.41 33 77.00 33 78.91 33 77.68 33 e00 33 77.48 

34 125.99 34 i24.50,34 126.23 34 123.83 34 131.33 34 129.00 34 a00 34 128.52 

TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 

RUN 6012 RUN 6412 RUN 51/2 RUN 7112 RUN 4812 RUN 74/2 RUN 41/2 RUN 85/2 

LN 24A9G1 LrU 24A9G1 LN 24AqG1 LN 24AVG1 LN 24A9Gl LN 24ApG1 LN 24AtG1 LN 24A9G1 

22 27.32/22 26.74122 27.74122 27.40 22 28.11 22 27.91,22 m00 22 28.30 

23 67.34 

24 135.56 

RN ZkB9G1 

32 28.86 

33 77.16 

34 126.29 

TEST 7 

,RUh 62/2 

LN 24AfG1 

22 26.08 

23 89.65 

24 139.39 

RN 2489G1 

32 27.39 

33 77.50 

34 130.89 

24 129.25 

RN 248961 

32 29.94 

33 75.39 

34 126.31 

TEST 7 

RUN 70/6 

LN 24AfG1 

22 26.78 

23 80.11 

24 130.32 

RN 24B9G1 

32 28.95 

33 75.06 

34 128.62 

24 133.39 

RN 24BVG1 

32 30.57' 

33 78.39 

34 133.19 

TEST 7 

RUN 4712 

LN 24A961 

22 27.-72 

23 84.45 

24 139.35 

RN 24BqC1 

32 30.23 

33 80.02 

34 140.96 

23 80.54 23 a00 23 81.66 

24 127.85 24 e00 24 127.27 

RN 248961 

32 30.31 

33 76.18 

34 127.06 

TEST 7 

RUN 7512 

LN 24'A,G1 

22 27.61 

23 80.95 

24 128.64 

RN 24BgG1 

32 29.85 

33 76.04 

34 128.40 

RN 24B9G1 RN 24R9G1 

32 e00 32 30.72 

33 .oo 33 76.84 

34 moo' 34 127.14 

TEST 7 

RUN 5914 

LN 24AtG1 

22 28.12 

23 81.39 

24 129.42 

RN 248961 

32 30.49 

33 77.45 

34 130.08 

TEST 7 

RUN 84/2 

LN 24AfGl 

22 28.05 

23 82.19 

24 127.77 

RN 248961 

32 30.35 

33 16.77 
CI 

43 

43 

TAP PC/P 

TEST 7 

RUFl 46/2 

LN 24AVG1 

22 a00 

23 a00 

24 a00 

RN 248961 

32 a00 

TABLE B-7. (Continued) 

TAP PC/P TAP PC/P TAP PC/P 

TEST 7 TEST 7 TEST 7 

RUN 7612 RUN 4313 RUN 79/3 

LN 24AVG1 LN 24AgG1 LN 24AVG1 

22 27.68 22 a00 22 28.43 

23 80.67 23 mOG 23 81.65 

24 128.90 24 a00 24 129.69 

RN 248961 RN 24BpG1 RN 24BgG1 

32 29.82 32 a00 32 30.62 

33 e00133 75.97 

34 a00 34 128.42 

33 a00 33 77.33 

34 a00 34 130.00 

RUN 55/3 RUN 67/2 RUN 68/2 GUN 54/L RUN 45/3 RUN 7713 RUN 44/2 RUN 78/2 

LN 24ApG1 LF( 24AtGl LN 24A9G1 LN 24ApG1 LN 24AVG1 LN 24A9G1 LN 24A9G1 LN 24AtG1 

22 27.33 22 26.86 22 27.11 22 27017'22 000 22 28.10 22' 000 22 28.62 

23 89.94123 01.75 23 79.37 23 31.92'23 a00 23 81.52 23' a00 23 82.27 

24 150.58 24 141.58 24 132.17124 139.40 24 a00 24 131.86 24 mOO'24 130.13 

32 29.63 32 28.54 32 29.29 32 29.37 32 a00 32 30.24 32 000 32 30.89 

33 64.37 33 77.49 33 75.44133 77.83 33 a00 33 77.21 33 a00 33 77.80 

34 137.30 34 133.27 34 129.93 34 137.40 34 a00 34 132.33 31 a00 34 130.44 

RN 24@,G1 Rh 24B9G1 RN 24B9G1'RN 24R9G1 RN 24BVG1 RN 24B9G1 RN 2489C1 RN 24RpG1 

TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 

RUN 16414 RUN 16312 RUN 16212 RUk 16113 RUN 114/2 RUN 12112 RUN 109/3 RUN 113/2 

LN 24A9GI LN 24A~G1 LN 24AVG1 LN 24A9G1 LN 23AVG1 LN 23AVG1 LN 23AVtl LN 23AtG1 

22 29.21 22 28.41 22 23.55 22 27.98 22 24.50 22 24.50 22 24.52122 24.15 

23 70.40 23 75.76 23 77.12 23 74091 23 31.74 23 31.68 23 32.34,23 31.95 

24 140.44 24 133.11 24 131.75 24 124.47 24 40.16 24 39.40 24 40.62 24 40.51 

RN 240,Gl RIU 24BvG1 RN 24R9G1 FiN 24E9G1 RN 238961 RN 238,Gl RN 23B~G1 RN 23B,G1 

32 30.77 32 30.66 32 30.97 32 30.31 32 22.37 32 23.03 32 23.39 32 22.32 

33 73.08 33 75.43 33 76.45 33 73.24 33 30.03 33 30.00 33 30.34 33 30.07 

34 126.08 34 127.68 34 128.51 34 122.70 34 40.74 34 39.73 34 40.01 34 41.27' 

TAP PC/P 

TEST 7 

RUk 5612 

22 27.23 

LN 24AVG1 

23 63.81 

24 143.18 

TAP PC/P TAP PC/P TAP PC/P 

TEST 7 TEST 7 TEST 7 

RUN 6612 RUN 5312 RUN 69/2 

22 26.44 22 27.14 22 26.83 

LN 24AVG1 LN 24A9G1 LN 24AqG1 

23 81.65 23 83.72 23 b0.82 

24 138.62 24 142.37 24 133.02 

RN 246961, RN 24B9G1 RN 24B9G1 

32 26.30 32 27.99 32 29.47 

133 78.09 33 76.17 33 79.13 

34 132.30 34 130.64 34 140.62 

RN 2489G1 

32 29.03 

33 75.63 

34 131.56 
TABLE B-7. (Continued) 

TEST 7 , TEST 7 

RUN 135/2 RUN 140/2 

LN 22AtCZ'LN 22ApG2 

22 3.67'22 3.68 

23 15.96 23 16.04 

24 42.42 24 41.96 

RN 228962 RN 22BpG2 

32 3.80 32 3.84 

33 16.97 33 16.94 

34 44.58 34 44.28 

- 

TAP PCIP 

I 

\TAP 'c. TAP PC/P 

I 

TAP PC/P ITAP PC/P ;TAP PC/P TAP PC/P TAP PC/P 

-- 

TEST 7 

RUN 147/2 

LN 22A9G2 

22 4.56 

23 16.09 

24 44.65 

RN ZZB9GZ 

32 4.55 

33 16.98 

34 45.33 

TEST 7 itST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 

RUN 111/2 RUN 110/2 RUN 115/2 RUN 120/2 RUN 122/3 RUN 116/2 RUN 119/2 RUN 117/2 

I 

LN 23AtG1 Lh 23AVG1 LN 23AVG1 LN 23ApG1 LN 23A9G1 LN 23ApG1 LN 23ApG1 LN 23ApG1 22 24.15 22 24.43 22 23.81 22 24.12 22 24.28 22 23.86 22 24.25 22 24.58 

24 39.17 24 39.47 24 40.30 24 39.34 24 39.31 24 40.33 24 39.34 24 40.12 

RN 238161 RN 23BVGl RN 23BtGl'RN 23BrG1 RN 238961 AN 23BpG1 RN 23BpG1 RN 23BtG1 

33 29.93 33 30.22 33 29.81 33 29.89 33 30.21 33 29.93 33 29.88 33 30.05 

34 39.82,34 137.25,34 40.77 34 39.77 34 39.73 34 41.12 34 39.79 34 40.80 4 

23 31.81 23 32.03 23 31.91 23 31.66 23 31.95 23 32.01 23 31.67 23 31.74 

32 22.65 32 23.06 32 21.89 32 22.56 32 22.97 32 21.88,32 22.65 32 22.34 

LN 22AtG2 

22 3.64 

23 16.34 

24 44.81 

RN 22B9G2 

32 3.85 

33 17.32 

34 47.11 

TEST 7 TEST 7 TEST 7 TEST 7 

RUN 118/3 RUN 123/2 RUN 172/2 RUh 171/2 

'LN 23AqG1 LF( 23ApG1 LN 23AfGI'LN 23AVG1 

22 24.45 22 24.47 22 24.75 22 24.51 

23 31.69'23 31.84 23 30.60 23 31.14 

24 39.29 24 39.33 24 40.76 24 39.79 

RN 2389G1 RFJ 23BVG1 RN 2389C1 RN 2369G1 

32 22.67 32 23.07,32 23.18 32 23.12 

33 29.91 33 30.09 33 29.88 33 29.87 

34 39.47 34 40.01 3L 40.02 

LN 22ApC2 

22 3.68 

23 15.95 

24 42.42 

RN 2289G2 

32 3.82 

33 17.03 

34 44.53 

TEST 7 

RUN 139/2 

LN 22AtG2 

22 3.69 

23 16.07 

24 42.14 

RN 22B9G2 

32 3.85 

33 17.00 

34 44.36 

TEST 7 

RUN 139/2 

LN 22A9G2 

22 3.63 

23 16.24 

24 44.19 

RN 22BpG2 

32 3.79 

33 17.13 

34 46.16 

TEST 7 TEST 7 TEST 7 (TEST ? 

RUN 17015 RUN 137/2 RUN 12812 RUN 138/3 

LN 23ApG1 LN ZZA9G2 LN 2ZApG2 LN 22A9G2 

22 24.53 22 3.68 22 3.63 22 3.69 

23 31.44 23 15.97 23 16.14 23 16.07 

24 39.38 24 42.63 24 43.53 24 42.23 

RN 22BpG2 

32 3.85 

33 17.04 

34 44.46 

TEST 7 

RUN 13112 

LN Z2A9G2 

22 3.62 

23 16.09 

24 43.98 

RN 228962 

32 3.78 

33 17.05 

34 45.93 
TABLE B-7. (Continued) 

TAP PC/P 

TEST 7 

RUN 134/3 

LN 22A9G2 

22 3.66 

23 15.95 

24 42.56 

RN 22B9G2 

32 3.81 

TAP PC/P TAP PC/P TAP PC/P TAP PC/P TAP PC/P TAP PC/P TAP PC/p 

TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 TEST 7 

RUN 14212 RUN 146/2 RUN 132/2 RUN 13312 RUN 14112 RUN 14512 RUN 15614 

LN 22A9G2 LN 2ZA9C2 LN 22AtG2 LN 22A9G2 LN 22AtG2 LN 22AtG2 LN 22ApG2 

22 3.68 22 4.55 22 3.63 22 3.66 22 3.69 22 4.54 22 3.66 

23 15.98 23 16.05 23 16.01 23 15.82 23 15.89 23 16.10 23 15.50 

24 41.78 24 44054 24 44.13 24 42.10 24 41.62 24 44.41 24 43.41 

RN 228962 RN 22B9G2 RN 228962 RN 22B9GZ RN 22BtG2 RN 22BtG2 RN 22BtG2 

32 3.83 32 4.54 32 3.76 32 3.80 32 3.84 32 4.52 32 3.80 

16.92 

44.04 

TEST 7 TEST 7 

154/2 

22A9G2 

3.69 

15.79 

41.36 

2269G2 

32 3.81 32 3.85 

33 16.84 33 16-82 

33 16.05 33 16.96 33 16.83 33 16.86 33 16.94 33 16.92 

34 45.22 34 46.01 34 44.27 34 43-84 34 45.07 34 45.29 

TEST 8 TEST 8 TEST 8 TEST 8 TEST 8 TEST 8 

RUN 14 RUN 31 RUN 20 RUN 33 RUN 21 RUN 7 

LN 21ApC5 LN 21AVG5 LN 21AtG5 LN 2lAsG5 LN 21AtG5 LN 21ApG5 

25 8.37 25 8.58 25 8.30 25 8.79 25 8.93 25 8.05 

26 13.57 26 1C.84 26 10.73 26 11.11 26 11.23 26 10.15 

27 13.04 27 13.32 27 13.44 27 13.65 27 13.78 27 13.04 

RN 218965 HN 2189G5 RN 218965 Rlu 218965 RN 21BtG5 RN 21FgG5 

22 8.22 22 7.76 22 7.82 22 8.54 22 7.26 22 7.67 

23 10.52 23 9.27 23 10.51 23 13.15 23 15.29 23 8.28 

34 43.89 34 43.52~24 13.48 

TEST 8 TEST 8 TEST 8 

RUN 24 RUN 6 RUh 25 

LN 21A965 Lh 21AtG5 LN 21AqG5 

25 6.60 25 8.18 25 8.03 

26 11.04 26 10.55 26 10.44 

27 13.60 27 12.90 27 13.08 

RN 21B9G5 RN 21BtG5 RN 21BpC5 

22 8.31 22 7.86 22 7.52 

23 11.36 23 14.73 23 10.86 

24 14.23.24 13.26 24 14.06 

24 14.02 24 13.82 24 15.08 24 13.71 24 12.87 

TEST 8 TEST 8 TEST a TEST 8 TEST 8 

RUB 8 RUN 15 RUN 27 RUN 17 RUN 28 

LN 21AvG5 LN 21AtG5 LN 21AvG5 LN 21AtG5 LN 21AVG5 

25 8.58 25 9.15 25 7.87 25 8.49 25 8.23 

26 10.60 26 11.78 26 9.83 26 10.98 26 10.49 

27 13.20 27 14.30 27 12.57 27 13.72 27 13.19 

RN 21BpG5 RN 216965 RN 218965 RN 2IBtGS RN 21BtG5 

22 8.29 22 7.57 22 7.66 22 8.14 22 7.99 

23 14.40 23 10.89 23 10.54 23 10.60 23 10.59 

24 13.97 24 13.87 24 13.94 24 14.15 24 14-35 
TABLE B-7. (Concluded) 

TAP PC/P 

TEST 8 

RUh 19 

LN 21AtG5 

25 8.46 

26 10.68 

27 13.24 

RN 21B9S5 

22 7.04 

23 14.84 

24 13.34 

TEST S 

RUh 30 

LN 2IA9G5 

25 0.67 

26 11.26 

27 13.93 

RN 21ApG5 

22 8.53 

23 11.14 

24 16.54 

TAP PC/P 

TEST 8 

RUN 5 

LN 21ApG5 

25 8.20 

26 10.53 

27 12.96 

RN 21BpG5 

22 7.16 

23 10.41 

24 12.89 

TEST 8 

RUN 26 

Lh 21A~G5 

25 9.55 

26 11.91 

27 14.87 

Rh 21BvG5 

22 8.28 

23 11.75 

24 14.51, 

TAP PC/P 

TEST 8 

RUN 10 

LN 21AqG5 

25 8.16 

26 10.52 

27 13.12 

RN 218965 

22' 7.91 

23 8.42 

24 13.84 

TEST 8 

RUN 32 

LN 21AtG5 

25 8.64 

26 10.90 

27 13.19 

RN 21BfG5 

22 7.82 

23. 9.85 

24 14.34 
TABLE B-8. NOZZLE WALL PRESSURES FOR SRB CLASS 

TAP PC/P TAP PC/P TAP PC/P 

TEST 10 TEST 10 TEST 10 

RUN 106/0 RUN 107/0 RUN 103/0 

Nll , G2 N11 9 GZ Nll 9 G2 

1 43.90! 1 42.90 1 42.60 

2 33.5i;I 2 32.60 2 32.20 

3 18.RC'! 3 18.30, 3 18.10 

TAP PC/P 

TEST 10 

RUN 104/0 

Nll 9 G2 

2 33.70 

3 18.90 

TEST 10 

[RUN 96/0 

,hll , G2 

~ 1 43.80 

2 33.10 

TAP PC/P TAP PC/P TAP pc/P 

TEST 10 TEST 10 TEST 10 

RUN 102/0 RUN 101/0 RUN 100/0 

N11 t G2 N11 9 G2 Nll 9 G2 

1 44.10 1 44.00 1 43.70 

2 33.50 2 33.501 2 33.30 

3 18.70, 3 18.701 3 18.50 

TAP PC/P 

1 46.00 

2 35.00 

3 27.50 

TEST 10 

RUN 105/0 

Nll 9 G2 

1 44.00 

2 33.50 

3 18.60 

1 46.101 1 47.601 1 44.70 1 46.00 

2 35.201 2 35.80 2 34.00 2 34.90 

3 27.901 3 27.70 3 26.60 3 27.40 

TEST 10 

RUN 97/0 

1 44.9'2 

h11 9 G2 

Z 34.00 

, 3 20.30 3 20.50: 3 19.001 3 18.70 3 21.30, 3 18.60; 3 21.10 3 22.10' I I 

TEST 10 TEST 10 TEST 10 'TEST 10 TEST 13 TEST 10 'TEST 10 'TEST 10 

RUh 8911 RIJh 108/1 RUN 1Oo/d RUh 110/0 HUN 111/0 RUN 5010 RUN 4910 RUN 4810 

Nll p G2 hll G2 N11 9 G? Fill G2 hll 9 G2 N12 9 G1 N12 9 GI NIZ t GI 

, 1 43.30 1 44.60, 1 45.60 1 44.40 1 43.90 1 46.80 1 46.56 1 46.20' 

! 2 33.00 2 33.60 2 34.:0 2 33.6G 2 33.40 2 35.30 2 35.20 2 35.00 

\ 3 19.90 3 19.80: 3 20.32 5 19.10 3 19.20 3 27.50 3 27.50 3 27.50 

TEST 10 'TEST 10 TEST 10 TEST 10 TEST 10 TEST 10 TEST 16 TEST 10 

RUh 4711 RUN 51/0 RUN 5216 KUk 53/G ,RUN 5410 RUN 58/0'RUN 5710 RUN 5610 

h12 , GI hlZ 9 G1 k12 9 G1 hl2 p GI h12 9 GI k12 9 GI N12 9 GI N12 9 GI 

1 46.00 1 46.90' 1 46e50 1 46.0G 1 46.00' 1 47.30 1 46.60 1 46.00 

2 35.00 2 35.40 2 35.10; 2 35.00 2 35.00 2 35.70 2 35.30 2 35.00 

, 3 27.50 3 27.60 3 27.40, 3 27.40 3 27.60 3 27.60, 3 27.50 3 27.50 

TEST 10 TEST 10 

,RUN 5510 RUlv 62/0 

h12 , GI N12 9 G1 

46.10 1 47.40 

2 35.10 2 35.70 

TEST 1U 

RUN 61/1 

1 46.50 

2 35.20 

3 27.50 

N12 9 G1 
TABLE B-8. (Concluded) 

'TAP pc/p TAP Fc/P TAP pc/p 'TAP pc/p TAP pc/p TAP pc/p TAP pc/p TAP pc/p 

TEST 10 TEST 10 ;TEST IO TEST IO TEST 10 TEST 10 TEST 10 TEST 10 

N12 , G1 NIZ 9 GI N12 9 GI N12 9 GI "I2 p GI N12 9 GI N12 9 GI Ft12 9 GI 

RUN 6GfO RUIr 4610 RUN 4510 RUN 44fO RUN 43fO RUN 27fO RUN 2810 RUN 2910 

1 46.20 1 47.70 1 46.40 1 46.00 1 46.30 1 46.70 1 46.40 1 45.50 

2 35.30 2 36.00 2 35.10 2 35.10 2 35.30 2 35.30 2 35.10 2 36.60 

3 28.00 3 27.80 3 27.50 3 27.70 3 28.00 3 27.40 3 27.40, 3 27.00 

I 

I. 

J 

TEST 10 TEST 10 

RUN 30fO RUN 26fO. 

N12 GI N12 , C1 

1 45.50 1 46.20 

2 34.60 2 34.90 

3 27.20 3 27.10 

TEST 10 

RUtv 22fO 

1 46.00 

N12 9 GI 

2 35.20 

3 27.80 

TEST IO 

RUN 14fO 

h12 9 GI 

1 46.20 

2 35.40 

3 28.00 

TEST 10 

RUN 18fO 

N12 , G1 

1 48.10 

2 35.80 

3 27.60 

TEST 10 

RUN 34fO 

N12 9 GI 

1 47.50 

2 36.10 

3 27.80 

TEST 10 

RUN 25fO 

N12 9 GI 

1 46.50 

2 35.20 

3 .27.40 

TEST 10 

RUN 1710 

N12 1 GI 

1 46.70 

2 35.20 

3 27.50 

TEST 10 

RUN 33f1 

N12 9 G1 

1 46.20 

2 35.20 

3 27.40 

, 

TEST 10 TEST 10 TEST 10 TEST 10 TEST 10 

RUlv 24f1 RUN 23fO RUN 19fO RUN 20fO RUN 21fO 

1412 G? hl2 9 GI N12 , GI N12 9 GI N12 , G1 

1 46.10 1 45.80 1 47.90 1 46.80 1 46.00 

2 35.00 2 35.00 2 35.60 2 35.20 2 35.00 

3 27.40 3 27.60 

TEST 10 

RUIr 16fO 

ru12 , 51 

1 46.10 

2 35.10 

3 27.60 

TEST 10 

RUN 31f1 

N12 9 GI 

1 45.9G 

2 35.10 

3 27.70 

TEST 10 

RUN 15fO 

N12 9 GI 

1 46.20 

2 35.40 

3 28.00 

TEST 10 

RUN 32f1 

1 45.90 

N12 , GI 

2 35.20 

3 27.80 

TEST iir TEST IO TEST io 

N12 RUN, 11,1IRUN GI N12 9 12fOiRUN GI N12 9 13fO GI 

1 44.80 1 46.70 1 46.10 

2 33.90 2 35.313 2 35.00 

3 26.30 3 27.40 3 27.40 
APPENDIX C 

NOZZLE CALI BRATION DATA 

The. nozzle calibration data (wind-off) available for each of the nozzles 

used during the wind-on runs of the seven selected tests are presented in this 

appendix. Air was the gas used for most of the calibrations; CF4 was used with 

three nozzles. The test setup is described in Section IV of text. Instrumentation consisted of schlieren photographs of the plumes, model chamber conditions, plenum (ambient) conditions, and nozzle wall pressures. Locations of 

those nozzle wall pressure taps used only during calibrations are given in 

Table C-1, and those nozzle taps used during both calibration and wind-on runs 

are given in Table 7 of text. 

Data are given in Tables C-2 through C-4, grouped according to body 

geometry types. (There were no valid nozzle calibration data for the nozzles 

used with the ET/SRB body class.) Within each table, data are grouped first 

by test number, then by gas and nozzle number. This grouping is the same as 

that used in Appendices A and B. However, there are several additions (air 

calibrations of nozzles which were used wind-on with nonair gases) and omissions (no calibrations with gases G3, G4, or G5; no calibration of nozzles N21, 

N22, N23, NZ4, or N3?). For each of the test/gas/nozzle groups, a subtitle is 

provided which includes nozzle design values of A/A, and 8 ; exact values of 

nozzle geometry are given in Table 3 of text. Beneath each subtitle the data are 

presented in run number sequence. 

n 

172 
TABLE C-1. NOZZLE PRESSURE INSTRUMENTATION LOCATIONS 

USED ONLY FOR CALIBRATION RUNS 

Upstream Tap Middle Tap Downstream Tap 

Nozzle 

A/ A, Tap $ Tap 9 Tap $ Tap 9 

No. (deg) X/L No. (deg) X/L A/A* No. (deg) X/L A/A* No. (deg) X/L 

31A 

B 

C 

32A 

B 

C 

33A 

B 

C 

34A 

B 

C 

I 

1A 44 335 0.265 1.58 48 30 0.594 3.96 46 150 0.945 7.39 

3 44 330 0.671 2.11 48 30 0.783 2.56 46 150 0.899 3.07 

4 44 330 0.721 3.53 48 30 0.837 4.66 46 150 0.944 5.84 

5 44 330 0.467 1.69 48 30 0.633 2.19 46 150 0.813 2.80 

- 

44 

46 

49 

44 

46 

49 

45 330 0.941 7.35 

45 330 0.897 3.07 

45 330 0.959 6.02 

45 330 0.810 2.79 

270 

30 

330 

270 

30 

330 

4.29 

3.82 

4.78 

2.90 

2.78 

2.75 

0.711 

0.707 

0.715 

0.712 

0.686 

0.687 

45 

45 

45 

46 

45 

46 

48 

0.883 

0.882 

0.807 

- 

5.08 

3.79 

6.99 

6.96 

2.98 

3.08 

3.07 

7--- 

6.97 

6.93 

3.02 

2.90 
Il! I1 II Ill I l11111~1111l1l11l111111 

Run/ 'amb P C T cRerun (psia) (psia) (OR) 

- 

pw 

Tap NO. 

44 48 45 46 47 

609 

630 

637 

642 

643 

596 

615 

638 

631 

632 

973 

997 

998 

~ 

63.44 

63.63 

63.50 

63.58 

63.66 

65.15 

65.18 

65.24 

65.14 

65.21 

63.60 

62.95 

63.02 

TABLE C-2. NOZZLE CALIBRATION DATA FOR CLASSIC GEOMETRY 

Test 1, G1, N3 (Air, A/A, = 3.5, 25 deg) 

26.55 

26.13 

26.77 

27.07 

27.36 

27.47 

2.610 

2.610 

2. 610 

2.610 

2.610 

2.610 

181.3 

408.1 

639.2 

923.9 

1267.6 

1467.1 

941 

9 84 

996 

987 

1023 

1043 

17.02 

16.71 

17.12 

17.54 

17.36 

17.41 

22.14 

21.66 

22.12 

24.11 

31.75 

32.53 

26.28 

26.34 

27.02 

26.89 

27.24 

27.29 

26.51 

26.32 

26.86 

26.98 

27.14 

27.30 

301/0 

302/ 0 

303/ 0 

304/ 0 

306/ 0 

307/ 0 

Test 1, G N (Air, A/A,= 6.5, 35 deg) 1' 4 

99.11 

95.79 

97.85 

102.46 

104.28 

103.73 

102.15 

92.42 

96.99 

97.75 

98.33 

98.72 

98.62 

100.30 

94.34 

96.34 

97.56 

99.30 

100.50 

100.00 

89.85 

89.53 

89.85 

92.68 

93.63 

97.38 

98.14 

87.80 

94.79 

94.97 

95.15 

95.06 

94.88 

95.69 

89.13 

92.76 

92.76 

93.55 

94.79 

95.42 

90.58 

89.21 

89.53 

91.83 

91.91 

94.43 

94.79 

86.66 

93.28 

92.59 

92.42 

92.59 

91.83 

93.37 

87.95 

91.41 

89.85 

91.24 

92.17 

92.25 

111.93 

112.39 

112.03 

112.09 

112.20 

114.84 

114.96 

115.04 

114.77 

114.79 

113.74 

112.43 

112.54 

1.089 

0.762 

0.587 

0. 500 

0.467 

0.369 

0. 330 

0.533 

0.570 

0.454 

0. 572 

0. 531 

1.175 

0.356 

0.579 

0.642 

0.564 

0.413 

0.435 

0. 371 

115.9 

274.4 

472.4 

936.6 

1295.0 

1654.4 

1820.3 

210.3 

412.9 

666.1 

818.7 

960.3 

1298.2 

1716.6 

194.0 

373.4 

546.1 

810.8 

1014.4 

1278.2 

542 

557 

563 

577 

575 

567 

918 

897 

928 

9 32 

969 

970 

993 

1008 

629 

714 

7 39 

809 

852 

904 

81.04 

77.88 

77.52 

80.19 

81.83 

84.82 

84.25 

77.16 

81.17 

81.17 

81.43 

81.63 

80.78 

82.78 

78.68 

80.06 

79.74 

80.65 

81.43 

81.63 

101/0 

102/ 0 

103/0 

104/0 

105/0 

106/0 

107/0 

108/0 

109/ 0 

LlO/O 

L11/0 

L12/0 

L13/0 

L14/0 

!19/0 

!20/0 

!21/0 

'22/0 

!23/0 

!24/ 0 

63.69 

57.47 

55.71 

57.50 

56. 56 

56.43 

56.92 

55.31 

55.22 

55.01 

54.59 

55.40 

57.80 

57.05 

56.31 

56.24 

55.07 

55.07 

~ 

Test 3, 

1 

G N (Air, A/ 1' 4 * = 6.5, 35 deg) 

85.37 

85.62 

85.45 

85.57 

85.69 

88.02 

88.15 

88.22 

88.06 

88.13 

87.57 

86.84 

87.00 

0.567 

0.993 

2.141 

4.059 

5.912 

0.567 

1.016 

1.901 

4.001 

7. 656 

0.544 

0.939 

1.836 

979.6 

981.1 

983.0 

981.9 

984.4 

1484.0 

1491.4 

1472.7 

1478.7 

1479.9 

1453.1 

1462.5 

1463.6 

51/0 

52/0 

53/ 0 

54/ 0 

55/0 

56/ 0 

57/ 0 

58/ 0 

59/ 0 

60/0 

61/0 

62/0 

63/0 

174 
TABLE C-2. ( Continued) 

Run/ 

Rerun 

164/0 

165/0 

166/0 

167/ 0 

168/0 

169/ 0 

170/0 

171/0 

172/0 

173/0 

174/0 

175/0 

176/0 

177/ 0 

178/0 

179/0 

180/0 

181/0 

1/1 

2/ 1 

3/ 1 

4/ 1 

5/ 1 

6/ 1 

7/ 1 

8/ 1 

9/ 1 

10/1 

11/0 

12/0 

I 

13/0 

14/ 0 

15/0 

16/ 1 

17/2 

18/ 0 

19/ 0 

20/0 

21/1 

22/ 0 

23/0 

24/ 0 

3.986 

7.586 

0.540 

0.923 

2.168 

3.963 

7.525 

0.540 

0.896 

2.118 

3.909 

7.439 

0. 556 

0.811 

2.021 

3.816 

7.664 

11. 303 

0.579 

0.869 

1.774 

3.885 

5.676 

0.525 

0.904 

1.747 

3.854 

5.579 

0.563 

0.927 

1.844 

3.963 

5.785 

0.590 

0.799 

1. 511 

3.498 

5.425 

0.590 

0.548 

0.590 

0.560 

1467.0 

1471.1 

1460.7 

1459.9 

1465.9 

1476.8 

1483.15 

1496.27 

1492.52 

1496.65 

1488.77 

1484.27 

1989.25 

1970.75 

1971.75 

1981.75 

1972.25 

1973.25 

T 

C 

(OR) 

992 

9 84 

863 

854 

857 

860 

8 56 

711 

718 

720 

726 

716 

615 

614 

615 

612 

617 

609 

44 

63.52 

63.76 

63.54 

63.65 

63.62 

63.82 

63.96 

64.00 

63.99 

63.92 

64.01 

64.00 

66.93 

66.73 

67.01 

67.03 

66.90 

66.94 

48 

87.66 

87.98 

87.49 

87.72 

87.53 

87.94 

88.08 

88.08 

87.97 

87.98 

88.10 

87.99 

91.05 

90.78 

91.20 

91.22 

91.00 

90.90 

Tap No. 

45 

Test 3, G1, N (Air, A/A, = 3.5, 35 deg) 5 ~ 

1039.34 

1035.97 

1002.22 

992.47 

1002.22 

977.09 

996.22 

981.59 

986.84 

982.72 

929.47 

938.09 

931. 34 

932.09 

924. 59 

1684.47 

1694.47 

1682.99 

1696.49 

1704.49 

1496.47 

1043.97 

1337.47 

631.97 

590 

619 

619 

617 

616 

6 72 

697 

712 

710 

702 

840 

863 

868 

866 

865 

660 

681 

689 

695 

696 

871 

844 

735 

512 

20.11 

20.18 

20.09 

20.08 

20.05 

20.07 

20.15 

19.97 

20.13 

20.04 

19.78 

19.85 

19.78 

19.91 

19.79 

20.91 

20.96 

20.86 

20.90 

20.07 

20.35 

19.79 

20.24 

19.41 

28.23 

28.30 

28.16 

28.06 

28.12 

28.28 

28.31 

28.08 

28.33 

28.14 

27.81 

27.91 

27.81 

27.94 

27.80 

29.23 

29.35 

29.27 

29.33 

29.34 

28.66 

27.76 

28.47 

27.18 

35.85 

35.91 

35.74 

35.67 

35.70 

35.72 

35.81 

35.51 

35.79 

35.64 

35.09 

35.22 

35.06 

35.28 

35.06 

37.30 

37.35 

37.20 

37.27 

37.26 

36.38 

35.39 

36.23 

34.70 

46 

35.20 

35.26 

35.07 

35.02 

35.07 

35.09 

35.10 

34.89 

35.17 

35.01 

34.49 

34.55 

34.40 

34.57 

34.48 

36.94 

36.86 

36.85 

36.83 

36.87 

36.18 

35.00 

35.85 

34.18 

47 

113.76 

114.61 

113.55 

114.03 

113.70 

114.34 

114.70 

114.46 

114.23 

114.29 

114.47 

114.52 

118.35 

117.98 

118.42 

118.39 

118.20 

118.51 

34.98 

35.03 

34.85 

34.78 

34.82 

34.89 

34.94 

34.68 

34.99 

34.79 

34.40 

34.47 

34.23 

34.49 

34.33 

36.40 

36.35 

36.35 

36.33 

36.32 

35.78 

34.79 

35.44 

33.89 

175 
TABLE C-2. ( Continued) 

Run/ 

Rerun 

P,/Pw Pc/Pw 

P P T Tap No. amb C cr 

(psia) (psia) (OR) 2 3 4 

~ ~~~~ 

I . 

~~ 

904/1 1.05 214.79 525 

905/0 1.05 415.45 521 

906/0 1.06 615.45 519 

415.18 

~~ ~ ~~ 

6.26 29.49 

6.27 1 29.15 

6.30 28.95 

~ 

~ 

7.97 

7.99 

8.05 

-~ 

6.77 34.36 

~ 6.78 1 

6.79 

=_ - 

~~- - 

34.50 

33.70 

33.37 

~~~ ~ 

103.59 

102.56 I 

102.43 

~ ~ ~ -~ 

Test 6, G1, NID (Air, A/A, = 8.0, 15 deg) I 

_- 

5/1 0.923 407.0 524 10

4/1 0.908 215.4 

6/0 0.915 509.5 51 1 - 

0.968 401.0 

3/1 0.975 505.0 513 

- -I iil i::: 34.38 

~~ 

86.33-8.13 1 :- 

85.57 

- ~.~ 

-_ 

801/0 1.05 214.84 

802/0 1.06 415.68 

803/0 1.05 615.51 

901/0 0.61 216.12 

902/0 1.05 415.45 

903/0 1.21 616.29 

Test 6, G1, N2B (Air, A/A, = 4.0, 15 deg) 

- __ -~ -~ ~ 

6.71 

- - _- 

7/0 0.975 200.6 504 

8/0 0.983 400.4 505 

9/0 1.170 507.2 506 

~~ 

116.85 

114. 51 

114.32 -~ 

51 7 

499 

502 

52 5 

518 

514 

~ ~~ 

6.10 

6.i3 

6.15 

6.13 

6.15 

6.18 

__ 

. ~- 

14.61 

14.62 

14.65 

14.75 

14.83 

15.01 

~- ~~ 

91.66 

91.87 

91.80 

- 

30.17 

30.04 

30.03 

28.58 

28.72 

28.82 

176 
TABLE C-2. ( Concluded) 

C 

P 

(psia) 

Tap No. 

Tc 

(OR) 44 48 45 46 47 

501/0 

502/0 

503/0 

504/0 

505/0 

I I 

0.585 

0.480 

0.379 

0.390 

0.386 

P /Pw 

506/0 

507/0 

508/0 

509/0 

511/0 

512/0 

513/0 

514/0 

0.424 

0.435 

0.371 

0.720 

0.409 

0.424 

0.416 

0.473 

1488.21 

1574.00 

588.84 

5.68 

5.66 

5. 82 

5. 87 

5.82 

5.68 

5.76 

5.87 

18.79 

18.49 

19.03 

18.97 

18.65 

18.43 

19.40 

20.39 

46.00 

45.62 

47.26 

46.77 

48.83 

44.88 

50.35 

53.16 

49.19 

48. 54 

50.23 

49.88 

51.07 

46.97 

53.08 

56.59 

47.53 

46.95 

48.52 

48.12 

50.15 

46.34 

51.76 

54.91 

177 
TABLE C-3. NOZZLE CALIBRATION DATA 

FOR ORBITER CLASS 

- .- 

3G. 71 

3G. G5 

3G. G3 

3G. 82 

3G. 34 

3G. 24 

3G. 28 

3G. 19 

38.93 

38.90 

38.85 

37. G7 

... 

Test 3, GI, N,i (Air, A/A, = 5. 3, Contoured) ~ 

976.20 

980.32 

972.07 

975.07 

472.45 

475.70 

476. 57 

482.07 

99.47 

99.26 

100.16 

99.59 

903 

909 

905 

899 

904 

912 

915 

925 

889 

890 

884 

881 

24.58 

24. 54 

24. 51 

24. GO 

24.16 

24.11 

24.14 

24.07 

25.32 

25.32 

25.30 

25.18 

36.79 

36.72 

3G. 70 

3G. 84 

36.47 

36.40 

36.43 

36.33 

38.24 

38.15 

38.1G 

3G. 41 

182/0 

183/0 

184/0 

185/0 

186/0 

187/0 

188/0 

189/0 

190/0 

191/ 0 

192/0 

193/0 

0.492 

0.852 

1.823 

2.758 

0.529 

1.012 

2.021 

2.977 

0.529 

1.062 

2.048 

3.201 

42. OG 

41.98 

11.94 

12.14 

41.81 

41.73 

41.7G 

41.64 

42. G1 

42. GG 

42.48 

35. G3 

Test 3, GI (Air, A/A, = 4.0, 10 deg) 

19.82 

19.74 

19. GG 

19.74 

19.27 

19.20 

19.21 

19.24 

19. G7 

19. G1 

19. GO 

19.57 

45 

.- 

__~ 

~ 

860 

867 

874 

877 

8 86 

888 

890 

895 

873 

882 

8G7 

861 

;.,:,;.,:..: :' 

,._.'. " ' 

.' '...'.< .,.. > .; ,.,. y,: :. :. ..4,'l:..:. I. 

. . ~- 

,., ,\>.;:.:;: 

21.81 

21.75 

21.68 

21.75 

21.40 

21. 31 

21.35 

21.39 

44 

~ 

20.95 

20.87 

20.80 

20.90 

20.49 

20.43 

20.13 

20.48 

20.45 

20.47 

20. 41 

4G 

~. 

29.8G 

29.77 

29. GG 

29.77 

29. 38 

29. 31 

29. 31 

29. 38 

29.68 

29. 51 

29.55 

29.40 

47 

~ 

978.26 

980.88 

980.51 

982.76 

483.63 

487.88 

488.51 

490.76 

104.42 

113.06 

114.14 

115.1G 

..:._:. , .'...;.. .. , . .. ~. ..., ~ 

.:::;:, ;.:;+ ;-:, <s'( + ......' ;:-?:.><;.: ...._. 

...' :....:.::., .: I . _.:. . . 

97/ 0 

98/0 

99/ 0 

loo/ 0 

101/ 0 

102/ 0 

103/ 0 

105/0 

104/0 

10G/O 

107/0 

108/ 0 

0.482 

0.819 

1.797 

2.729 

0.521 

0.997 

2. 137 

2.988 

0.637 

1.078 

2.087 

3.240 

29.99 

29.89 

29.75 

29.92 

29.01 

28.90 

28.90 

28.96 

29.85 

29.72 

29.70 

29. 58 

30.93 

30. 88 

30.73 

30.85 

29.94 

29.81 

29.79 

29.84 

31:02 

33.50 

33.44 

33.40 

48 49 

Test 1, GI, N:$, (Air, A/A, = 4.0, 25 deg) - 

1G77. G2 

1313.93 

743. 90 

475. G2 

1493.90 

1704.95 

, 

I 24.93 

' 24.86 

24.21 

23.87 

24.74 

25.23 

8 54 

849 

8 50 

851 

51 :: 

97G 

26.40 

2G. 1G 

25. 39 

24.99 

2G. 03 

2G. 45 

::o. 24 

*30. 03 

29.10 

28.49 

29.94 

:;o. 49 

2G. 54 

2G. GO 

2.5. 18 

24.99 

26. 08 

26. 37 

27.74 

27. 63 

2G. 77 

2G. 33 

27. 6.5 

27.99 

25. 31 

25.21 

24.50 

24.19 

25.21 

25.59 

178 
TABLE C-3. (Concluded) 

Run/ 

Rerun 

a nib 1 'c 

(psia) (psia) 

T 

46.62 

43.18 

41.91 

41.48 

41.65 

42.68 

601/0 

602/ 0 

G03/ 0 

604/ 0 

605/ 0 

GOG/ o 

44.03 

41.03 

39.37 

39.22 

39.48 

39.98 

2.610 

2. GI0 

2.610 

2.610 

3. 610 

2.610 

1067.12 

963.96 

563.96 

1076.07 

1468.17 

1759.22 

T C 

(OR) 

St 1, G,, 

581 

810 

937 

1000 

1019 

1017 

T 

44 I 45 I 46 

43.71 

41.08 

39.48 

39.35 

39.59 

40.23 

No. 

47 

45.48 

42.05 

40.65 

40.58 

40.75 

41.48 

44.84 

41.44 

40.29 

40.02 

40.19 

41.02 

45.45 

41.44 

39.48 

39.37 

39.51 

40.27 

179 
TABLE C-4. NOZZLE CALIBRATION DATA 

FOR SRB-ALONE CLASS 

Run/ 

Rerun 

P amb C 

P 

(psia) (psia) 

I 29.2 

30.6 

59.1 

60.5 

82.1 

85.1 

45.9 

45.8 

46.5 

35/0 14.479 1275.8 

36/0 14.475 827.4 

37/0 14.473 412.3 

42.8 

45.7 

44.3 

27.8 35.2 

27.5 35.0 

27.5 35. 3 

180 

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

:-

113/0 14.509 417.5 

114/1 14.507 1547.3 973 19.7 

34.327 

33.6 
APPENDIX D 

BIBLIOGRAPHY OF TEST DATA REPORTS 

Test 1 

Andrews, C. Donald and Cooper, C. E., Jr. : A Transonic and Supersonic Investigation of Jet Exhaust Plume Effects on the Afterbody and 

Base Pressures of a Body of Revolution. LMSC-HREC D306909, Lockheed 

Missiles and Space Company, 1974. 

Test 2 

Hair, Leroy M. : Test Data Report for Solid Propellant Plume Aerodynamics Test Program in MSFC 14 x 14 Inch Trisonic Wind Tunnel. 

RTR 016-1, REMTECH, Inc., 1974. 

Test 3 

Andrews, C. Donald and Ketter, F. C., Jr. : A Subsonic and Transonic 

Investigation of Triple Nozzle Jet Exhaust Plume Effects on the Base 

Pressures of a Body of Revolution. LMSC-HREC D390200, Lockheed 

Missiles and Space Company, 1974. 

Test 44 4B 

Andrews, C. Donald: A Subsonic and Transonic Investigation of Jet 

Exhaust Plume Effects on the Afterbody and Base Pressures of a Body 

of Revolution in the NASA-ARC 6 x 6 Foot Supersonic Wind Tunnel. 

LMSC-HREC D390656, Lockheed Missiles and Space Company, 1975. 

Test 4C 

Andrews, C. Donald: An Investigation of Solid Rocket Booster Jet Exhaust 

Plume Effects on the Base Pressures of the Space Shuttle External Tank 

and Solid Rocket Booster, Interim Report. 

Lockheed Missiles and Space Company, 1975. 

LMSC-HREC D390657, 

Test $ 

Hair, Leroy M. : Test Data From Solid Propellant Plume Aerodynamics 

Test Program in Ames 6 x 6 Foot Supersonic Wind Tunnel. RTR 016-2, 

REMTECH, Inc., 1975. 

181 
Test 6 

Baker, D. C. : Investigation of Solid Propellant Plume Effects on Model 

Base Pressures at Mach Numbers 0.5, 0.9, and 1.2. AEDC-DR-75-79, 

Arnold Engineering Development Center, 1975. 

Test 7 (except P ) 

C 

Anderson, C. F. : An Experimental Investigation Into the Effects of Jet 

Plumes on the Space Shuttle External Tank Base Pressure Distributions. 

AEDC-DR-75-111, Arnold Engineering Development Center, 1975. 

P Values for Test 7 

C - 

Boyle, W. W. and Jordan, T. A. : Tabulated Test Data and Plume CharaCharacteristics for the Plume Technology Test Program. M-9230-76-31, 

Northrop Services, Inc., 1976. 

Test 8 

Hendershot, K. C. : Results of the NASA/MSFC FA-23 Plume Technology 

Test Program Performed in the NASA/ Ames Unitary Wind Tunnels. 

XN-5798-A-2, Calspan Corp., 1977. 

Nickel, Charles E. : FA23 Data Selection. RM016-7, REMTECH, Inc. , 1977. 

Test 9 

Love, Don A. : A Subsonic, Transonic and Supersonic Investigation of 

Triple and Single Nozzle Jet Exhaust Plume Effects on the Base Pressures 

of a Body of Revolution (FA15). LMSC-HREC D568090, Lockheed Missiles 

and Space Company, 1977. 

Test 10 

Love, Don A. : Investigation of Jet Exhaust and Local Mach Number Effects 

on the Solid Rocket Booster (SRB) Base Pressures (FA19) Final Report. 

LMSC-HREC D568157, Lockheed Missiles and Space Company, 1978. 

182 
IA P PROVAL 

SPACE SHUTTLE AFTERBODY AERODYNAMI CSI PLUME 

S IMULATI ON DATA SUMMARY 

By Kenneth L. Blackwell and Leroy M. Hair 

The information in this rep’ort has been reviewed for technical content. 

Review of any information concerning Department of Defense or nuclear energy 

activities or programs has been made by the MSFC Security Classification 

Officer. This report, in its entirety, has been determined to be unclassified. 

183 
TECHNICAL REPORT STANDARD TITLE PAC 

Space Shuttle Afterbody Aerodynamics/ Plume Simulation 

eorge C. Marshall Space Flight Center 

echnical Memorandum 

National Aeronautics and Space Administration 

Prepared by Systems Dynamics Laboratory, Science and Engineering 

*Engineering Specialist, REMTECH, Inc. Huntsville, Alabama 35805. 

16. ABSTRACT 

A series of parametric wind tunnel tests was conducted to provide a base for developing 

a simulation of afterbody/base aerodynamics for multibody/ multibase rocket-powered vehicles 

(such as Space Shuttle) which use unheated air as the simulant gas in development wind tunnel 

tests. The tests described herein were parameterized on external configuration, nozzle internal 

configuration, base geometry, propulsion gas type (air, CF4, solid propellant exhausts), and 

freestream Mach number (0.5 to 3.5). The tests were conducted over a 4-year period in the 

MSFC 14-Inch Trisonic, AEDC-PWT-4T, and Ames 11-Foot wind tunnels. Presented in this 

report are the data and pertinent reference information necessary to perform an analysis which 

would lead to a simulation procedure. The type of data obtained during the tests described 

herein include model base, afterbody, and nozzle internal surface static pressure distributions, 

model chamber pressure and temperature, and freestream conditions. Also included is a brief 

description of simulation procedures that have been used by the Space Shuttle program. 

Plume-induced aerodynamics 

Plume simulation 

Wind tunnel tests 

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NASA-Langley, 1978 

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