NUREG/IA-0070

International

Agreement Report

Assessment of RELAP5/MOD2

Cycle 36.04 with LOFT

Large Break LOCE L2-3

Prepared by

Y. S. Bang, H. J. Kim, Korea Institute of Nuclear Safety

S. H. Kim, Korea Atomic Energy Research Institute

Korea Institute of Nuclear Safety

P.O. Box 16, Daeduk-Danji

Daejoni 300-3 1

Republic of Korea

Office of Nuclear Regulatory Research

U.S. Nuclear Regulatory Commission

Washington, DC 20555

April 1992

Prepared as part of

The Agreement on Research Participation and Technical Exchange

under the International Thermal-Hydraulic Code Assessment

and Application Program (ICAP)

Published by

U.S. Nuclear Regulatory Commission
NOTICE

This report was prepared under an international cooperative

agreement for the exchange of technical information.' Neither

the United States Government nor any agency thereof, or any of

their employees, makes any warranty, expressed or implied, or

assumes any legal liability or responsibility for any third party's

use, or the results of such use, of any information, apparatus product or process disclosed in this report, or represents that its use

by such third party Would not infringe privately owned rights.

M

Available from

Superintendent of Documents

U.S. Government Printing Office

P.O. Box 37082

Washington, D.C. 20013-7082

and

National Technical Information Service

Springfield, VA 22161
NUREG/IA-0070

SInternational

Agreement Report

Assessment of RELAP5IM\OD2

Cycle 36.04 with LOFT

Large'Break LOCE L2-3

Prepared by Y. S. Bang, H. J. Kfim, Korea Institute of Nudear Safety

S. H. Kim, Korea Atomic Energy Research Institute

Korea Institute of Nuclear Safety

P.O. Box 216, Daeduk-Danji

Daejoni 300-31

Republic of Korea

Ofice of Nuclear Regulatory Research

U.S. Nuclear Regulatory Commission

Washington, DC 20555

April 1992

Prepared as part of

The Agreement on Research Participation and Technical Eicbangc

under the Jnternatioaial Thermal-Hydraulic Code Assessment

and Applicuio Program (1CMP
NOTICE

This report is based on work performed under the sponsorship of The Korea

Advanced Energy Institute of Korea. The information-in this report has been

provided to~the USNRC under the terms of an information exchange agreement

'between the United S tates and Korea (Agreement on Thermal-Hydriaulic Research

between.the United States. Nuclear Regulatory Commiission and The Korea Advanced

Energy Research Institute, May 1, 1986). Korea has consented to the publication

of this report as a USNRC document in order that it may receive the widest

possible circulation among the reactor safety community. Neither the United

States Government nor Korea or any agency thereof, or any of their employees,

makes any warranty, expressed or- implied, or assumes any legal liability of

responsibility-for any third party's use, or the results of such use, or any

information, apparatus, product or process disclosed in this report or

represents that its use by such third party would not infringe privately

owned rights.
ICAP

ASSESSMENT OF RELAP5/IIODZ Cycle 36.04

USING LOFT LARGE BREAK LOGE L2-3

Abstract

The LOFT LOGE L2-3 was simulated using the RELAP5/110D2 Cycle 36.04 code to

assess its capability to predict the thermal-hydraulic phenomena in LBLOCA of

the PWR. The reactor vessel was simulated with two core channels and split

downcomer modelling for a base case calculation using the frozen code. From

the results of the base case calculation, deficiencies of the critical flow

model and the GRE correlation at high flow rate were identified, and the severeness, of the rewetting criteria were also found. Additional calculation using

an updated version of RELAP5/110D2 Cycle 36.04 including modifications of the

rewet criteria shows a substantial improvement in the core thermal response.

Mi

List of Contents

Page

Abstract . .. . . .. . . . . . . .. . . . .. . . . . .. iii

List of Tables............................................ vi

List of Figures .......................................... vii

1. Introduction ................................... 1......I1

2. Facility and Test Description .................. 0...... 3

2.1 Facility Description ......... o................ 3

2.2 Test Description ... ..................o............. 3

2.3 Measurement Uncertainty ............. o..... o.........4

3. Code and Modelling Description ............ o.............5

3.1 input modelling .... o... o........................... 5

3.2 Initial Conditions and Boundary Conditions ........... 6

4. Base Case Calculation.......................... i........ 8

4.1 Loop Behavior ...... o......o... o.............. o.......8

4.2 Secondary Side Behavior and F(CCS Performance ......... 9

4.3 Reactor Vessel Behavior ...............-............ 10

4.4 Fuel Rod Thermal Response ... o...o....... o...... 12

5.Sensitivity Study .... o................................ 14

6. Run Statistics ......................o.............o.....16

7. Conclusions..........................o.............. 17

References .......................................... 18

Appendix A Update List for RELAP5IMOD2 Cycle 36.04 ........ A-1

Appendix B A Base Case Input Deck for A Steady State

Calcuation .... .......... o......... o.......o. B-1

Appendix C A Base Case Input Deck for a Transient

Calculation.........................-,...... C-i

Appendix D Update List for PSI-EIR 83 based on

RELALP5/moD2 c 36.04o......................... D-1

V
List of Tables

Page

Table 1 Summary of comparison of the initial conditions

between the measured and the calculated in base case 19

Table 2 Summary of comparison of the sequence of events

between the measured and the calculated in base case 20

Table 3 Uncertainties of measurements 21

Table 4 Summary of reactor vessel modelling in base case calculation 22

Table 5 Run statistics data in base case calculation 23

Vi
List-of Figures Page

Fig.l Axonometric configuration of LOFT L2-3 test 24

Fig.2 Nodalization diagram for base case calculation-of LOFT L2-3 test 25

Fig.3 Axial power distribution in base-case calculation of L2-3 test 26

Fig.4 Comparison of mass flow rate at broken loop cold leg

between the base case calculation and the experiment 27

Fig.5 Comparison of mass flow rate at broken loop hot leg

between the base case calculation and the experiment 28

Fig.6 Comparison of mass flow rate at intact loop cold leg

between the base case calculation and the experiment 29

Fig.7 Comparison of net mass flow rate into the core.

between the base case calculation and the experiment 30

Fig.8 Comparison of steam dome pressure at S/G secondary side

between the base case- calculation and the experiment 31

Fig.9 Comparison of accumulator injection flow rate

between the base case calculation and the experiment 32

Fig.1O Comparison of accumulator liquid level

between the base case calculation and the experiment 33

Fig.11 Comparison of IIPSI flow rate

between the base case calculation and the experiment- 34

Fig. 12 Comparison of LPSI flow rate

between the base case calculation and the experiment 35

Fig. 13 Comparison of primary system pressure between the base case calculation and the experiment 36

Fig.14 Comparison of coolant temperature in lower plenum

between the base case calculation and the experiment 37

Fig.15 Collapsed liquid levels calculated in the base case calculation

for the broken side downcomer, intact side downcomer, hot core

channel and average core channel of the reactor vessel 38

Fig.16 Comparison of cladding temperature at 5 inches of hot fuel

between the base case calculation and the experiment 39

Fig.17 Comparison of cladding temperature at 16.5 inches of hot fuel

between the base case calculation and the experiment 40

Fig. 18 Comparison of cladding temperature at 27.5 inches of hot fuel

between the base case calculation and the experiment 41

Vii
Page

Fig.l9 Comparison of cladding temperature at 39 inches of hot fuel

between the base case calculation and the experiment 42

Fig.20 Comparison of cladding temperature at 49.5 inches of hot fuel

between the base case calculation and the experiment 43

Fig.21 Comparison of cladding temperature at 60 inches of hot fuel, between the base case calculation and the experiment .44

Fig.22 Wall heat transfer coefficients calculated in the base case

calculation at volume 2 and 3 of hot fuel 45

Fig. 23 Liquid fractions calculated in the base case calculation

at volume 2 and 3 of hot fuel 46

Fig.24 Flow regimes predicted in the base case calculation

at volume 2 and 3 of hot core channel 47

Fig.25 Comparison of cladding temperature at 16.5 inches of hot fuel

between the base case calculation and the sensitivity calculation 48

Fig.26 Comparison of cladding temperature at 27.5 inches of hot fuel

between the base-case calculation and the sensitivity calculation 49

Fig.27 Comparison of cladding temperature at 39 inches of hot fuel

between the base case calculation and the sensitivity calculation 50

Fig. 28 Comparison of cladding temperature at 49.5 inches of hot fuel

between the base case calculation and the sensitivity calculation 51

Fig.29 Comparison of void fraction at volume 5 of hot core channel

between the base case calculation and the sensitivity calculation 52

Fig. 30 The required CPU time versus the advanced tine

in the base case calculation 53

Fig.3l Time step size of base case calculation 54

Viii
Executive Summary

This report documents the assessment calculations using the RELAP5/110D2

Cycle 36.04 to predict thermal-hydraulic response of Loss of Fluid Test (LOFT)

system during the Loss of Coolant Experiment (LOCE) L2-3. LOCE L2-3 simulated a

200 % offset shear at the discharge of the Primary Coolant Pump (PCI') in the

four loop commercial PWR.

To simulate LOFT system specific to L2-3 experiment, the reactor core was

modelled with two separate flow channels and the reactor vessel downcomer was

described by two equally-split channels. Three heat structures were used to

describe the LOFT fuel assemblies.

The results of the base case calculation using the frozen code of the RELAP5/

MOD2 were compared with the experimental data in terms of loop flows, secondary side pressure, Emergency Core Cooling System (ECCS) performance, reactor

vessel behavior and fuel rod thermal response. As result of comparisons, the

overall hydraulic behavior was well-predicted, while fuel rod thermal response

was poorly predicted.

Mlajor reasons of the discrepancies in the prediction were identified as the

code deficiencies in the thermal-hydraulic models ; (1) underprediction of cold

leg break flow due to the deficiency of critical flow model, (2) poor prediction of the core early heatup during blowdown due to the deficiency of CHF

correlation at high flow rate, and (3) poor prediction of rewetting phenomena

due to the severeness of the rewet criteria in the frozen code.

To reidentify the deficiencies found in the base case calculation and to

determine the effectiveness of the rewet criteria change in the frozen code,

a sensitivity calculation was performed using an updated code with the PSI

modification. The result of the sensitivity calculation shows that the rewet

phenomena was well-predicted by the PSI-modified criteria.

ix

1. Introduction

RELAP5/MOD2[l], a frozen version by US Nuclear Regulatory Commission (USNRC),

has been assessed through the International Code Assessment and Application

Program (ICAP) for its capability and deficiencies in the prediction of the

postulated Large Break Loss of Coolant Accident (LBLOCA) in Pressurized Water

Reactor (PWR).

This report is one of the Korean ICAP contributions to support code assessmnent, code deficiency identification and code improvement. In this study the

RELAP5/IIOD2 Cycle 36.04 was assessed for the Experiment L2-3 conducted in the

Loss of Fluid Test (LOFT) at Idaho National Engineering Laboratory (INEL) (2).

The Experiment L2-3, as one of the Integral Effect Test (IET), was a Large

Break Loss of Coolant Experiment (LBLOCE), which represented the postulated

LBLOCA in the typical Westinghouse type PWR with four loop. During LOCE L2-3,

two Primary Coolant Pumps (PCP) in LOFT system were set to operate without

coastdown, this PCP running was found to have significant effect on the reactor

core thermal response, i.e, the early core quenching in blowdown phase. This

blowdown quenching phenomena was called as 'rewet' which was due to a quick

return to the nulcleate boiling heat transfer regime from the post dryout

regime and was one of the important assessment items in the previous LRLOCA

calculations [3, 4].

The objectives of this study are to predict the major hydraulic behavior

and thermal response of the LOFT system during the LOCE L2-3 and to identify

deficiencies of the frozen RELAP5/MOD2 Cycle 36.04 code in simulating thermalhydraulic phenomena specific to LBLOCA by comparing the calculation results

with the experiment data. From the findings obtained by ICAP activities [5],

it was known that the major deficiencies of RELAP5/IIOD2 were summarized as

the Critical Heat Flux (CHF) correlations, the critical flow model and the

1
interfacial drag correlations. This, study, therefore, is focused to confirm

whether the deficiencies as stated above are still found in the Experiment

L2-3 simulation. And to investigate the sensitivity of the rewet criteria in

the RELAP5/IIOD2, an updated version from Cycle 36.04 using the modified rewet criteria by Aksan (6], at Paul Scherer Institute (PSI), Swiss was tested

in this study.

The descriptions for LOFT facility and L2-3 experiment are presented in

chapter 2,. the RELAP5 input modelling in chapter 3 and the results of a base

case calculation and their discussions in chapter 4. In chapter 5, a result

of sensitivity calculation is described and the conclusions obtained from

the present study are summarized in chapter 6.

2
2. Facility and Test Description

2.1 Facility Description

The LOFT facility is an experimental 50 NWt PWR designed to simulate LOGA's

and anticipated transients and to provide data on the thermal-hydraulic

phenomena occuring throughout the system (7]. It is a scaled representation

of a conmmercial PWR of Westinghouse type having 4 loops -with a volume ratio

of 1/60. The LOFT system consists of five major systems : rea ctor system,

primary coolant sysytem, blowdown suppression system, emergency core cooling

system and secondary coolant system, and also includes instrumentations. The

lengths of the core and reactor vessel is 1.68 and 7 m, respectively. The

overall configuration is shown in Fig.1.

2.2 Test Description

Experiment L2-3 was performed as part of LOFT program Power Ascension Series

(L2), which was designed to investigate the response of LOFT nuclear core to

the blowdown, refill and reflood transient during LOCE.

Experiment L2-3 represents a postulate 200 X double ended offset shear of the

pump discharge piping in the cold leg of commercial PWR. The specific objectives

of L2-3 test were to determine the corewide and spatial variation of fuel rod

cladding thermal response, to identify thermal-hydraulic phenomena and their

effect on the core of LOFT and to determine the ECCS performance and core

reflood characteristics. During L2-3 eprimen, primary coolant pumps were set

to continue to operate, which results in the early quenching during blowdown,

called rewet. The phenomena of rewet is currently known as early return to

3
nucleate boiling in the core, w hich has been a common interesting point of

code assessment [3, 4J.

Prior to Experiment L2-3, LOFT facility was set to be a primary system

pressure of 15.06 MPa, primary system cold leg and hot leg temperature of

560.7 K and 592.9 K repectively, and a loop mass flow rate of 199.7 kg/sec.

Initial reactor power level was 36.7 M1W with a maximnum linear heat generation

rate (LHGR) of 39.4 !'M/m. Table 1 presents a summary of initial conditions of

Experiment LZ-3.

The experiment was initiated by opening the Quick Opening Blowdown Valves

((QJBV) both in hot leg and cold leg. Reactor was scrammed at 0.103 sec after

initiation of the experiment by operator signal. Identifiable phenomena in

the experiment are listed in Table 2. Injection from accumulator began at 17

sec, approximately when primary system pressure moved down to 4.18 IlPa. High

Pressure Safety Injection (HPSI) system and Low Pressure Safety Injection (L

PSI) system started to inject at 14 sec and 29 sec and LOFT core volume was

finally reflooded at approximately 55 sec.

2.3 Mieasurement Uncertainty

Uncertainties of the experimental data and computed variables were fully discussed in reference [2] for L2-3 test. Uncertainties on the measured values

and computed values used for comparisons with calculation in this report are

presented in Table 3.

4
3. Code and Modelling Description

RELAP5/M'1D2 Cycle 36.04, frozen version of the code by USNRC, was used in the

present calculation with modifications of some indexing schemes. An update

procedure is listed in Appendix A, which is exactly the same as that in L2-5

assesment report [8]. Since any RELAP5 input specific to L2-3 experiment was

not obtained from INEL, a reference input was developed by the authors based

on the input used in the previous L2-5 experiment assessment [8].

3.1 Input Modelling

All components except a reactor-core and a reactor vessel downcomer of LOFT

for L2-3 experiment were geometrically modelled as the same as those for L2-5

case (8] i.e, equal volumes, junctions and heat structures. A nodalization

diagram used in the present calculation is shown in Fig.2. Total number of

hydrodynamic volumes, junctions and heat structures are 128 149 and 27.

The reactor core was modelled by two flow channels; a hot channel and an

average channel representing the central fuel assembly ( numbered by 5 in the

reference [7]) and the other peripheral fuel assemblies, respectively. Each

flow channel was divided by six volumes with equal lengths. Two flow channels

were linked by six crossflow junctions to allow crossflow in the core with

a specified junction loss coefficient of 4.69 for all crossflow junctions.

These junction loss coefficients were selected as the same as those in the

Best Estimate Prediction for L2-5 experiment [9].

The reactor vessel downcomer was modelled by two split f low channels : an

intact side downcomer and a broken side downcomer. Each downcomer has five

volumes including a volume representing an upper annulus part above the

cold leg nozzles. To describe an azimuthal flow across the downcomer, four

5
crossf low junctions were used to link four volumes between the intact-side

douncomer and the broken-side one with exception of the volumes representing

the cold leg nozzles. Loss coefficients at the downcomer crossflow junctions

were tuned to match the measured loop flow behavior, accroding to the reference

[9]. The values used in the present calculation ranges from 18.0 to 98.0

with their junction elevations.

Originally LOFT fuel rods had two types of axial power profile : a high

power shape for central fuel assembly and a low power shape for peripheral fuel

assemblies. Both of them have almost identical shapes but have different magnitudes in LHGR. During L2-3 input preparation, however it is found that an

actual summation of rod power integrated over the full length of rod did not

match and was lower than the experimental total power level, 36.7 NW. In the

present study, three heat structure component were used to model the LOFT fuel

rods: 204 hot rods in the central fuel assembly, 572 average rods and 574

intermediate rods in the peripheral fuel assemblies repectively. And the axial

power shapes can be determined by the experimental LHGR distributions (2) for

the hot rods and average rods. For the intermediate fuel rods heat structure,

a mean LHGR distribution of hot and average rods can be used. This modelling

scheme of fuel rods can match a given total power. The profiles of LHGR's were

shown in Fig.3 and Table 4 presents a summary of reactor vessel modelling.

3.2 Initial Conditions and Boundary conditions

To provide all initial conditions of the whole system prior to transient, a

steady state run was carried out with seven steady state controllers : two

primary coolant pump speed controllers, a pressurizer heater power controller

a pressurizer spray valve area controller, a letdown and charging valve area

controller, a main steam control valve (IISCV) area controller and a feedwater

6
flow rate controller. A steady input deck was provided in Appendix B.

The result obtained from the steady state run was compared with the measured

initial conditions in Table 1. The RELAP5 calculated results generally agree

with the experimental conditions.

Boundary conditions required to simulate the L2-3 experiment are almost the

same as those in L2-5 experiment except PCP running. The PCP speed during the

the transient was assumed to be constant, which was a simple approximation of

the real PCP running behavior showing oscillations around a fixed speed during

the transient [2].

Based on the experiment data (2], the reactor power history and containment

pressure were described as time dependent tables. Performance curves for HPSI

and LPSI flow rate as function of cold leg pressure were provided in the input.

Feedwater flow rate was reduced to be zero in 2.5 seconds after LOGE initiation

using a time-dependent junction as the same as the L2-5 experiment. And the

steam generator secondary side air-cooled condenser was modelled as a timedependent volume with a constant pressure of 2.069 IlPa during the transient.

All informations of the boundary conditions were provided in the steady and

transient input deck., The transient input deck was listed in Appendix C.

7
4. Base Case Calculation

The L2-3 LOCE was calculated up to 100 sec using all initial conditions

obtained from steady state run. Some additional components such as pressurizer

spray, letdown and charging systems used for the steady state calculation are

deleted in transient input deck.

The sequence of events during transient calculation are presented in Table 2

as compared with L2-3 experiment chronology. In this chapter, the predicted

important thermal-hydraulic parameter such as system pressure, loop mass flow

rates and cladding temperatures are compared with the measured data.

4.1 Loop Behavior

Fig.4 shows a comparison of the calculated mass' flow rate with the measured

one at the broken loop cold leg up to 40 sec. An overall behavior of break

flow was well predicted by RELAP5/IIOD2 except the underprediction during a

short period from 3 sec to 9 sec. This period corresponded to the transition

phase from the subcooled break flow to the two-phase break flow. The subcooled

break flow was completed at about 3 sec both in calculation and in experiment

as shown in Table 2. After that time the break flow was well simulated by the

RELAP5 calculation. The underprediction of break flow during the phase transition period can be considered as a deficiency of the RELAP5/M'JD2 critical flow

model. This led the reactor vessel to contain more coolant inventory than the

experiment, which amounts to 400 kg approximately. This overestimated coolant

inventory may suppress the core heatup discussed in later chapter.

Fig.5 presents a comparison of mass flow rate in the broken loop hot leg.

As expected, the magnitude of break flow was less than that in the cold leg due

8
to higher flow resistance in the hot leg. The calculated break flow in hot leg

was well-agreed with the experimental result.

Mass flow rate in the intact loop cold leg was shown in Fig.6. The predicted

mass flow rate was almost similar to the measured one. However, the calculation

did not show several jumps which can be found in the experimental behavior with

high frequencies after 20 sec. It was regarded as the effect of void oscillation phenomena induced by the highly subcooled ECC injection water during the

reflood phase.

Fig.7 indicates a comparison of the net flow into the core, iLe intact loop

cold leg flow minus broken loop cold leg flow. The intact loop cold leg mass

flow, driven by the operating pumps, exceeded the broken loop flow from 3 sec'

to 6 seconds causing an increase in positive core flow, which had reversed

after saturation in the lower plenum at about 7 sec. The calculation result

was in good agreement with the experimental data.

In general,* the predicted loop behaviors agreed-well with the experiment data

within the range allowed by the instrument uncertainty except the underprediction of cold leg break flow during the transition period.

4.2 Secondary Side Behavior and ECCS Performance

Fig.8 shows a comparison of the steam dome pressure of the steam generator

secondary side. The experimental data used in this comparison was not fully

qualified one but accurate for initial condition only. The predicted pressure

was fairly well-agreed to the measured one up to 40 sec. Difference after 40

sec was considered to have little effect on the primary side behavior since

the transient was fast enough to neglect the heat transfer from the secondary

side.

Fig.9 presents a comparison of acculumator injection flow rate and Fig.10

9
a comparison of accumulator liquid level. The calculated injection flow rate

was larger before 42 sec and then lower than the experiment, while the accumlator liquid level was well agreed to the experiment. The overprediction of mass

flow rate during 20 to 40 sec can be due to a underprediction of the p rimary

system cold leg pressure discussed in later chapter. The overpredicted injection mass amounts to 180 kg approximately. The experiment shows that the injection continued until 60 sec, while the calculation shows that the injection

was completed at 42 sec. From the fact that the measured liquid level was

almost stationary at 42 sec as shown in Fig.l0, it can be stated that the jump

and oscillation in the injection mass flow rate is not a real situation but a

measurement error.

Figs. 11 and 12 show comparisons of mass flow rates through a HPSI line and

LPSI line. During the early period of injection, some overpredictions were

found in both injection flow rates, whose total amount was about 65 kg. This

overprediction was also due to the primary system pressure. However, the overall injection behaviors were comparatively close to the experiment.

4.3 Vessel Phenomena

Fig. 13 shows a comparison of primary system pressure at the upper plenum.

The predicted behavior agreed with experiment data very well. A little

earlier depressurization was found in calculation than that in the experiment

before 10 sec , which was resulted partly from an underprediction of cold leg

break flow (Fig.4). The calculation also presented a little lower pressure

after 20 sec than the experiment. It resulted in the early high ECC injection

behavior as stated in the previous chapter and yielded a underestimation of the

liquid coolant temperature in the lower plenum as shown in Fig. 14, which was

a saturation temperature at the corresponded pressure.

10
Fig. 15 shows the collapsed liquid levels in the two downcomer channels and

in the two core channels of reactor vessel. Since no experiment data for these

items were availbie, the predicted levels are plotted only.

The liquid level behaviors in core were found to be almost identical in both

average channel and hot channel. From these level behaviors, it is shown that

the LOFT core was almost empty in. 5sec and then filled with liquid up to 2.36

in in 8 sec by the positive net flow into the core as explained in the previous

chapter. This substantial liquid filling up for a short period yielded a

corewide rewet, and the rewet was completed in 8 sec. A core re-empty was predicted at 14 sec, a lower plenum was fully refilled by ECC water injection at

35 sec, and a core-reflood was completed at 43 sec, approximately. The end

of reflood was predicted to be quite earlier than the measured tine as shown

in Table 2. This earlier end of reflood, i.e, earlier core quenching, than the

experiment was due to the overestimated coolant inventory, which was mainly

caused by underprediction of cold leg break flow.

The liquid level in the broken side downcomer were predicted to be different

from that in the intact side one due to the split nodalization of vessel downcoiner. In the early blowdown period up to 3 sec, the broken side liquid level

dropped more rapidly than the intact side one due to less flow resistance. Both

levels ceased to drop and increased a little slightly at the tine of the

transition from subcooled break flow to two-phase break flow. The increase of

level is caused that the break flow was reduced significantly at the transition

time, while the incoming flow was still maintained by the operation of the

intact loop pumps. During core rewetting period, downcomer liquid levels decreased again. The slope of the broken side liquid level was slower than

that in intact side one, which was due to upward water flow from the lower

plenum to the broken side downcomer. At the time of accumulator injection,

16 sec, both levels moved up again with some time delay in the broken side.

11
4.4 Fuel Thermal Response

Figs. 16, 17, 18, 19, 20 and 21 present comparisons of cladding temperatures

of hot fuel rods at 5, 16.5, 27.5, 39, 49.5 and 60 inch elevations from the

bottom of core, repectively. From these comparisons, the following features

were found,

1) For a lower part (5 in and 16.35 in), the predicted DND(departures from

nucleate boiling) times were later than the measured values during blowdown phase. And the calculated cladding temperature s during blowdown he atup period were appreciably lower-and core rewet was completed earlier than

the measured data.,

2) The predicted thermal response during ref load heatup period were also

later in timing and smaller in heatup amounts than the experimental data.

Consequently, core quenching tines were predicted as substantially earlier

than the experiment.

3) For a middle part(27.5 in and 39 in), the prediction shows earlier DNB's,

higher heat up's and earlier core quenchings than the experiment, and

the absences of blowdown rewets. The peak cladding temperature (PCT) was

predicted as 950 K at 27.5 inch elevation in blowdown phase, whch was

higher than the experiment, 891-K at 2 4 inch elevations.

4) For a higher part (49.5 in and 60 in), core was not heated up both in

blowdown and reflood phases.

To find out some reasons of such thermal responses that deviated from the experimental behaviors, the calculated fuel surface heat transfer coefficients

were presented as shown in Fig.22 for a volume 2 (16.5 in) and a volume 3 (27.

5 in). For a volume 3, heat transfer coefficient rapidly dropped as soon as

12
the experiment was initiated (transition from the saturated nucleate boiling to

the film boiling) and the filni boiling heat transfer mode was sustained until

20 sec, while for a volume 2, the saturated nucleate boiling remained for 4

or 5 sec, and then changed to the film boiling during a short period (rewet).

Fig.2.3 shows liquid fractions at volume 2 and volume 3. Both volumes had

experienced an almost similar transient in liquid fraction for the first 2 sec.

as shown in this figure, however a DNB was not predicted in volume 2 as shown

in Fig.17. As a result of poor prediction of DiNB, flow regimes at these two

volumes were different during the same period as shown in Fig.24. Therefore,

it can be stated that the deficiency of OHF correlation in the frozen RELAPS!

110D2 was also found in the LOCE L2-3 simulation in the condition of high flow'

rate ( the predicted mass flux into the core was about 1000 kg/mZ sec )

The increasing behavior of liquid fraction at volume 3 was almost the same

as that in volume 2 during 5 to 8 sec except some time delay, however no rewetting was -found at the volume 3. This indicates the severeness of rewet

criteria in the frozen RELAP5/MOD2 Cycle 36.04.

Some features found in reflood heat up calculation can be regarded as an over

prediction of coolant inventory as mentioned in the previous chapter. Total

amount of coolant inventory overestimated by the present calculation was 545

kg, approximately. This amount was not so small when compared to the primary

coolant system inventory 5646.8 kg at the steady state condition. This added

inventory can be considered to suppress the core heat up during reflood period.

13
5. Sensitivity Study

From the findings in the base case calculation, the severeness of the rewet

criteria in the frozen code was one of the most noticeable problems in the

point of the fuel cladding thermal response. In this study, to investigate the

sensitivity of rewet criteria, an updated code with PSI modification from the

RELAP5/110D2 Cycle 36.04 was used in the re-calculation with the same input as

in the base case calculation. The PSI modification (6) includes, three major

changes : interfacial friction formula, rewet criteria and heat transfer correlations in reflood phase. A whole list of the updates was presented in the

Appendix D. Especially in the rewet, three independent criteria was checked as

follows

1) (Tw +Tsat) <1250 K

2) Equilibrium quality less than 0.99

3) Mass flux less than -100 kg/sec m2

Figures 25, 26, 27 and 28 show comparisons of the calculated cladding

temperatures by the frozen Cycle 36.04 with those by PSI updated version at

16.5, 27.5, 39 and .49.5 inch elevation, respectively. The predicted thermal

responses at 5 and 60 inch elevation were not plotted since almost the same

result was obtained as base calculation. Even at 16.5 inch location (Fig.25),

a similar thermal response to the base case calculation was obtained except a

little higher heat up in blowdown phase. And both calculation still show

differences from the experimental cladding temperature.

At the middle elevations, 27.5 inches in Fig.26 and 39 inches in Fig.27, the

sensitivity calculation shows the blowdown rewet evidently, which were not

predicted in the base case calculation. As the result calculated by the PSIupdated version, the core heatups were a little higher than the base case calculation result. It was due to some modifications of heat transfer coefficients

14
in the subcooled or saturated transition film boiling regime included in the

PSI updates [6].

At 49 inch elevation, the sensitivity calculation result. shows a appreciable

blowdown heatup and a rewet, which was not found in the base case one. The

onset of CHF at this elevation was- currently understood 4s a deficiency of

Biasi's CHF correlation in the RELAP5/110D2. A comparison of void fraction at

the 5th volume in hot channel was presented in Fig. 29. In spite that the'void

fraction predicted by the PSI version was lower than that calculated by Cycle

36.,04 version until 1.5 sec approximately, as shown in Fig.29, a heatup was

found in the calculation by the PSI version.

From these comparisons, it is concluded that the deficiency of the Biasi's

CHF correlation was re-identified at high flow rate and that the modification

of rewet criteria using PSI updates can predict the rewet phenomena during

blowdown phase properly

15
6. Run Statistics

The main frame computer used in the present calculations was CDC 170-875

Series at XAERI, with NOS Version 2.6.1.

Fig.30 presents the plot of the required .-CPU time for the transient time in

.the base case calculation. And the time-step size are also plotted in Fig.31.

The user-specified maximum time step was. 0.05 sec up to 20 second. in. real time

and then reduced to 0.01 sec up to 100. second as recommended in reference(1J.

The -run statistics is summarized in Table 5 from the major edit and the grind

time can be calculated as follows.

Computer time, CPU 1795.36 --3.121 =1792.239 .(sec)

Number of time step, DT =.9635 - 76 =-9559

Number of volume, C =128

Transient real time, lIT .=100 (sec)

Grind time =CPU xlOOO/ C C* DT )=1.4647 CPU mn sec/vol/step

16
7. Conclusions

RELAP5/MOD2 Cycle 36.04 code was assessed using LOFT L2-3 LBLOCE data. A base

case calculation was carried out using the original version of the-code. And

one sensitivity calculation was conducted with an updated version by the PSI

modification. The calculated thermal-hydraulic behaviors were compared with

the experimental data to identify code capability. As a result of the present

calculations, the following conclusions are obtained

1) Using LOFT LOCE L2-3, a base case calculation and a sensitivity calculation

were successfully executed from the-point of view of specific objectives

and requirements of ICAP assessment activity.

2) The loop flow behaviors were faily well predicted by the frozen RELAP5/11D2

Cycle 36.04 code. The secondary side behavior and ECCS performance were

also well simulated by the-base case calculation. Hydraulic behavior such as

liquid levels in downcomer and core in the reactor vessel were resonably predicted. The thermal response of fuel rods was calculated, and the calculated

PCT was 950 K, a little higher than the measured PCT of 891 K.

3) From the base case calculation using the frozen RELAP5/110D2, the cold leg

break flow was underpredicted due to the deficiency of the critical flow

model in the transition phase from subcooled flow to two-phase flow. This

led a overprediction of coolant inventory. The early core heatup during the

blowdown phase was not well-predicted due to a deficiency of CHF correlation at high flow rate of the frozen code. The rewet phenomena was also

poorly predicted due to the severeness of the criteria.

4) As a result of the sensitivity calculation'using the updated rewet criteria

by PSI, blowdown quenching behavior was relatively well-predicted.

17
References

1. Ransom, V.H. and Wagner, R.J. RELAP5/IJOD2 Code Manuals,

NUREG/CR-4312, EGG-2396, EG&G Idaho Inc., Dec. 1985.

2. Prassinos, P.G., et al, Experimental Data Report for LOFT Power Ascension

Experiment L2-3, N1JREG/CR-0792, TREE-1326, July 1979.

3. Carbajo, 3.3, "A Study on the Rewetting Temperature,"

Nuclear Engineering and Design, Vol 84, pp 21-52, 1985.

4. Aksan, SN, "Investigation on Rapid Cladding Cooling and Quench During

the Blowdown Phase of a LBLOCA Using RELAP5/110D2,"

Presentation on the Fourth International Topical Meeting on Nuclear

Reactor Therinal-Hydraulics(NURETH-4), Karlsruhe, FRG, Oct. 1%98

5. Driskell W.E. et al, Sumanary of ICAP Assessment Results for RELAP5/110D2,

Draft of ICAP Annul Report for M99, INEL.-

6. Aksan, S.N., Analytis, G.Th.., and Lubbesmeyer, D.,

Switzerland's Code Assessment Activities in Support of the ICAP

the 16th Water Reactor Safety Meeting, Oct. 1988, Gaithersburg,.USA,

7. Reeder, P.L., LOFT System and Test Descriptions, NUREG/CR-0247, July 1978

8. Young Seok Bang, et al,

Assessment of RELAP5/110D2 Cycle 36.04 Using LOFT Large Break Experiment

L2-5, N1JREG/IA (to be published), KAERI, Korea, 1990.

9. Demmie, P.N., et al, Best Estimate Prediction for LOFT Nuclear Experiment

L2-3, EGG-LOFT-5869, EG&G, INEL, Nay 1982.

18
Table 1 Summary of comparison of the initial conditions

between the measured and the calculated in base case

Parameter Measured Calculated

-Primary Coolant System

Mass flow rate* , kgs 199.0 199.01

Hot leg pressure* , MPa 15.06 15.07

Cold leg temperature* ,K 560.7 560.39.

Hot leg temperature , K 592.9 592.75

-Reactor Vessel

Power level , MW 36.0 36.0

Maximum linear heat generation

rate(MLHGR), kW/m 39.4 39.8

-Pressurizer

Liquid temperature , K 615.3 613.8

Pressure , MPa 15.06 15.066

Liquid level* ,m 1.19 1.172.3

Water volume, m3 0.67 0.627

-Steam Generator sec.side -

Saturation temperature ,K - 482.1 487.88

Pressure , MPa 6.18 6.1

Mass flow rate , kg/s. 19.5 19.129

Level* , m 3.11 3.11

Note * : Setpoint in steady state controllers

19
Table 2 Summary of comparison of the sequence of events

between the measured and the calculated-in base case

Event lleasured,sec Calculated~siec

Experiment initiated 0. 0.

End of subcooled blowdown 0.05 *

Reactor scrammed * 0.103 0.103

First indication of DND 0.96 0.4

End of subcooled break flow (cold leg) 3.0 3.05

Maximum cladding temperature attained 4.95 5.0

Earliest corewide rewet 8.0 7:.8

HPSI initiated *14.0 14.0

Pressureizer emptied 14.0 14.0

Accumulator injection initiated 16.0 15.66

LPSI initiated'* 29.0 29.0

Lower plenum refilled 35.0 35.0

Saturated blowdown ended 40.0 *

Accumulator liquid flow ended 45.0 42.0

Core volume reflooded 55.0 43.0

Note *:specified by input , **:not predicted

20
Table 3. Uncertainties of Measurements

item type range uncertainty

Primary system pressure

Secondary system pressure

Coolant Temperature

Accumulator liquid level

Accumulator flow rate

HPSI flow rate

LPSI flow rate

Mass flow rate at

broken loop cold leg

broken loop hot leg

Cladding Temperature

primary Coolant Pump Speed

Reactor Power

M

M

M

N

N

N

M

C

C

M

C

Ii

0.1

0.1

311

0.0

0.0.

0.0 - 0.0

20.8 MPa

8.4 NPa

977.4 K

3 m

126.2 1/s

1.9 1/s

25.2 1/s

1533 K

4500 RPM

100 %

0. 22 NPa

0. 11 IlPa

5.1 K

0. 02 m

3.5-1/s

0.02 1/s

Not available

63.7 kg/s

23.7 kg/s

6.5 K

8.2 RPM

3.0 X

422 -

0.0 -

0.0 -

Note. M : Measured data,

C : Computed varibles from the measured data

21
Table 4. Summary of the important items in nodalization

items Description

Core

Number of flow channel

Channel area ratio (hot/total) Number of volume per channel

Number of crossflow junction between channels

Loss coefficients at crossf low jucntions

Number of heat structure component (hot:average)

Power ratio (hot/total)

Number of volume per heat structure

Gap. conductance model

Reflood optiofi Number of mesb poin in heat structure

Number of maximum fine mesh

Number of volume in core bypass component Core Bypass flow ratio

Downcomer

Number of flow channel

Area ratio (intact side channel/broken side channel) Number of volume per flow channel

Number of crossflow junctions for downcomer bypass Loss coefficients at crossflow junction

2

13.7 %

6

6

4.2

1:2

20.5 X

6

used

Pressure*

10

8

3

5 %

2

1/1

5

5

18.0 - 98.0 *

Note *:Pressure at core top less than 0.1 flPa;

**:Loss coefficients varies with elevation

22
Thble 5 . Run statistics data in base case

transient time CPU time Attempted Repeated Last Courant

(sec) (Sec) ADV ADV -DT DT

0 3.121 0 0 0.05 0

10 122.678 669 12 0.0125 0.01546

20 Z65.146 1469 12 0.0125 0.01202

25 352.17 1969 12 0.01 0.00958

30 446.903 2469 12 0.01 0.01097

35 542.424 2969 12 0.01 0.00916

40 645.349 3497 12 0.01 0.02857

45 750.017 4020 21 0.01 0.01576

50 845.089 4520 21 0.01 0.02828

55 940.003 5020 .21 0.01 0.02852

60 1035.32 5520 21 0.01 0.03126

65 1130.72 6028 25 0.01. 0.02552

70 1223.29 6528 25 0.01 0.03884

75 1316.72 7028 25 0.01 0.0450

80 1410.51 7528 25 0.01 0.01604

85 1504.71 8050 35 0.01 0.03274

90 1594.56 8550 35 0.01 0.04819

95 1693.06 9083 50 0.01 0.05249

100 1795.36 9635 76 0.01 0.04379

23
lnlaclt loop

Fig. 1 Fig.1 Axonometric configuration of LOFT L2-3 test
EJvaAtww

-N-* SoVflwbM

OFOS4ft PAPC"

JJUNt

STUN W!I4ATUR

ad~-W CyC" "HeaUr

REACTw VTM~ RLUfl~M StFPtRSSMf TAWC

N) Lfl

TMK

VffACT Lap

Fig. 2 Fig.2 Nodalization diagram for base case calculation of LOFT L2-3 test
LOFT L-2-3 Base Calculation

Core Power Didtribution

50

E 40

0

C

0

X

C

:3

30

20

10

0

0 0.2 0.4 0.6 0.6 1 1.2 1.4 1.6

Height from the bottom. m

Fig.3 Fig.3 Axial power distribution in base case calculation of L2-3 test
LOFT L2-3 Base Calculation

Mass flow In Brokeon lo"p cold leg

N

I

0

U

U

a

1100

700

800

500

400

300

200

1 00

-.1

0

-100

-200

-10 10 30

TIM6. Bee

Comparison of mass flow rate at broken loop cold leg

between the base case calculation and the experiment Fig.4
LOFT L-2-3 Base Calculation

Maas flow In Smroin loop hot Wa

200 - _____

180 - RELAP5 Base C~alculat

160 + Expedniont

140

o120

100

*80 60

00~

40

20

0-

-20

-40

-60-

-10 10 30

Time. moo

Fig.5 Comparison of mass flow rate at brokeni loop hot leg

between the base case calculation and the experiment
LOFT 1-2-3 Base Calculation

Mass flow In' Intact looD cold lea

500

400 -RELAP5 lfase Cakmklr

300

0

0

-.200

o 100

- 100003

TIMe, see

Fig.6 Comparison of mass flow-.rate at intact loop cold leg between the base case calculation and the experiment
LOFT L2-3 Base CacuJcuat1oi

600

400

800

zoo

100

C

S

I 0

CI.. -100

-*00

-800

--400

-600

0 .8 4 6 a 10

Time. "a

Comparison of net mass flow rate into the core

between the base case calculation and the experiment

Fig.7
LOFT 1-2-3 Base Calculation

a

0. ~

U

'-0

ii, 0.

8.4

8.3

8.2

6.1

a

5.9

5.a

5.7

5.6

5.5

5.4

5.3

5.2

CA~

-20 020 40 Go W0

lime, eec

1W0

Fig.8 Comparison of steam dome pressure at S/G secondary side

between the base case calculation and the experiment
LOFT 1-2-3 Base Calculation

Accumulator Moa" Flow Rate

e

N

CR

Op

+12

0

0

U

0

90

s0

70

60

s0

40

30

20

- 'RELAP5 Calculot~on

9 Experiment Fr-P120-36-1

10

0

-10 -*1-.

0 20 40 60 s0 100

Ilo lowrat

Comparison of accumulator injection flwrt

between the base case calculation and the experiment

Fig. 9
LOFT 1-2-3 Base Calculation

Accumulator Liquid Level

2.1

2

1.9

1.8

1.7

1.6

E

(A~

'1.4

1.3

1.2

1.1

1

0.9

0 20 40 80 s0 100

'rime, Beec

Fig. 10 Comparison of accumulator liquid level

between the base case calculation and the experiment
L-2-3 Base calculation

HPIS flow rate

0

rJ

1.8

1.7

1.6

1.5

1.4

1.3

1.2

1.1I

0.9

0.8

0.7

0.6

0.5

0.4

0.3

0.2

0.10

E

o3 Experiment - Calculation

Lv77Z7

-Y

(AJ .a:b

.9 -. 

-

-

80 

100

a 20 40 60

Time after rupture, sec

80I

I

100

Fig. 11 Comparison of UPSI flow rate

between the base case calculation and the experiment
L-2-3 Base calculation

LPIS flow rate

9, N

0'*1

0

7

6

5

4

3

2

0

W,

0 20 40 60 80 100

Time after rupture. sec

Fig. 12 Comparison of LPSI flow rate

between the base case calculation and the experiment
LOFT 1-2-3 Base Calculation

Primary System Pressure

a

a.

16

15

14

13

12;

11

10

9

a

7

6

5

4

3

2

1

0

wa~b

0 20 40 60 80

1ime. e

Fig. 13 Comparison of primary system pressure between the base case calculation and the experiment

100!
LOFT L-2-3 Base Calculation

Lower Plenum Coolant Temperature

L

2

C

0.

E

S

I700

650

800,

550

500

450

400

350

300

0 20 40 80 80 100

'rime. Bec

Fig. 14 Comparison Of coolant temperature in lower plenum between the base case calculation andI the experiment
LOFT 1-2-3 Base Calculation

Collapsed Water Level, In Reactor Vessel

E

00

a

7

6

5

4

3

2

1

0

0 20 40 60

Time. sWc

Fig. 15 Collapsed liquid levels calculated in the base case calculation

for the broken side-downcoumer. intact side downcomer, hot core

channel and average core channel of the reactor vessel
LOFT L-2-3 Base Calculation

Claddtng Temperature at 5 Inches

WA

t~o

.3

0.

E

g0o

800

700,

BO00

500

400

300

0 20 40 60 80 100

Time. seec

Fig. 16 Comparison of cladding temperature at 5 inches of hot fuel

between the base case calculation and the experiment
. . " , I , 0 ,i

LOFT L-2-3 Cladding Temperature

Hot Fuel 16.5 Inch..

go0

800

2

3

41

2

V

700

600

4:

500

400

300

0 20 40 . 60 80

limo. Sac

Fig.17 Comparison of cladding temperature at 16.5 inches of hot fuel

between the base case calculation and the experiment

100
LOFT L2-3 Cladding Temperature

Hot Fuel 27.5 Inch

6

0

U

0.9

0.8

0.7

0.6

0.5

0.4

0.3

0 20 40 60 80 100

Time. see

Fig. 18 Comparison of cladding temperature at 27.5 inches of hot fuel

between the base case calculation and the experiment
LOFT 1-2-3 Base Calculation

Cladding Temperature at 39 Inches

900

800

4..2

0

0.

E

S

1-*

C

0

0

700

600

500

400

300

0 20 40 80 s0 100

Time. sac

Fig. 19 Comparison of cladding temperature at

between the base case calculation and

39 inches of hot fuel

the experiment
LOFT L-2-3 Cladding Temperature

Hot Fuel 49 Inches

900

Boo

6

L

4 J

I,

L

a.

E

0

I0'

C

0

700

600

CA)

500

400

300 -T0 20 40 60 80 100

lime, sec

Fig.20 Comparison of cladding temperature at 49.5 inches of hot fuel

between the base case calculation and the experiment
LOFT 1-2--3 Base Calculation

Cladding Temperature at 60.5 Inches

900

800

y

4 J

'a

0.

U

700

600

500

400

300

0 20 40 60 80 100

Time. sec

Fig. 21 Comparison of cladding temperature at 60 inches of hot fuel

between the base case calculation and the experiment
LOFT 1-2-3 Base Calculation

Hot Fuel Surface Heat Transfer Cool.

4U,

C%4

E

00

5 .D

Go

20

19

18

17

16

15

14

13

12

11

10

9

8

7

6

5

4

3

2

1

0

0 20 40 80 100

Time. see

Fig.22 Wall heat transfer coefficients calculated in the base case

calculation at volume 2 and 3 of hot fuel
L-2-3 Base Calculation

Uquld fractions of core

41-

C

0~

1

0.9

0.8

0.7

0.8

0.5

0.4

0.3

0.2

0.1

0

0 2 4 6 8 10 12 14 16 18 20

Time. see

Fig. 23 Liquid fractions calculated in the base case calculation

at volume 2 and 3 of hot fuel
LOFT L2-3 Base Calculation

Flow Regime In Hot Core Vol 2. 3

12-

11-

10-

4 : Bubbly flow

5 : Slug flow

6 : Annular Mist flow

7 : Inverted Annular flow

8 :Inverted Slug flow

9 : Dispersed flow

- : Vol 2. + : Vol 3

9 -

E

z

E0

0

cc

8

5-

4-

3-

2-

-I 

I I

PIL~J1

20 40 60 soI

I

0 100

Time. sec

Fig.Z4 Flow regimes predicted in the base case calculation

at volume 2 and 3 cf hot core channel
LOFT L-2-3 Cladding Temperature

Hot Fuel 16.5 Inches

900

B00

0

0.

E

'I

I0a

C

0

0

0

C)

700

600

500

400

300

0 20 40 60 80 100

lime. sac

Fig.25 Comparison of cladding temperature 4A 16i.5 iniches of hot fuel

between the base case calculation andu the sensitivity calculation
LOFT 1-2-3 Cladding Temperature

Hot Fuel 27.5 Inch

0 r

E .0

0

to

0.9

0.8

0.7

0.8,

0.5

0.4

0.3

I'D

0 20 40 80 s0 100

Time, sac

Fig.26 Comparison of cladding temperature at 27.5 iniches of hot fuel

between the base case calculation and the, sensitivity calculation
LOFT 1-2-3 Cladding Temperature

H-ot Fuel 39 Inches

L"

0)

90

co

'0.9

0.8

0.7

0.6

0.5

0.4

0.3

0 20 40 60 *80 100

Time, sac

Fig.27 Comparison of cladding temperature at 39 inches of hot fuel

between the base case calculation and the sensitivity calculation
LOFT L2-3 Cladd~ing Temperature

Hot Fuel 49 Inches

g00

800

L,

L

0

0.

E

0

I0~

C

*0

0

700

600

500

400

300

0 20 40 60 80 100

Time, sec

Fig.28 Comparison of cladding temperature at 49.5 inches of hot fuel

between the base case calculation and the sensitivity calculation
LOFT L2 -3 Void Fraction Comparison

Void fraction at volume 5

0

1

0.9

0.8

0.7

0.6

0.5

0.4

0.3

0.2

0.1

0

(31 r~3

0 2 4 6 8 10 12 14 16 1e 20

Time, sac

Fig. 29 Comparison of void fraction at volume 5 of hot core channel

between the base case calculation and the sensitivity calculation
LOFT L-2-3 Base Calculation

CPU time

0

Em

0

01

w

1.8

1.7

1.6

1.5

1.4

1.3

1.2

1.1

1

0.9

0.6

0.7

0.8

0.5

0.4

0.3

0.2

0.1

0

0 20 40 60 s0

Time. MMc

Fig.30 The required CPU time versus the advanced time

in the base case calculation

100
LOFT 1-2-3 Base Calculation

Time Stop Size

0.07

T ime Stop

0.06 - A Crount Time Stop UmIt

User specified Max. step

0.05 n - ---

U 0.04

E ~0.03I

0.02

0.01

0-

0 20 40 60 80 100

Time. see

Fig.31 Time step size of base case calculation
Appendix A. Update List for MEAP5IIOD2 Cycle 36.04

APPENDIX A Update list for RELAP5/110D2 Cycle 36.04

/JOB

R11364B,T200.

IUSER

ATTACH,0LDPLgREL364S.

PURGE, RE364BS/NA.

PURGE ,RE364BX/NA.

PURGE, RE364BL/NA.

*IM1PORTANT H! * THE UPDATE DIRECTIVE *

* SHOULD HAVE *COMPILE DEFINE * AS THE FIRST DIERECTIVE

UPDATE,N=RE364BS.

UPDAE, P=RE364BS, Q, C=R5SEG.

REPLACE,R5SEG.

RETURK,OLDPL.

*DEFINE, RE364BS.

RETURN,RE364BS.

ATTACH, ENVRLX=ENVR41X.

LIBRARY,ENVRLX.

SELECTA,CONPILE,COMP.

LIBRARY.

RETURN,ENVRLX.

REWIND,COMP.

FTN5, I=COMP,DO,ET,STATIC ,OPT=2,ROUND,LO=ZVAIR/S,L=0.

RETURNICOIIP.

REWIND,LGO.

ATTACH, RELAP5I=REL364L.

GTR,RELAP5I ,ADD.REL/*

*DEFINE, RELAP5O=RE364BL.

LIBEDIT,P=RELAP5O, I=O,B=ADD,LO=F,UC.

LIBEDIT,P-RELAP50,B=LGOI=-O,LO=F,UC.

RETURN, NULL, LGO, RELAP51.

RETURN,RLP5Fl,RLP5F2.

ATTACH,ENVRL=ENVR4IL.

FILE,RSTIN ,RT=S,SBF=NO,USE,F0=SQ.

RFL,EC=200.

DEFINE,RE364BX.

SEGLOAD, I=R5SEG ,B=RE364BX.

LDSET, LIB=RELAP5O/ENVRL.

LDSET,PRESETA=NGIHDEF ,ERR=NONE,1IAP=SB.

LDSET,STAT=RSTIN.

LIBLOAD,ENVRL,$HDR=$.

LIBLOADFTN5LIB,$FERCAP.$,$RPVCAP.$,$FTNRP2. $,$Q2NTRY.$.

NOGO.

PERIIIT,RE364BXj(A41202.

RETURN,RELAP5OIIENVRL,COMPILE.

SKIPJWK.

EXIT.

ENDIF,KKK.

DAYFILE,KMRRAY.

REPLACE, IXRRAY.

/EOR

*COMPILE DEFINE

*IDl CBD3604

*D D11K3601.484

A-1
*D PLOTMD.24

901 FORMAT ('OPLOTFL SCRACH FILE GENERATED.') *COMPILE DEFINE, SEGDIR

*COMPILE RELAP5

*D RJW3603.23

DATAnPITLE/"RELAP5/2/3" ,"6. 04-NSC" ,"REACTOR LO"1,1"55 OF COOL",

~/ ENDIF

*ID KWU01 ALREADY IMPLEMENTED IN RELAP5OLDPL36O4C,

WHICH IS USED AS BASIS

*/ CORRECTIONS OF INDEX IN SUBROUTINE RACCUII

*I RACCU1I.618

IELV=I

*1 *B DMX3602.581

*/ I=IELV

*COMPILE DEFINE, SEGDIR ,RACCUM

*ID KWU01

*I RACCUN.618

IELV=I

*B DMK3602.581

I=IELV

*/ END OF KWUl-UPDATES TO CYCLE 3604

*COMPILE DEFINE ,SEGDIR

*IDENT SKI01

THESE UPDATES ARE RECOMMENDED BY SKI TO BE

IMPLEME NTE D IN RELAP5/MOD2-36. 04

SOURCE: LETTER FROM STUDSVII( (MR.SANDERVAG)

*/TO I(WU (MR.GRUBER)

1987-06-25

*/ COMPILE RELAP5

*COMPILE IHTCMP

FIX AN INDEXING ERROR IN IHTCIP

ERROR CAUSED ROD PLENUM VOLUME FOR GAP-GAS PRESSURE CALCULATION

TO BE INCORRECT. FOUND AND FIXED BY D.CARAHER 20MAY87

FIX ONLY CDC-VERSION CODING

*D IHTCMP.1041

L=( .NOT.MASK(43).AND.IHTPTR(J))+FILNDX(8)

*1 UPDATE ROUTINE IRFLHT TO ALLOW REFLOOD TO WORK

*/ HEAT STRUCTURE FILE GETS CHANGED ON RESTART (FOR

EXAMPLE BY DELETING OR ALTERING SOME STRUCTURES)

*/NOTE.. HEAT STRS ASSOCIATED WITH REFLOOD CANNOT BE ALTERED

*/ ON RESTART AS IRFLHT IS NOW PROGRAMMED

*COMPILE IRFLHT

*I IRFLHT.330

C UPDATE THE GEOMETRY POINTER IN IGLRFL BITS 44-60 IN CASE THE

C HEAT STRUCTURE FILE CHANGED ON RESTART.

.J=(.NGT.MASIQ43).AND.IH) + lIHT

J=(.NOT.MASK (43).AND.IHTPTRG1)) + lIHT

NCOLS=.NOT.MASK(43) .AND. INXGOM(J)

IGLRFL(I)=(MASK(43).AND.IGLRFL(I)).OR.NCOLS

*/ END OF UPDATES SKI01

IEOR

*COMPILE SEGDIR

A-2
Appendix B. A Base Case Input Deck for a Steady State Calculation

/JOBI

L23TRA2 ,T4000.

/USER

ATrACH,STH2XT,RE364BX.

FILE, RSTPLT, SgF=NO.

DEFINE ,RSTPLT=L23RR.

RFL,CM=37OOOO,EC=2OO.

REDUCE( - RE364BX, ,*PL=5000(0.

/EOR

=LOFT L2-3 POST TEST ANALYSIS

* L2-3 INITIAL CONDITIONS

*POWER = 36.0 M1W

*PCS FLOW z 199.0 KG/S

*TCOLD = 560.7 K

*PCS PRESSURE = 15.06 MPA *PZR LEVEL = 1.19 M (45 IN)

*BASE CASE CALCULATION

*TWO CORE FLOW CHANNEL MODELLING IMPLEMENTATIONN

*CORE : HO CHANNEL(231), AVERAGE CHANNEL(230) * HOT FUEL RODS(12311), AVERAGE FUEL RODS(12301) * ~INTERIIIDIATE FUEL RODS( 12302)

0000100 NEW STDY-ST

0000101 RUN

0000105 5.0 10.0 * TIME STEP CONTROL CARDS *REQUIRED

*END TIME MIN DT MAXPDT OPTN MNR MJR RST

0000201 900.0 1.0-6 1.0 3 1 100 450

* MINOR EDIT VARIABLES

*STEADY STATE PLOT'REQUESTS

000030----1------ 01------1-----1-----1-----1---

0000301 P 530010000 * PRIONARY PRESSURE

0000302 PF 2530010000 * SECOARYP RESSUR

0000303 TEMPF 1850010000 * TE-UPC-001

0000305 TEMPF 515010000 * SECONDARY COOLANT TEMPERATURE

0000306 MFLOWJ 540000000 * FT-P004-012 STEM FLOW

0000307 MFLOWJ 985000000 * LETDOWN SINK FLOW

0000308 MFLOWJ 995000000 * CHAGING SOURCE FLOW

0000309 CNTEL VAR 1 * LT-P004-042 S/6 LEVEL

0000310 CNTRL VAR 2 * LT-PI39-007 PZR LEVEL

0000311 MFLOWJ 556000000 * FT-PO04-72-2 FEEDWATER FLOW

0000312 CNTRL VAR 910 . * TCONTROL

0000313 NFLOWJ 100010000 * FT-P139-27-1 INT.L .HOT L. FLOW

0000314 P 420010000 * PZR PRESSURE PE-PC-005

0000315 VOIDG 500010000 * SEPARATOR VOID

0000316 TEMPF 100010000 *TE-PC-002 ILHL

0000317 TEMPE 114010000 *TE-SG-001 S/G INLET

0000318 TEMP! 116010000 *TE-SG-002 S/G OUTLET

0000319 TENPF 300010000 *TE-BL-002 BLHL

0000320 TENPF 335010000 *TE-BL-001 BLCL

B-1
0000321 TEMIPF 702010000 *TE-ZST-002 DC STALK 2

0000322 TEMPF 215010000 * TE-5LP-0O1 LOWER PLENUM

*CLADDING TEMIPERATUJRES

*0000(321 HTTEMP .001100210*

*0000322 HTTEMP 001100310*

*0000323 HTTEMIP 002100210*

*00J00324 HTTEMP 002100310*

*0000325 HTTEMP 002100410*

*FUEL CENTERLINE TEMPERATURES

*0000326 IfflEMP 002100201*

*0000327 H~TEMP 002100301*

*000328 HITEMP 002100401*

* TRIPS

* 501-504 TEST SPECIFIC TRIPS

*------------1 -------- 1 -------- 1 ------ 1--I------- 1--------1---

*0000501 TIME 0 GE NULL 0 0.0 L * LOGE LZ-3 INITIATION

*000050)2 TIME 0 GE NULL 0 0.103 L *REACTOR SCRAI'

*0000503 TIME 0 GE NULL 0 14.0 N * IWIS INITIATION

*0000504 TIME 0 GE NULL 0 29.0 N * LPIS INITIATION

* ------------1---- ---- 1 -------- 1 -------- 1 ---- --- -- -1

* REPLACE TRIPS RELEVANT TO STEADY CALCULATION

*----- ---- 1----1------1-------- 1-------- 1---- --- 1-------- 1---

0000501 TIME 0 GE NULL 0 1.0+6 L

0000502 TIME 0 GE NULL 0 1.0+6 L

0000503 TIME 0 GE NULL 0 1.0+6 L

0000504 TIME 0 GE NULL 0 1.0+6 N

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

* CALCULATIONALLY REQUIRED TRIPS

*----- ---- I----1------1-------- 1-------- 1-------- 1-------- 1----

0000530 CNTRLVAR 21LE NULL 0 0.381 L * PZR LOW PRES. ALARM

0000555 P 016010000 LE NULL 0 1.0+6 L *REFLOOD INITIATION

* PUMP TMDP SPEED TABLE TRIP FOR STEADY STEADY CONTROLLER ONLY

0000510 TIME 0 GE NULL 0 -1.0 L

* LT 681 ECC CHECK VALVE CARD 6000301

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1--------1I----

0000577 MFLOWJ 600000000 GE NULL 0 0.0 N

0000578 P 605010000 GT P 185010000 0. N

0000681 577 AND 578 N

I T 682 ACCUMULATOR VALVE CARD 6100301

0000579 TIME 0 GE NULL 0 1.0+9 L

0000682 579 AND 579 L

* ------------1--------1 -------- 1 -------- 1 -------- 1 -- --I--

* T 685-686 STEAM VALVE CARD 5400301

*OPEN TRIP

0000589 P 530010000 OT NULL 0 7.1125+6 N

0000590 P 530010000 LT NULL 0 6.9747+6 N

0000670 685 OR 589 N

B-2
Q00071 -590 AND

0000685 671 AND

* CLOSE TRIP

000591 P 530010000

0000592 P 530010000

0000672 686 OR

000073 -591 AND

000674 -685 AND

000086 673 AND

*-- --- ---- 1----1------1-------

* LT 695 PCP 1 TRIP

0000695 510 OR

i ---- ------1--------1 ---- ---

Lk T 696 PCP 1 VELOCITY TABI

0000696 510 AND

*LT 697 PCP 2TRIP

0000697 510 OR

*- -l -- - 1------- - *-LT 698 PUP 2 VELOCITY TAB!

0000698 510 AND

*----- ---- 1----1---- 1--1------

-686 N

670 N

GT NULL

LT NULL

592

672

699

674

CARD

N

N

N

N

0

0

6.5613+6 N

6.4924+6 N

1350301

510 N

.1---

zE CARD 1356100

510 N

*1---~-

CARD 1650301

510 N

-1----

~E CARD 1656100

510 N

I-1--- ----1 --------1 --------1 ----

* LT 699 HSCV CLOSE TRIP BY SCRAM

0000699 502 OR 502 L

*INTACT LOOP

*REACTOR VESSEL NOZZLE - INTACT LOOP HOT LEG

1000000 "RVN ILHL BRANCH

1000001 2 0

1000101 0.0 1.58878 0.102752 0.0 0.0 0.0

1000102 4.OE-5 0.0 00

1000200 0 15009300. 1410030. 2458100. .00000000

1001101 252010000 100000000 0.0634 .0.1 0.1 0002

1002101 100010000 105000000 0.0 0.1 0.1 0000

1001201 4.6275000 4.6275000 0.0

1002201 4.6243000 4.6243000 0.0

* ------------1--------1 -------- 1 ------ 1--I------- 1--------1----

*PRESSURIZER CONNECTION TEE REACTOR VESSEL SIDE

1050000 "PZR T RVS "BRANCH

1050001 1 0

1050101 0.0634444 1.0531192 0.0 0.0 0.0 0.0

1050102 4.OE-5 0.0 00

1050200 0 15007600. 1410030. 2459730. .00000000

1051101 105010000 107000000 0.0 0.12 0.12 0000

1051201 4.8409000 4.8409000 0.0

* -------- 1---------11------ 1--- ---- -- --1----1------1--------1I----

*PRESSURIZER CONNECTION TEE

1070000 "PZR T BRANCH

1070001 1 0

1070101 0.0620253 0.2810215 0.0 0.0 0.0 0.0

1070102 4.OE-5 0.0 00

1070200 0 15006000. 1328625. 2459750. .00000000

1071101 107010000 110000000 0.0 0.135 0.135 0000

1071201 4.98 4.98 0.0

B-3
*PRESSURIZER CONNECTION TEE STEA1I GENERATOR SIDE

1100000 "PZR TSGS" BRANCH

1100001 1 0

1100101 0.0606063 0.9207292 0.0 0.0. 0.0 0.10

1100102 4.OE-5 0.0 00

1100200 0 15005300. 1410030. 2459800. .00000000

1101101 110010000 112000000 0.0 0.15 0.15 0000

1101201 5.1146000 5.1146000 0.0

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1-------- 1----

*HOT LEG PIPING

1120000 "HOT LEG PP" PIPE

1120001 a

1120101 0.0 2

1120201 0.0 1

1120301 1.38893 1

1120302 0.707687 2

1120401 0.0796973 1

1120402 0.0579614 2

1120501 0.0 2

1120601 0.0 1

1120602 90.0 2

1120701 0.0 1

1120702 0.246447 2

1120801 4.OE-5 0.0 2

1120901 -0.20 0.20 1

1121001 00 2

1121101 0000 1

1121201 0 1502900. 1410030. 2459870. .00000000 0.0 01

1121202 0 15005500. 1410030. 2459770. .00000000 0.0 02

1121300 0

1121301 5.1146000 5.1146000 0.0 01

*SG INLET PLENUMI

1140000 "SG IN PLNM" BRANCH

1140001 2 0

1146101 0.0 0.629795 0.33532 0.0 90.0 0.512756.

1140102 43E-5 0.0102 00

1146200 0 14987200. 1410020. 2460000. .00000000

1141101 112010000 114000000 0.0512 0.0 10.0 0100'

1142101 114010000 115000000 0.0 0.0 0.0 0100

1141201 3. 5832000 3.5832000 0.0

1142201 1.9414000 1.9414000 0.0

*------------1 -------- 1 ----------- 1-----1--~------1--

*SG U-TUBES

1150000 "1SO TUBES 11 PIPE

1150001 8

1150101 0.0 8

1150201 0.151171 7

1150301 0.902 1

1150302 0.6096 3

1150303 0.462908 5

1150304 0.6096 7

1150305 0.902 8

1150401 0. 136356 1

1150402 0' 0921538 3

1150403 0.0699783 5

B-4
1150404 0.0921538 7

1150405 0.136356 8

1150501 0.0 8

1150601 90.0 4

1150602 -90.0 8

1150701 0.902 1

1150702 0.6096 3

1150703 0.299572 4

1150704 -0.299572 5

1150705 -0.6096 7

1150706 -0.902 8

1150801 1.27-7 0.01022 8

1150901 0.0 0.0 7

1151001 00 8

1151101 0000 7

1151201 0 14979600. 1367230. 24600

1151202 0 14972800. 1333400. 24600

1151203 0 14967300. 1306120. 24600

1151204 0 14962900. 1288520. 24600

1151205 0 14962000. 1273520. 24600

1151206 0 14964300. 1257470. 24600

1151207 0 14967600. 1244800. 24600

1151208 0 14971800. 1233820. 24600

1151300 0

1151301 1.8921000 1.8921000 0.0 01

1.151302 1.8565000 1.8565000 0.0 02

1151303 1.8299000 1.8299000 0.0 03

1151304 -1.8134000 1.8134000 0.0 04

1151305 1.7997000 1.7997000 0.0 05

1151306 1.7856000 1.7856000 0.0 06

1151307 1.7746000 1.7746000 0.0 07

*----- ---- 1----1------1-------- 1-------- 1---- *SG OUTLET PLENUMN

1160000 "SG OUT PLN" BRANCH

1160001 2 0

10.0

20.0

30.0

40.0

50.0

40.0

30.0

20.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

01

02

03

04

05

06

07

08

1160101 -90.0 -0.512756

1160102

1160200

1161101

1162101

1161201

1162201

0.0 0.629795

4.E-5 0.0102

0 14976400.

115010000 116000000

116010000 118000000

1.7656000 1.7656000

3.2740000 3.2740000

0.33532

00

1233810.

0.0

0. 0512

0.0

0.0

0.0

2460100.

0.0

0.0

.00000000

0.0

0.0

0100

0100

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUMIP SUCTION PIPING

1180000 "PNP SUC PP", PIPE

1180001 3

1180101 0.0 3

1180201 0.0 2

1180301 0.546638 1

1180302 0.688596 2

1180303 0.558577 3

1180401 0.0445625 1

1180402 0.0445137 2

1180403 0.0354278 3

1180501 0.0 3

1180601 -90.0 3

1180701 -0.498052 1

1180702 -0.688596 2

1.180703 -0.355604 3

B- 5
1180801 4.E-5 0.0 3

1180901 0.083 0.083 1

1180902 0.104 0.104 2

1181001 00 3

1181-101 0000 2

1181201 0 14965800. 1233810. 2460030.0 .00000000 0.0 01

1181202 0 14967700. 1233810. 2460033.0 .00000000 0.0 02

1181203 0 14970500. 1233810. 2460035.0 .00000000 0.0 03

1181300 0

1181301 4.1288000 4.1288000 0.0 01.

1181302 4.2081000 4.2081000 0.0 02

* ------------1--------1 -------- 1 -------- 1---- -- 1--I-------- I--

*PUMP SUCTION TEE

1200000 P112M SCT T 1" BRANCH

1200001 3 0

1200101 0.0 0.759614 0.0487901 0.0 0.0 0.0

1200102 4.OE-5 0.0 00

1200200 0 14974000. 1233810. 2460020. .00000000

1201101 118010000 120000000 0.063427 0.0 0.0 0000

1202101 120010000 125000000 0.063427 1.075 1.25 0000

1203101 120010000 155000000 0.063427 1.075 1.25 0000

1201201 4.2080000 4.2080000 0.0

1202201 1.9967000 1.9967000 0.0

1203201 2.2113000 2.2113000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUMPi SUCTION TEE OUTLET

1250000 "PMP1 SOT TV BRANCH

1250001 1 0

1250101 0.0 1.00308 0.0640548 0.0 90.0 0.520704

1250102 4.OE-5 0.0 00

1250200 0 14974500. 1233810. 2460022. .00000000

1251101 125010000 130000000 0.0 0.13 0.13 0000

1251201 3.2631000 3.2631000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUMP 1 INLET

1300000 "IPMP1 INLET" SNGL VOL

1300101 0.0 0.457201 0.0177444 0.0 90.0 0.457201

1300102 4.OE-5 0.0 00

1300200 0 14968300. 1233810. 2460030. .00000000

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PRIMARY COOLANT PUMP 1

1350000 "lPCPUMP 1 " PUMPW

1350101 0.0 0.4572 0.0991 0.0 90.0 0.317900

1350102 0

1350108 130010000 0.0 0.017 0.017 0000

1350109 140000000 0.0 0.05 0.05 0000

1350200 0 15010900. 123320. 2459500. .00000000

1350201 0 3.2631000 3.2631000 0.0

1350202 0 3.4591000 3.4591000 0.0

1350301 0 0 0 -1 -1 0 0

1350302 369.00000 .35501355 .31550000 96.000000 500.60000 1.4310000

1350303 613.60000 .00000000 207.43300 .04440000 19.598700 .00000000

1350310 0.0 0.0 0.0

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1-------- 1----

*PUMP 1 OUTLET PUMPW SIDE

1400000 "21121 OUT P2" SNGL VOL

B-6
1400101 0.0 0.502185 0.0183849 0.0 0.0 0.0

1400102 4.OE-5 -0.0 00

1400200 0 15046700. 1233820. 2459000. .00000000

*PUMPi OUTLET PIPE TEE SIDE

1450000 "PNP1 OUT T" BRANCH

1450001 2 0

1450101 0.0 1.40843 0.0633861 0.0 0.0 0.0

1450102 4.OE-5 0.0 00

1450200 0 15048400. 1233820. 2458800. .00000000

1451101 140010000 145000000 0.0 0.0 0.0 0000

1452101 145010000 150000000 0.0 0.57456 0.050347 0000

1451201 3.4589000 3.4589000 0.0

1452201 2.8137000 2.8137000 0.0

* ------------1------1--I------- 1--------1 --------1 --------1----

*PUMP' OUTLET TEE

1500000 "P111' OUT T "BRANCH

1500001 1 0

1500101 0.0 0.496511 0.0316011 0.0 0.0 0.0

1500102 4.OE-5 0.0 00

1500200 0 15042300. 1233820. 2458700. .00000000

1501101 150010000 175000000 0.063427 0.0 0.0 0000

1501201 4.2075000 4.2075000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUMP 2 SUCTION TEE OUTLET

1550000 "PMP2 SCI T" BRANCH

1550001 1 0

1550101 0.0 1.00308 0.0640548 0.0 90.0 0.520704

1550102 4.OE-5 0.0 00

1550200 0 14973600. 1233810. 2460020. .00000000

1551101 155010000 160000000 0.0 0.13 0.13 0000

1551201 3.6137000 3.6137000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUNTP 2 INLET PIPE

1600000 "PMP2 INLET" SNGL VOL

1600101 0.0 0.457201 0.0177444 0.0 90.0 0.457201

1600102 4.OE-5 0.0 00

1600200 0 14966800. 1233810. 2460030. .00000000

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PRIMARY COOLANT PUMP 2

1650000 "PCPUMP2 "PUMP

1650101 0.0 0.514 0.0991 0.0 90.0 0.317900

1650102 0

1650108 160010000 0.0 0.017 0.017 0000

1650109 170000000 0.0 0.1 0.1 0000

1650200 0 15010900. 1233820. 2459500. .00000000

1650201 0 3.6138000 3.6138000 0.0

1650202 0 3.7364000 3.7364000 0.0

1650301 135 135 135 -1 -1 0 0

1650302 369.00000 .35501355 .31550000 96.000000 500.60000 1.4310000

1650303 613.60000 .00000000 207.43300 .04440000 19.598700 .00000000

1650310 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PUMP 2 OUTLET

1700000 "PNP2 OUT T" BRANCH

B-7
1700001 1 0

1700101 0.0 0.514071 0.0192958 0.0 0.0 0.0

1700102 4.OE-5 0.0 00

1700200 0 15046300. 1233820. 2459000. .00000000

1701101 170010000 150000000 0.036611 0.3847 0.6316 0000

1701201 3.8305000 3.8305000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*INTACT LOOP COLD LEG PIPE

1750000 "ILCL PIPE "PIPE

1750001 2

1750101 0.0 2

1750201 0.0 1

1750301 0.558577 1

1750302 0.613244 2

1750401 0.035428 1

1750402 0.038895 2

1750501 0.0 2

1750601 0.0 2

1750701 0.0 2

1750801 4.OE-5 0.0 2

1750901 0.0 0.0 1

1751001 00 2

1751101 0000 1

1751201 0 15043000. 1233820. 2459500.0 .00000000 0.0 01

1751202 0 15042800. 1233820. 2459500.0 .00000000 0.0 02

1751300 0

1751301 4.2076000 4.2076000 0.0 01

* ------------1--------1--- -1 -------- 1 -------- 1 -------- 1----

*ECC CONNECTION TEE

1800000 "ECC T "BRANCH

1800001 1 0

1800101 0.0 1.15189 0.0730598 0.0 0.0 0.0

1800102 4.OE-5 0.0 00

1800200 0 15042500. 1233830. 2459500. .00000000

1801101 175010000 180000000 0.0 0.0 0.0 0000

1801201 4.2076000 4.2076000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*REACTOR VESSEL NOZZLE - INTACT LOOP COLD LEG

1850000 "RVN ILCL "BRANCH

1850001 2 0

1850101 0.0 1.00965 0.0644920 0.0 0.0 0.0

1850102 4.OE-5 0.0 00

1850200 0 - 15041900. 123383. Z459550. .00000000

1851101 185010000 730000000 0.0634 2.8 2.8 0001

1852101 180010000 185000000 0.0 0.0 0.0 0000

1851201 4.2093000 4.2093000 0.0

1852201 4.2076000 4.2076000 0.0

REA~CTOR VESSEL

*INLET ANNULUS UPPER VOLUME INTACT SIDE

7000000 "INANUPRINT" ANNULUS

7000001 1

7000101 0.1308530 1

7000301 0.1876129 1

B-8
7000401 0.0 1

7000501 0.0 1

7000501 90.0 1

7000801 3.81-6 0.172 1

7001001 00 1

7001201 0 15028400. 12,33830. 2459250. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*JUNCTION -UPPER TO LOWER INLET ANNULUS INTACT SIDE

7010000 "INANMUINT "SNGLJUN

7010101 730000000 700000000 0.129467 0.0000 0.0000 0100

7010201 0 .34062000 .34062000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*INLET ANNULUS MIDDLE VOLUME INTACT SIDE

7300000 "INANMIDINT" ANNULUS

7300001 1

7300101 0.1308530 1

7300301 0.2851823 1

7300401 0.0 1

7300501 0.0 1

7300601 -90.0 1

7300801 3.81-6 0.172 1

7301001 00 1

7301201 0 15028400. 12.33830. 2459250. 0.0 0.0 01

*------------1 ------ 1--I------- 1--------1 -------- 1 -------- 1----

*JUNCTION - MIDDLE TO LOWER INLET ANNULUS INTACT SIDE ---- -------- --- 1 I--------1 -------- 1-------- 1--- 1--l----

7310000 "INANIILINT " SNGLJUN

7310101 730010000 702000000 0.0709408 0.0 0.0 0100

7310201 0 1.5959 1.5959 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*INLET ANNULUS LOWER VOLUME INTACT SIDE

7020000 "INANLWRINT" ANNULUS

7020001 1

7020101 0.1464354 1

7020301 0.2525361 1

7020401 0.0 1

7020501 0.0 1

7020601 -90.0 1

7020801 3.81-6 0.172 1

7021001 00 1

7021201 0 15030500. 1233830. 2459300. .00000000 0.0 01

*JUNCTION -INLET ANNULUS TO DOWNCOMER INTACT SIDE

7030000 "INAN2DCINT" SNGLJUN

7030101 702010000 704000000 0.0709408 0.0000 0.0000 0100

7030201 0 1.5959000 1.5959000 0.0

*------------1 -------- 1 -------- 1 -------- 1 -------- 1--------1---

*DOWNCOMER UPPER VOLUME INTACT SIDE

7040000 "DNCRUPRINT" ANNUJLUS

7040001 1

7040101 0.0 1

7040301 1.5200561 1

7040401 0.1581866 1

7040501 0.0 1

7040601 -90.0 1

7040801 3.81-6 0.102 1

B- 9
7041001 00 1

7041201 0 15036100. 1233810. 2459350. .00000000 0.0 01

*JUNCTION -UPPER TO MIDDLE DOWNCOMER INTACT SIDE

7050000 "UPRZIIIDINT". SNGLjUN

7050101 704010000 706000000 0.0709408 0.0000 0.0000 0100

7050201 0 1.5106000 1.5106000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1---

*DOWNCOMER MIDDLE VOLUME INTACT SIDE

7060000 "DNCRIIIDINT" AiNNULUS

7060001 1

7060101 0.0 1

7060301 1.2616333 1

7060401 0.1217000 1

7060501 0.0 1

7060601 -90.0 1

7060801 3.81-6 0.102 1

7061001 00 1

7061201 0 15045800. 1233800. 2459500. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*JUNCTION -MIDDLE TO LOWER DOWNCOMER INTACT SIDE

7070000 "IIID2LWRINT" SNGLJUN

7070101 706010000 708000000 0.07094-08 0.0000 0.0000 0100

7070201 0 1.4821000 1.4821000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*DOWNCOMER LOWER VOLUME INTACT SIDE

7080000 "DNCRLWRINT" ANNUJLUS

7080001 1

7080101 0.0 1

7080301 1.0792591 1

7080401 0.0986806 1

7080501 0.0 1

7080601 -90.0 1

7080801 3.81-6 0.102 1

7081001 00 1

7081201 0 15054000. 1233790. 2458600. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*JUNCTION -LOWER DOWNCONER TO LOWER PLENUM INTACT SIDE

7090000 "LRDC2LPINT" SNGLJUN

7090101 708010000 215000000 0.0709408 0.0000 0.0000 0100

7090201 0 1.4104000 1.4104000 0.0

* ------------1--------1 -------- 1 -------- 1 ------ 1--I-------1----

*INLET ANNULUS UPPER VOLUME BROKEN SIDE

7100000 "INANUPRBKN" ANNULUS

7100001 1

7100101 0.1308530 1

7100301 0.1876129 1

7100401 0.0 1

7100501 0.0 1

7100601 90.0 1

7100801 3.81-6 0.172 1

7101001 00 - 1

7101201 0 15027200. 1233830. 2459250. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

* JUNCTION - MIDDLE TO UPPER INLET ANNULUS BROKEN SIDE

B-10
7110000 "INANIIUBKN " SNGLJUN

7110101 740000000 710000000 0.129467 0.0000 0.0000 0100

7110201 0 -. Z2873200 -. 2873200 0.0

* --- -- 1 -- -- 1 -- --1-----1- 1 -- -- 1 -----1---

*INLET ANNULUJS MIDDLE VOLUME BROKEN SIDE

7400000 "INANNIDBKN" ANNUJLUS

7400001 1

7400101 0.1308530 1

7400301 0.2851823 1

7400401 0.0 1

7400501 0.0 1

7400601 -90.0 1

7400801 3.81-6 0.172 1

7401001 00 1

7401201 0 15028400. 1233830. 2459250. 0.0 0.0 01

* ------------1--------1 -------- 1----- 1--------1 -------- 1----

* JUNCTION -MIDDLE TO LOWER INLET ANNULUS BROKEN SIDE

7410000 "INANMLBI(N "SNGLJUN

7410101 740010000 712000000 0.0709408 0.0 0.0 0100

7410201 0 .86411 .86411 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*INLET ANNULUS LOWER VOLUME BROKEN SIDE

7120000 '

t

INANLWRBKN" ANNULUIS

7120001 1

7120101 0.1464354 1

7120301 0.2525361 1

7120401 0.0 1

7120501 0.0 1

7120601 -90.0 1

7120801 3.81-6 0.172 1

7121001 00 1

7121201 0 15029700. 1233820. 2459200. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*JUNCTION -INLET ANNULUS TO DOWNCOMER BROKEN SIDE

7130000 "INAN2DCBI{N" SNGLJ1JN

7130101 712010000 714000000 0.0709408 0.0000 0.0000 0100

7130201 0 .86411000 .86411000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*DOWNCOMER UPPER VOLUME BROKEN SIDE

7140000 "DNCRDPRBEN" ANNULUS

7140001 1

7140101 0.0 1

7140301 1.5200561 1

7140401 0.1581866 1

7140501 0.0 1

7140601 -90.0 1

7140801 3.81-6 0.102 1

7141001 00 1

7141201 0 15036100. 1233800. 2459350. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I---

*JUNCTION -UPPER TO MIDDLE DOWNCOMER BROKEN SIDE

7150000 "UPR2IIIDBKN" SNGLJUN

7150101 714010000 716000000 0.0709408 0.0000 0.0000 0100

7150201 0 1.1432000 1.1432000 0.0

B-1i
*DOWNCOMER MIDDLE VOLUME BROKEN SIDE

7160000 "DNCRIIIDBKN" ANNULUS

7160001 1

7160101 0.0 1

7160301 1.2616333 1

7160401 0.1217000 1

7160501 0.0 1

7160601 -90.0 1

7160801 3.81-6 0.102 1

7161001 00 1

7161201 0 15045800. 1233780. 2459500. .00000000 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*- JUNCTION -MIDDLE TO LOWER DOWNCOIIER BROKEN SIDE

7170000 "NID2LWRBKN' SNGLJ1JN

7170101 716010000 718000000 0.0709408 0.0000 0.0000 0100

7170201 0 1.3175000 1.3175000 0.0

* ------------1--------1 --------1 --------1 ------ 1--I-------1----

*DOWNCOMER LOWER VOLUMIE BROKEN SIDE

7180000 tfDNCRLWRBIN" ANNUJLUS

7180001 1

7180101 0.0 1

7180301 1.0792591 1

7180401 0.0986806 1

7180501 0.0 1

7180601 -90.0 1

7180801 3.81-6 0.102 1

7181001 00 1

7181201 0 15054000. 1233760. 2458600. .00000000 0.0 01

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1-------- 1----

*JUNCTION - LOWER DOWNCOrlER TO LOWER PLENUM BROKEN SIDE

7190000 "LRDC2LPBKN" SNGLJUN

7190101 718010000 215000000 0.0709408 0.0000 0.0000 0100

7190201 0 1.3892000 1.3892000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*CROSSFLOW JUNCTION - UPPER INLET ANNULUS

7200000 "UPRINANNXF" SNGLJUN

7200101 700000000 710000000 0.0296780 98.000 18.000 0003

7200201 0 .28732000 .28732000 0.0

*------------1 -------- 1 -------- 1 -------- 1- 1----l------ 1----

*CROSSFLOW JUNCTION -LOWER INLET ANNULUS

7220000 "LWRINANNXF" SNGLJIJN

7220101 702000000 712000000 0.0428706 98.000 18.000 0003-

7220201 0 .38395000 .38395000 0.0

*------------1 -------- 1 -------- 1 ------ ---- 1------1---

*CROSSFLOW JUNCTION - UPPER DOWNCOMER

7240000 "UPRDNCMRXF" SNGLJUN

7240101 704000000 714000000 0.03 98.0 18.0 0003

7240201 0 .19557000 .19557000 0.0

*CROSSFILOW JUNCTION -MIDDLE DOWNUOMER

7260000 "MIDDNCIIRXF" SNGLJUN

7260101 706000000 716000000 0.03 98.0 18.0 0003

B-i12
7260201 0 .10572000 .10572000 0.0

* --- -- 1 -- -- 1-- -- 1-----1 - 1--- 1--I-----I---

* CROSSFLOW JUNCTION - LOWER DOWNCO!IER

*----- ---- 1----1------1-------- 1-------- 1----

7280000 "LWRDNCNRX" SNGLJUN

7280101 708000000 718000000 0.03 98.0

7280201 0 .07171910 .07171910 0.0

*----- ---- 1----1------1-------- 1-------- 1----

*LOWER PLENUMI TOP VOLUME

2150000 "LWR PL TOP" BRANCH

2150001 2 0

2150101 0.0 0.3533183 0.2592277 0.0

2150102 3.81-6 0.0 00

2150200 0 15059400. 1233780. 24585~

2151101 215010000 220000000 0.0 0.005

2152101 215000000 225000000 0.1499 1.5

2151201 .571898-5 .571894-5 0.0

2152201 1.7076000 1.7076000 0.0

*----- ---- 1----1------1-------- 1-------- 1----

*LOWER PLENUM BOTTOM VOLUME

2200000 "LWR PL BOT" SNGLVOL

2200101 0.0 0.3741720 0.29656 0.0

2200102 4.OE-5 0.0 00

18.0 0003

-90.0 -0.3533183

50. .00000000

0.005 0000

1.5 0000

-90.0. -0.3741720

2200200 0 15062100. 1233780. 2458500. .00000000

*LOWER CORE SUPPORT STRUCTURE

2250000 "L CORE SUP" BRANCH

*2250001 2 0

2250001 3 0

2250101 0.2832456 0.5709989 0.0 0.0 90.0

2250102 3.81-6 0.095 00

2250200 0 -44970400. 1230690. 2460590.

2251101 225010000 011000000 0.09790318 1.5 1.5

2252101 225010000 021000000 0.01549682 1.5 1.5

2253101 225010000 235000000 0.0 12.0 12.0

2251201 2.0569000 2.0569000 0.0

2252201 2.0569000 2.0569000 0.0

2253201 0.0602599 0.15501 0.0

* ------------1--------1 ------ 1--I------- 1--------1 ----

*PERIPHERAL CORE VOLUMIE 1

0110000 "PERI#1" BRANCH

0110001 2 0

0.5709989

0.0

00100

00100

00100

0110101 0.1582181 0.279404 0.0

0110102 1.27-7 0.0 .00

0110200 0 14965200. 1241(

0111101 011010000 012000000 0.

0112101 011000000 02100000 0. 23~

0111201 1.3752 1.3752 0.0

0112201 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1----

*PERIPHERAL CORE VOLUME 2

0120000 "PERI#1" BRANCH

0120001 2 0

0120101 0.1462431 0.279404 0.0

0120102 1.27-7 0.0 00

0120200 0 14965200. 1241(

0.0 90.0 0.279404

310.- 2460710. 0.0

0.0 0.0 00100

)275 4.69 4.69 00003

0.0 90.0 0.27~

10O. 2460710. 0.0

9404

B-i13
0121101 012010000 013000000 0.122946 0.66 0.66 00100

0122101 012000000 022000000 0.239275 4.69 4.69 00003

0121201 1.3752 1.3752 0.0

0122201 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

*PERIPHERAL CORE VOLUME 3

0130000 "PERI#1" BRANCH

0130001 2 0

0130101 0.1479421 0.279404 0.0 0.0 90.0 0.279404

0130102 1.27-7 0.0 00

0130200 0 14965200. 1241610. 2460710. 0.0

0131101 013010000 014000000 0. 0.0 0.0 00100

0132101 013000000 023000000 0.239275 4.69 4.69 00003

0131201 1.3752 1.3752 0.0

0132201 0.0 0.0 0.0

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1----

*PERIPHERAL CORE VOLUME 4

0140000 "PERfI1"' BRANCH

0140001 2 0

0140101 0.1452617 0.279404 0.0 0.0 90.0 0.279404

0140102 1.27-7 0.0 00

0140200 0 14965200. 1241610. 2460710. 0.0

0141101 014010000 015000000 0.122946 0.66 0.66 00100

0142101 014000000 024000000 0.239275 4.69 4.69 00003

0141201 1.3752 1.3752 0.0

0142201 0.0 0.0 0.0

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1----

*PERIPHERAL CORE VOLUME 5

0150000 "PERI#1" BRANCH

0150001 2 0

0150101 0.1464111 0.279404 0.0 0.0 90.0 0.279404

0150102 1.27-7 0.0 00

0150200 0 14965200. 1241610. 2460710. 0.0

0151101 015010000 016000000 0. 0.0 0.0 00100

0152101 015000000 025000000 0.239275 4.69 4.69 00003

0151201 1.3752 1.3752 0.0

0152201 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

*PERIPHERAL CORE VOLUME 6

0160000 "PERI#1" BRANCH

0160001 1 0

0160101 0.1510117 0.279404 0.0 0.0 90.0 0.279404

0160102 1.27-7 0.0 00

0160200 0 14965200. 1241610. 2460710. 0.0

0161101 016000000 026000000 0.239275 4.69 4.69 00003

0161201 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

*CENTRAL CORE VOLUME 1

*----- ---- --- 1--- 1---------1 -------- 1 ---- ---- 1----

0210000 ??CET#1II BRANCH

0210001 1 0

0210101 0.0250439 0.279404 0.0 0.0 90.0 0.279404

0210102 1.27-7 0.0 00

0210200 0 14965200. 1241610. 2460710. 0.0

0211101 021010000 012000000 0.0 0.0 0.0 00100

0211201 1.3752 1.3752 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

B-14
* CENTRAL CORE VOLUME 1

0220000 "CENT#1" BRANCH

0220001 1 0

0220101 0.0250439 0.279404 0.0 0.0 90.0 0.279404

0220102 1.27-7 0.0 00

0220200 0 14965200. 1241610. 2460710. 0.0

0221101 022010000 023000000 0.021054 0.66 0.66 00100

0221201 1.3752 1.3752 0.0

* CENTRAL CORE VOLUME 3

*----- ---- I----1------1-------- 1-------- 1-------- 1----

0230000 "CEN'T'l" BRANCH

0230001 1 0

0230101 0.0262243 0.279404 0.0 0.0 90.0 0.279404

0230102 1.27-7 0.0 00

0230200 0 14965200. 1241610. 2460710. 0.0

0231101 023010000 024000000 0.0 0.0 0.0 00100

0231201 1.375:2 1.3752 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

* CENTRAL CORE VOLUME 4

*------------ 1---- -- 1-- -- -- I----1------1--- ---- 1----

0240000 "CENT#1" BRANCH

0240001 1 0

0240101 0.0250439 0.279404 0.0 0.0 90.0 0.279404

0240102 1.27-7 0.0 00

0240200 0 14965200. 1241610. 2460710. 0.0

0241101 024010000 025000000 0.021054 0.66 0.66 00100

0241201 1.3752 1.3752 0.0

* ------------1--------1 --------1---- -- 1--I---- 1---- I--

* CENTRAL CORE VOLUME 5

*-----------I-1--- ---- 1 -------- 1 ---- -- 1-I--------1 ----

0250000 "CENT#1" BRANCH

0250001 1 0

0250101 0.0250439 0.279404 0.0 0.0 90.0 0.279404

0250102 1.27-7 0.0 00

0250200 0 14965200. 1241610. 2460710. 0.0

0251101 025010000 026000000 0.0 0.0, 0.0 00100

0251201 1.3752 1.3752 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1----

* CENTRAL CORE VOLUME 6

*------------ 1------1--I------- 1------1--I-------1I----

0260000 "CENT#i" BRANCH

0260001 1 0

0260101 0.0262243 0.279404 0.0 0.0 90.0 0.279404

0260102 1.27-7 0.0 00

0260200 0 14965200. 1241610. 2460710. 0.0

0261101 026010000 240000000 0.021054 1.5 1.5 00100

0261201 1.3752 1.3752 0.0

*CORE BYPASS VOLUME

2350000 "CORE BYPSS" PIPE

2350001 3

2350101 0.0129428 3

2350201 0.0 2

2350301 0.5588068 3

2350401 0.0 3

2350501 0.0 3

2350601 90.0 3

B- 15
2350801 3.81-6 0.003 3

2350901 0.0 0.0 2

2351001 00 3

2351101 0000 2

2351201 0 15048000. 1233790. 2459550.0 .00000000 0.0 01

2351202 0 15042400. 1233790. 2459550.0 .00000000 0.0 02

2351203 0 15036500. 1233790. 2459550.0 .00000000 0.0 03

2351300 0

2351301 .71258000 .71258000 0.0 01

2351302 .73579000 .73579000 0.0 02

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*UPPER END BOXES AND SUPPORT STRUCTURE

2400000 "UPR END BXV' BRANCH

2400001 2 0

2400101 0.2423341 0.5867979 0.0 0.0 90.0 0.5867979

2400102 3.81-6 0.145 00

2400200 0 14946300. 1422480. 2461120. 1.37821-3

2401101 016010000 240000000 0.122945736 1.5 1.50 00100

2402101 235010000 24000000 0.0 12. 12. 00100

2401201 .67053000 .87895000 0.0

2402201 .67053000 .87895000 0.0

*----- ---- 1----I------I-------- 1--------1 ------- 1-I--- --- 1---- *UPPER CORE SUPPORT STRUCTURE -CROSS FLOW REGION

2450000 "UPR CR SLUP" BRANCH

2450001 2 0

2450101 - 0.0 0.4933Z48 0.128080 0.0 90.0 0.4933248

2450102 3.81-6 0.145 00

2450200 0 15025400. 1417510. 2459600. .00000000

2451101 240010000 245000000 0.0 0.0 0.0 0000

2452101 245010000 251000000 0.0 0.0 0.0 0000

2451201 1.1669000 1.1669000 0.0

2452201 .439867-4 .439867-4 0.0

*----I--- 1 ---- ----- 1--I------1 -------- 1 -------- 1 ---- *UPPER FLOW SKIRT-REGION

2500000 "U FLW SKRT" BRANCH

2500001 1 0

2500101 0.1547532 0.7850547 0.0 0.0 90.0 0.7850547

2500102 3.81-6 0.131 00

2500200 0 15020100. 1410020. 2459600. .00000000

2501101 24501000 250000000 0.0 0.0 0.0 0000

2501201 1.8273000 1.8273000 0.0

* ------------1--7----1l-------1 I--------1 ---- -- 1-I-------1 I----

*DEAD END OF FUEL HODULES

2510000 "DE FL MODS" SNGL VOL

2510101 0.0 0.784413 0.1.154214 0.0 90.0 0.7M4123

2510102 3.81-6 0.214 00

2510200 0 15021500. 1424270. 2459600. .00000000

*UPPER HEAD ---------- - -1--- --- 1 --- ---- 1--------1 --------1-------1---

2520000 "UPR HEAD "BRANCH

2520001 2 0

2520101 0.2622585 0.2869580 0.0 0.0 90.0 - 0.2869580

2520102 3.81-6 0.0 00

2520200 0 15019000. 1410020. 2459550. .00000000

2521101 250010000 252000000 0.0 0.006 0.006 0000

2522101 - 730000000 252000000 0.0 0.90+4 0.90+4 00Q3

B-1 6
2521201 -.1334300 .1334300 0.0

2522201 .05329530 .05329530 0.0

* ------------1--------1-------- 1--------1i------1--I------- 1---- *UPPER PLENUM BOTTOM VOLUME

2550000 "UPR PL BOT" BRANCH

2550001 2 0

2550101 0.2622585 0.6312304 0.0 0.0 90.0 0.6312304

2550102 3.81-6 0.0 00

2550200 0 15017200. 1410020. 2459500. .00000000

2551101 250010000 255000000 0.0 0.006 0.006 0000

2552101 255010000 260000000 0.0 0.03 0.03 0000

2551201 - .0450137 -. 0450137 0.0

2552201 .186978-4 .186979-4 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1---- *UPPER PLENUM TOP VOLUME

2600000 "UPR PL TOP" SNGL VOL

2600101 0.0 0.7747094 0.1914909 0.0 90.0 0.7747094

2600102 3.81-6 0.0 00

2600200 0 15013400. 1410020. 2459500. .00000000

*BROKEN LOOP

*REACTOR VESSEL NOZZLE - BROKEN LOOP HOT LEG

3000000 "RVN BLHL "BRANCH

3000001 2 0

3000101 0.0 0.876303 0.0575410 0.0 0.0 0.0

3000102 4.OE-5 0.0 00

3000200 0 15018100. 1231960. 2459500. .00000000

3001101 252010000 300000000 0.067014 0.7385868 1.2309481 0002

3002101 300010000 305000000 0.063426 0.1005 0.1005 0000

3001201 -.0578446 -.0578446 0.0

3002201 -.0611292 -.0611292 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*HOT LEG PIPE TO REFLOOD ASSIST BYPASS TEE

3050000 "HLP-RABS T" BRANCH

3050001 1 0

3050101 0.0 0.698336 0.0442927 0.0 0.0 0.0

3050102 4.OE-5 0.0 00

3050200 0 15018100. 1231980. 2459500. .00000000

3051101 305010000 310000000 0.063426 0.1005 0.1005 0000

3051201 - .0611386 - .0611386 0.0

* ------------1--------1 --------1 --------1 ---- -- 1-I--------1---- *BROKEN LOOP HOT LEG CONTRACTION

3100000 "BLHL CONTR" BRANCH

3100001 2 0

3100101 0.0 1.50013 0.0678467 0.0 0.0 0.0

3100102 4.OE-5 0.0 00

3100200 0 15018100. 1231950. '2459500. .00000000

3101101 380010000 310000000 0.0388 0.84 0.84 0000

3102101 310010000 315000000 8.3647-3 0.553 1.09056 0000

3101201 .10016000 .10016000 0.0

3102201 .922485-3 .922485-3 0.0

* ------------1---- -- 1-I--------1 --------1 --------1 ---- ----1----

* STEAM GENERATOR AND PUMP SIMIJLATIOR

B-1 7
3150000 "ISG+PIIP Sim" PIPE

3150001 8

3150101 0.0 8

3150201 8.3647-3 1

3150202 1.12-2 2

3150203 0.105626 3

3150204 1.12-2 4

3150205 8.3647-3 7

3150301 0.919969 1

3150302 1.987956 2

3150303 0.849744 4

3150304 1.987956 5

3150305 1.371350 6

3150306 1.365029 7

315030Y7 1.674812 8

3150401 7.75291-3 1

3150402 0.1721108 2

3150403 8.97552-2 4

3150404 0.1721108 5

3150405 1.82303-2 6

3150406 5.46687-2 7

3150407 1.82489-2 8

3150601 90.0 3

3150602 -90.0 7

3150603 90.0 8

3150701 0.679201 1

3150702 1.987956 2

3150703 0.457202 3

3150704 -0.457202 4

3150705 -1.987956 5

3150707 -1.371350 6

3150708 -0.520701 7

3150709 1.212851 8

3150801 4.OE-5 0.0 8

3150901 0.93596 0.93596 1

3150902 2.0. 2.0 2

3150903 0.5 0.5 3

3150904 2.0 2.0 4

3150905 0.23025 0.23025 5

3150906 2.534 2.534 6

3150907 5.069 5.069 7

3151001 00 8

3151101 0000 7

3151201 0 15015600. 1243880. 2459924. .00000000 0.0 01

3151202 0 15005700. 1237630. 2459924. .00000000 0.0 02

3151203 0 14996600. 1237670. 2459924. .00000000 0.0 03

3151204 0 14996600. 1237680. 2459924. .00000000 0.0 04

3151205 0 15005600. 1237680. 2459924. .00000000 0.0 05

3151206 0 15018100. 1237680. 2459924. .00000000 0.0 06

315120Y7 0 15025100. 1237680. 2459924. .00000 0.0 0r7

3151208 0 15022500. 1237680. 2459924. .0000000 0.0 08

3151300 0

3151301 .910345-3 .910345-3 0.0 01

3151302 .487913-3 .487915-3 0.0 02

3151303 .411825-4 .411825-4 0.0 03

3151304 .289111-3 .289109-3 0.0 04

3151305 .133199-3 .133198-3 0.0 05

3151306 . 106449-3 .106449-3 0.0 06

3151307 .266103-4 .266103-4 0.0 07

* -----------1--------1 -------- 1 -------- 1 -------- 1--------1----

B- 18
*HOT LEG BREAK VALVE

3170000 "HlL BREAK "VALVE

3170101 315010000 800000000 8.3647-3 0.94883 0.94883 0100

3170102 0.93 0.84

3170201 0 .00000000 .00000000 0.0

3170300 TRPVLV

3170301 501

*REACTOR VESSEL NOZZLE - BROKEN LOOP COLD LEG

3350000 "RVN BLCL "BRANCH

3350001 2 0

3350101 0.0 0.749305 0.047979 0.0 0.0 0.0

3350102 4.OE-5 0.0 00

3350200 0 15028400. 1233660. 2459250. .00000000

3351101 740000000 335000000 0.064130 1.455594 0.812933 0002

3352101 335010000 340000000 0.063426 0.1005 0.1005 0000

3351201 .06071680 .06071680 0.0

3352201 .06138070 .06138070 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

*COLD LEG PIPE TO REFLOOD ASSIST BYPASS TEE

3400000 "CLP-RABS T" BRANCH

3400001 1 0

3400101 0.0 0.698336 0.0443927 0.0 0.0 0.0

3400102 4.OE-5 0.0 00

3400200 0 15028400. 1233140. 2459250. .00000000

3401101 340010000 342000000 0.063426 0.1005 0.1005 0000

3401201 .06137130 .06137130 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

*BROKEN LOOP COLD LEG RABS TO DTT

3420000 "BLCL 2DTT "BRANCH

3420001 1 0

3420101 0.0 0.5715069 0.0362484 0.0 0.0 0.0

3420102 4.OE-5 0.0 00

3420200 0 15028400. 1232540. 2459250. .00000000

3421101 342000000 370000000 0.0388 0.84 0.84 0000

3421201 .10030000 .10030000 0.0

*----- ---- I----1------1-------- 1-------- 1-------- 1-------- 1----

*BROKEN LOOP COLD LEG DTT TO BREAK PLANE

3440000 "BLCL 2BRK "BRANCH

3440001 1 0

3440101 0.0 0.9286231 0.0310679 0.0 0.0 0.0

3440102 4.OE-5 0.0 00

3440200 0 15028400. 1232300. 2459250. .00000000

3441101 342010000 344000000 0.0540157 6.545 14..05 0000

3441201 .759199-5 .759199-5 0.0

* ------------1---- ---- 1 ---- -- 1-I--------1 -------- 1 -------- 1 ----

*COLD LEG BREAK VALVE

3470000 "Cl, BREAK "VALVE

3470101 34401000 805000000 8.3647-3 0.415 0.415 0100

3470102 0.93 0.84

3470201 0 .00000000 .00000000 0.0

3470300 TRPVLV

3470301 501

* ------- 11------ 1---- ---- -- --I----1 ------1-------- 1--------1I----

* REFLOOD ASSIST BYPASS PIPING - COLD LEG SIDE

B-1 9
3700000 "RABS C L " PIPE

3700001 3

3700101 0.0388 2

3700102 0.0776 3

3700201 0.0388 2

3700301 0.0 3

3700401 0.0279 1

3700402 0.070 2

3700403 0.1165 3

3700601 90.0 1

3700602 0.0 3

3700701 0.64 1

3700702 0.0 3

3700801 4.0-5 0.0 3

3700901 0.28 0.28 1

3700902 0.84 0.84 2

3701001 00 3

3701101 0000 2

3701201 0 15026000. 1232040. 2459300. .00000000 0.0 01

3701202 0 15023600. 1231420. 2459300. .00000000 0.0 02

3701203 0 15023600. 1231430. 2459300. .00000000 0.0 03

3701300 0

3701301 .10029000 .10029000 0.0 01

3701302 .10027000 .10027000 0.0 02

* ---- ---- 1--------1 -------- 1 -------- 1 --------I -------- 1 ---- *REFLOOD ASSIST BYPASS VALVES

3750000- "RABS VALVS" SNGLJ1N

3750101 370010000 380000000 0.0 0.90+4 0.90+4 0000

3750201 0 .05011390 .05011390 0.0

* ---- ---- 1--------1 -------- 1 -------- 1 ---- --- 1 -------- 1 ---- *REFLOOD ASSIST BYPASS PIPING - HOT LEG SIDE

3800000 "RABS H L " PIPE

3800001 3

3800101 0.0776 1

3800102 0.0388 3

3800201 0.0388 2

3800301 0.0 3

3800401 0.0915 1

3800402 0.048 2

3800403 0.0489 3

3800601 0.0 1

3800602 -90.0 2

3800603 0.' 0 3

3800701 0.0 1

3800702 -0.64 2

3800703 0.0 3

3800801 4.0-5 0.0 3

3800901 0.84 0.84 1

380090 0.28 0.28 2

3801001 00 3

3801101 0000 2

3801201 0 15013400. 1231620. 2459400. .00000000 0.0 01

3801202 0 15015700. 1231730. 2459400. .00000000 0.0 02

3801203 0 15018100. 1231820. 2459400. .00000000 0.0 03

3801300 0

3801301 .10020000 .10020000 0.0 01

3801302 .10018000 .10018000 0.0 02

B-20
* PRESSURIZER

*SURGE LINE PCS SIDE

4000000 "SRG LN PCS" BRANCH

4000001 2 0

4000101 1.44561-3 2.30 0.0 0.0 90.0 0.54

4000102 2.3622-5 0.0 00

4000200 0 15012400. 1418060. 2459400. .00000000

4001101 107000000 400000000 1.44561-3 3.9 3.9 0002

4002101 400010000 405000000 1.44561-3 2.85 2.85 1000

4001201 -.0607909 - .0607909 0.0

4002201 - .0608265 -.0608265 0.0

*----- ---- I----1------1-------- 1-------- 1-------- 1-------- 1----

*PRESSURIZER SURGE LINE

4050000 "SRG LN PZR" PIPE

4050001 2

4050101 1.44561-3 2

4050201 1.44561-3 1

4050301 2.30 2

4050401 0.0 2

4050601 90.0 2

4050701 0.30 2

4050801 2.3622-5 0.0 2

4050901 2.85 2.85 1

4051001 00 2

4051101 1000 1

4051201 0 15010800. 1427980. 2459500. .00000000 0.0 01

4051202 0 15010100. 1444040. 2459500. .00000000 0.0 02

4051300 0

4051301 - .0608633 - .0608633 0.0 01

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PRESSURIZER SURGE LINE

4100000 "SRG LINE "SNGLJ1JN

4100101 405010000 415000000 1.44561-3 0.42 1.00 1000

4100201 0 -.0608789 -.0608789 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

*PRESSURIZER VESSEL

4150000 "PZR VESSEL" PIPE

4150001 6

4150101 0.0 2

4150102 0.5653 5

4150103 0.0 6

4150201 0.0 5

4150301 0.1815 1

4150302 0.1524 2

4150303 0.3967 3

4150304 0.5289 4

4150305 0.3967 5

4150306 0.1943 6

4150401 0.0684 1

4150402 0.0838 2

4150403 0.0 5

4150404 0.0732 6

4150501 0.0 6

4150601 90.0 6

B-21
4150801 4.0E-5 0.0 6

4151001 00 6

4151101 0000 5

4151201 0 15009100. 1586220. 2459600. .00000000 0.0

4151202 0 15008000. 1586220. 2459600. .00000000 0.0

4151203 0 15006300. 1586220. 2459600. .00000000 0.0

4151204 0 15003800. 1586220. 2460000. .03846070 0.0

4151205 0 15002300. 1586220. 2466560. 1.0000000 0.0

4151206 0 15002000. 1586220. 246160. 1.0000000 0.0

4151300 0

4151301 -.23340-3 -.23340-3 0.0 01

4151302 -. 15968-3 -. 15968-3 0.0 02

4151303 -.19217-3 .36250000 0.0 03

4151304 -.4272500 -.48004-4 0.0 04

4151305 -.23263-4 - .23253-4 0.0 05

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PRESSURIZER VESSEL TO TOP HAT

4170000 "VSSL-TPHAT" SNGLJUN

4170101 415010000 420000000 0.0 0.0 0.0 0000

4170201 0 -. 21090-4 -. 21090-4 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*PRESSURIZER TOP HAT AND RELIEF CONNECTION

4200000 "PZR TOPHAT" PIPE

4200001 2

4200101 0.0 2

4200201 0.0 1

4200301 0.1104915 2

4200401 0.0139870 2

4200601 90.0 2

4200801 43E-5 0.346066 2

4201001 00 2

4201101 0000 1

4201201 0 15001900. 1509900. 2482590. 1.0000000 0.0

4201202 0 15001800. 1509900. 248480. 1.0000000 0.0

4201300 0

4201301 - .11442-4 - .11442-4 0.0 01

*STEAII GENERATOR SECONDARY SIDE

*PRIMARY SEPARATOR

5000000 "SEPARATOR " SEPARATR

5000001 3 0

5000101 0.0 0.4445 0.2425 0.0 90.0 0.4445

5000102 43E-5 0.2840 00

5000200 0 5828810.0 n45280. 2580000. .49664000

5001101 500010000 520000000 0.087745 0.0 0.0 0100

5002101 500000000 505000000 0.087745 0.0 0.0 0100

5003101 515010000 500000000 0.29187 0.4 0.4 0100

5001201 .30829000 1.0170000 0.0

5002201 1.1801000 .17265000 0.0

5003201 2.4900000 2.4900000 0.0

*SEPARATOR BYPASS

5030000 "SEPBYPASS "BRANCH

5030001 2 0

01

02

03

04

05

06

01

02

B-22.-
5030101 0.0 0.4445 0.4384 0.0 90.0 0.4445

5030102 4.E-5 0.3678 00

5030200 0 5827350.0 1150000. 2591270. .99988000

5031101 505000000 503000000 0.98627 0.0 0.0 0100

5032101 503010000 520000000 0.98627 0.8 0.0 0100

5031201 -1.265400 .17607000 0.0

5032201 -.3871600 .07560020 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*SEPARATOR OUTLET REGION

5050000 "LWR SEPAR "BRANCH

5050001 1 0

5050101 0.0 1.2131 1.4850 0.0 -90.0 -1.2131

5050102 4.E-5 1.9048 00

5050200 0 5830080.0 1236530. 2580000. .02870570

5051101 505010000 508000000 0.0 0.0 0.0 0100

5051201 .64364000 -2.022800 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*FEED INLET VOLUME

508000 "UPR DWNCMR" BRANCH

5080001 1 0

5080101 0.0 0.6096 0.22107 0.0 -90.0 -0.6096

5080102 43E-5 0.163697 00

5080200 0 5835210.0 1145280. 2580000. .00000000

5081101 503010000 510000000 0.0 0.0 0.0 0100

5081201 .66587000 .66587000 0.0

* ------------1------1--I------- 1--------1 --------1 --------1----

*STEAM GENERATOR DOWNCOMER

5100000 "DWNCIIR " ,ANNUJLUS

5100001 3

5100101 0.232 3

5100201 0.0 2

5100301 0.6096 3

5100401 0.0 3

5100601 -90.0 3

5100701 -0.6096 3

5100801 4.E-5 0.10793 3

5100901 0.0 0.0 2

5101001 00 3

5101101 0000 2

5101201 0 5839840.0 1145550. 2580000. .00000000 0.0 01

5101202 0 5844480.0 1145820. 2580000. .00000000 0.0 02

5101203 0 5849120.0 1146090. 2580000. .00000000 0.0 03

5101300 0

5101301 .66594000 .66594000 0.0 01

5101302 .66602000 .66602000 0.0 02

* ------------1--------1 ------ 1--I------- 1------1--I------- 1---- * JUNCTION - DOWNCOIIER TO BOILER

5130000 "DNCMR-BLR "SNGLJ1JN

5130101 510010000 515000000 0.0 17.5 17.5 0100

5130201 0 .66609000 .88146000 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*STEAM GENERATOR BOILER

5150000 "BOILER "PIPE

5150001 5

5150101 0.2776 4

5150102 0.306294 5

B-23
5150201 0.0 4

5150301 1.8288 4

5150302 1.2131 5

5150401 0.0 5

5150601 60.0 4

5150602 90.0 5

5150701 0.6096 4

5150702 1.2131 5

5150801 4.E-5 0.0234 4

5150802 4.E-5 0.5962 5

5150901 4.05 4.05 4

5151001 00 5

5151101 0100 4

5151201 0 5846670.0 1222840. 2580000. .01975860 0.0 01

5151202 0 5842700.0 1274560. 2580000. .05552290 0.0 02

5151203 0 5838650.0 1321.180. 2580000. .08907110 0.0 03

5151204 0 5834160.0 1360130. 2580000. .11715000 0.0 04

5151205 0 5829740.0 14414230. 2580000. .15606000 0.0 05

5151300 0

5151301 .83850000 1.1089000 0.0 01

5151302 1.3147000 1.8082000 0.0 02

5151303 1.7463000 2.4614000 0.0 03

5151304 2.1057000 2.9324000 0.0 04

*------------1 -------- 1 -------- 1 -------- 1--------1 -- *---1----

*LOWER PORTION OF STEAM DONE ----- ----- 1---1------1 -------- 1 ---- ---- 1-----1 -- 1--

5200000 "LWR Sill DMI" BRANCH

5200001 1 0

5200101 0.0 0.46956 0.705312 0.0 90.0 0.46956

5200102 4.E-5 1.383 00

5200200 0 5827210.0 1150000. Z591540. .99979000

5201101 520010000 525000000 0.0 0.0 0.0 0000

5201201 - .0806823 .41903000 0.0

*----- ---- 1----1---- 1--1------ 1-------- 1-------- 1-------- 1----

*UPPER PORTION OF STERN DOME

5250000 "UPR Sill DM" BRANCH

5250001 1 0

5250101 0.0 0.46956 0.705312 0.0 -90.0 0.46956

5250102 4.E-5 1.383 00

5250200 0 5827070.0 1150000. 2591710. .99990000

5251101 525010000 530000000 0.0 0.8 0.8 0100

5251201 13.328000 13.578000 0.0

*----- ---- 1----1------1-------- 1------l--1------ 1-------- 1----

*STEAM PIPE* FROM GENERATOR- TO CONTROL VALVE

5300000 "STERN PIPE" SNGL VOL

5300101 0.04635 25.0Y74 0.0 0.0 0.0 0.0

5300102 4.E-5 0.0 00

5300200 0 5819190.0 1148038. Z591620. 1.0000000

* ------------1--------1 -------- 1 -------- 1 -------- 1--------1---

*STEAM FLOW CONTROL VALVE.

5400000 "CV-P4-10 " VALVE

5400101 530010000 541000000 0.0047772 0.0 0.0 1100

5400201 1 0.0 19.6 0.0

5400300 I¶ERVLV

5400301 685 686 0.05 0.44405 540

20254000 NORIIAREA

20254001 0.0 0.0

20254002 9.25-4 9.25-4

1!B-24
20254003 1.0 1.0

*PIPE DOWNSTREAM OF STEAM CONTROL VALVE

5410000 "COND INLET" BRANCH

5410001 1 0

5410101 0.06557 54.44 0.0 0.0 0.0 0.0

5410102 4.E-5 0.0 00

5410200 0 2072970.0 914598. 2598620. .86686000

5411101 541010000 542000000 0.0 0.0 0.0 0100

5411201 13.013000 25.588000 0.0

* ------------1--------1 -------- 1 ------ 1--I------- 1--------1----

*AIR COOLED CONDENSER

5420000 "CONDENSER TMDP VOL

5420101 0.21677 17.67 0.0 0.0 0.0 0.0

5420102 4.E-5 0.02 00

5420200 2 *ICO1

54210207 0.0 2.069E6 1.0 *ICO1

* ------------1--------1-------- 1-------- 1------1--I-------1I----

*SIMPLIFIED FEED SYSTEM

*FEED STORAGE TANK

5650000 "FEED TANK" ThDP VOL

5650101 29.81 3.048 0.0 0.0 0.0 0.0

5550102 42E-5 0.0 00

5650200 3 502

5650201- 0.0 7.58E6 482.0

* ------------- 1--- ----1 --------1 --------1 ---- -- 1-I--------1 ----

*FEED WATER

5660000 "FEED " ThDPJUN

5660101 565000000 508000000 0.05

5660200 1 502

5660201 -100.0 19.150 0.0 0.0 4L2-3

5660202 0.0 19.150 0.0 0.0 *L2-3

5660203 0.5 10.0 0.0 0.0 4L2-5

5660204 1.0 2.50 0.0 0.0 *L2-5

5660205 1.5 1.00 0.0 0.0 4L2-5

5660206 2.0 0.25 0.0 0.0 4L2-5

5660207 2.5 0.00 0.0 0.0 42-5

* ECC SYSTEM

*ECC CHECK VALVE

6000000 "ECC CHKVLV" VALVE

6000101 605010000 185000000 5.9896-3 0.935 0.935 1120

6000201 0 .00000000 .00000000 0.0

6000300 TRPVLV

6000301 681

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

*ECCS HEADER TO PCS

6050000 "ECCS HEADR" SNGL VOL

6050101 5.9896-3 5.0148 0.0 0.0 90.0 3.3071202

6050102 4.0-5 0.0 00

6050200 0 4.5E+6 172410. -2459920. .00000000

B -25
*ACCUMULATOR VALVE

6100000 "ACCUII VLV "VALVE

6100101 615010000 605000000 5.9896-3 6.278

6100201 0 -.4902-15 .79206-11 0.0

6100300 TRPVLV

6100301 682

*----- ---- 1----1------1-------- 1-------- 1----

*ACCUMULATOR PIPE

6150000 "ACC PIPE "SNGL VOL

6150101 0.0 25.997165 0.4074774 0.0

6150102 4.0-5 0.0 00

6.278 1000

0.0 0.0

6150200 0 4. 5E+6 112409. 2459920. .00000000

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*ACCUMULATOR VESSEL

620000 "ACCUMULATE" ACCUII

6200101 0.0 1.8103 2.3422 0.0 -90.0 -1.8103

6200102 4.0-5 0.0 00

6200200 4.180+6 305.40

6201101 615000000 8.2132-3 40.0 40.0 0

6202200 0.0 1.0662 2.4509 1.6927 0.04445 0 0 0 0

*----- ---- 1----1------1-------- 1-------- 1-------

*BWSI LPIS

6250000 "BWST LPIS "TNDP VOL

6250101 20.44 5.0 0.0 0.0

6250102 4.OE-5 0.0 00

6250200 3

6250201 0.0 1.0+5 300.0

*LOW PRESSURE INJECTION SYSTEM

6300000 "LPIS " TMDPJUN

6300101 625000000 605000000 5.9896-3

6300200 1 504 P 605010000.

6300201 -1.0 0.0 0.0 0.0

6300202 0.0 0.0 0.0 0.0

6300203 8.483+4 7.045 0.0 0.0

6300204 4.297+5 6.091 0.0 0.0

6300205 7.745+5 5.045 0.0 0.0

6300206 9.448+5 4.313 0.0 0.0

6300207 1.119+6 3.454 0.0 0.0

6300208 1.186+6 3.173 0.0 .0.0

6300209 1.257+6 2.673 0.0 0.0

6300210 1.326+6 2.159 0.0 0.0

6300211 1.395+6 1.536 0.0 0.0

6300212 1.464+6 +0.7182 0.0 0.0

6300213 1.517+6 0.0 0.0 0.0

*------------1 --------1 --- ----1 ---- ----1---- -

*BWST HPIS

-6350000 "BWST HPIS " ThP VOL

6350101 20.44 5.0 0.0 0.0

6350102 4.OE-5 0.0 00

6350200 3

6350201 0.0 1.0+5 300.0

*----- ---- 1----1---- 1--1------ 1-------- 1--------

* HIGH PRESSURE INJECTION SYSTEM

90.0 5.0

90.0 5.0

-------------- ----1 ----

B-26
6400000 "HPIS 11 TNDP`JUN

6400101 635000000 185000000 5.9896-3

6400200 1 503 p 185010000

6400201 -1.0 0.0 0.0 0.0

6400202 0.0 1.50000000 0.0 0.0

6400203 7.72514+6 1.5 0.0 0.0

6400204 8.3597+6 .31536281 0.0 0.0

6400205 17.2436+6 .31536281 0.0 0.0

* CONTAINMENT

*------------ 1--------1 ----

*CONTAINMENT BROKEN LOOP

8000000 "CONT BLAL

8000101 0.0 1.0

8000102 0.0 0.0

8000200 2 501

8000201 0.0 1.0+5

8000202 1.0 2.1+5

8000203 1.2 1.65+5

8000204 20.0 2.9+5

8000205 24.0 2.9+5

.8000206 28.0 2.83+5

8000207 40.0 2.67+5

8000208 48.0 2.67+5

8000209 52.0 2.6+5

8000210 60.0 3.0+5

8000211 70.0 3.3+5

8000212 100.0 3.0+5

*------------ 1--------1 ----

---- 1--------1 ---- HOT LEG

TMDP VOL

0.1 0.0

00

1.0

1.0

1.0

1.0

1.0

1.0

1.0

1.0

1.0

1.0

1.0

1.0 ---- 1--------1 ----

----1------1----

----1------1----

0.0 0.0

---- 1--------1 ---- *CONTAINHENT BROKEN LOOP COLD LEG

8050000 "CONT BLCL "ThDP VOL

8050101 0.0 1.0 0.1 0.0 0.0 0.0

8050102 0.0 0.0 00

8050200 2 501

8050201 0.0 1.0+5 1.0

8050202 1.0 2.1+5 1.0

8050203 1.2 1.65+5 1.0

8050204 20.0 2.9+5 1.0

8050205 24.0 2.9+5 1.0

8050206 28.0 2.83+5 1.0

8050207 40.0 2.67+5 1.0

8050208 48.0 2.67+5 1.0

8050209 52.0 2.6+5 1.0

8050210 60.0 3.0+5 1.0

8050211 70.0 3.3+5 1.0

8050212 100.0 3.0+5 1.0

* REACTOR VESSEL HEAT STRUCTURES

" ACTIVE CORE

" STATION 116.91 TO 182.94

* HOT FUEL RODS HEAT STRUCTURE :12311

B-27
12311000 6 10 2 1 0.0 555 1 8

12311001 7.869+6

12311011 1.OE-6 2.OE-6 0.0 0.0 6

12311100 0 1

12311101 5 4.65564-3

12311102 1 4.75106-3

12311103 3 5.36806-3

12311201 1 5

12311202 -2 6

12311203 -3 9

12311301 1.0 5

12311302 0.0 9

12311401 560.0 10

12311501 0 0 0 1 56.998416 06

12311601 021010000 1000000 1 1 56.998416 06

1231.1701 900 0.02306447 0. 0. 1

12311,702 900 0.05103-4 0. 0. 2

1231.1703 900 0.05449747 0. 0. 3

12311704 900 0.0414851 0. 0. 4

12311705 900 0.02567737 0. 0. 5

12311706 900 0.0090072 0. 0. 6

12311901 0 0.013633 0.01504 1.6764 06

*AVERAGE FUEL RODS HEAT STRUCTURE :12301

12301000 6 10 2 1 0.0 555 1 8

12301001 7.869+6

12301011 1.OE-6 2.OE-6 0.0 0.0 6

12301100 0 1

12301101 5 4.65564-3

12301102 1 4.75106-3

12301103 3 5.36806-3

12301201 1 5

12301202 -2 6

12301203 -3 9

12301301 1.0 5

12301302 0.0 9

12301401 560.0 10

12301501 0 0 0 1 159.819088 06

12301601 011010000 1000000 1 1 159.819088 06

12301701 900 0.036746 0. 0. 1

12301702 900 0.0879275 0. 0. 2

12301703 900 0.0990847 0. 0. 3

12301704 900 0.0768387 0. 0. 4

12301705 900 0.0491237 0. 0. 5

12301706 900 0.0153074 0. 0. 6

12301901 0 0.013633 0.01504 1.6764 6

*INTERMIEDIATE FUEL RODS HEAT STRUCTURE :12302

12302000 6 10 2 1 0.0 555 1 8

12302001 7.869+6

12302011 1.OE-6 2.OE-6 0.0 0.0 6

12302100 0 1

B-28
12302101 5 4.65564-3

12302102 1 4.75106-3

12302103 3 5.36806-3

12302201 1 5

12302202 -2 6

12302203 -3 9

12302301 1.0 5

12302302 0.0 9

12302401 560.0 10

12302501 0 0 0 1 146.407696 06

12302601 011010000 1000000 1 1 146.407696 06

12302701 900 0.0433049 0. 0. 1

12302702 900 0.103621287 0. 0. 2

12302703 900 0.116769857 0. 0. 3

12302704 900 0.09055324 0. 0. 4

12302705 900 0.05789154 0. 0. 5

12302706 900 0.018039428 0. 0. 6

12302901 0 0.013633 0.01504 1.6764 6

* STEAM GENERATOR HEAT STRUCTURES

*TUBING

----1------1------1----

----1------1------1----

10060000 8 8 2 1 0.0051054

10060100 0 1

10060101 7 0.006348984

10060201 6 7

10060301 0.0 7

10060401 560.0 8

10060501 115010000 10000 1 1 1124.71 3

10060502 115040000 10000 1 1 849.063 5

10060503 115060000 10000 1 1 1124.71 8

10060601 515010000 10000 1 1 1124.71 3

10060602 515040000 0 1 1 849.063 4

10060603 515040000 0 1 1 849.063 5

10060604 515030000 -10000 1 1 1124.71 8

10060701 0 0 0 0 8

10060801 0 0 0 0 8

10060901 0 0 0 0 8

* HEAT STRUCTURE THERMAL PROPERTY DATA

*------------1 ------ 1--I------- 1----

20100100 TBL/FCTN 1 1

20100200 TBL/FCTN 3 1

20100300 TBL/FCTN 1 1

20100400 TBL/FCTN 1 1

20100500 C-STEEL

20100600 TBL/FCTN 1 1

*U02 - THERMAL CONDUCTIVITY

20100101 2.7315E2 8.44

20100102 4.1667E2 6.46

20100103 5.3315E2 5.782385

20100104 6.99817E2 4-.633177

20100105 8.66483E2 3.880307

*GAP

*ZR

*S-STEEL

*INCONEL 600

B-29
20100106 1.03315E3 3.357625

20100107 1. 0887IE3 3.155129

20100108 1. 19982E3 2.983787

20100109 1. 28315E3 2.836674

20100110 1. 36648E3 2.713792

20100111 1. 53315E3 2.521680

20100112 1. 61648E3 2.448990

20100113 1.69982E3 2.391875

20100114 1. 97759E3 2.2891762

20100115 2. 25537E3 2.307069

20100116 2.53315E3 2.433413

20100117 2. 81093E3 2.661870

20100118 3.08871E3 2.994171

*U02 - VOL0METIC HEAT CAPACITY

20100151 2. 73150E2 2. 310427E6

20100152 3. 23150E2 2. 571985E6

20100153 3.73150E2 2.746357E6

20100154 6. 7315E2 3. 138694E6

20100155 1. 37315E3 3 .443844E6

20100156 1.7735E3 3.531030E6

20100157 1. 97315E3 3. 792588E6

20100158 2.17315E3 4.228518E6

20100159 2. 37315E3 4. 882412E6

20100160 2.67315E3 6.015829E6

20100161 2. 7735E3 6. 320980E6

20100162 2.87315E3 6.582538E6

20100163 2.97315E3 6.713317E6

20100164 3. 11315E3 6. 805503E6

20100165 4.69982E3 6. 800503E6

*HELIUM( GAP) - THERMAL CONDUCTIVITY

20100201 HELIUMI 1.00

*HELIIJI(GAP) - VOLUMETRIC HEAT CAPACITY

20100251 273.15 5.4

20100252 5000.0 5.4

*ZIRCALOY-4 - THERMAL CONDUCTIVITY FROMI MATPRO

20100301 380.4 13.6

20100302 469.3 14.6

20100303 577.6 15.8

20100304 685.9 17.3

20100305 774.8 18.4

20100306 872.0 19.8

20100307 973.2 21.8

20100308 1073.2 23.2

20100309 1123.2 25.4

20100310 1152.3 24.2

20100311 1232.2 25.5

20100312 1331.2 26.6

20100313 1404.2 28.2

20100314 1576.2 33.0

20100315 1625.2 36.7

20100316 1755.2 41.2

20100317 2273.2 55.0

B-30
*ZIRCALOY-4 - VOLUIIETRIC HEAT CAPACITY FROM MATPR0

20100351 300.0 1.841E6

20100352 400.0 1.978E6

20100353 640.0 2.168E6

20100354 1090.0 2.456E6

20100355 1093.0 3.288E6

20100356 1113.0 3.865E6

20100357 1133.0 4.028E6

20100358 1153.0 4.709E6

20100359 1173.0 5.345E6

20100360 1193.0 5.044E6

20100361 1213.0 4.054E6

20100362 12933.0 3.072E6

20100363 1243.0 2.332E6

20100364 1477.0 2.332E6

*S-STEEL -THERMIAL CONDUCTIVITY

20100401 273.15 12.98

20100402 1199.82 25.1

*S-STEEL -VOLUMETRIC HEAT CAPACITY

20100451 273.15 3.83E6

20100452 366.5 3.83E6

20100453 477.59 4.190E6

20100454 588.59 4.336E6

20100455 699.82 4.504E6

20100456 810.93 4.639E6

20100457 922.04 4.77E6

,,20100458 1144.26 5.076E6

20100459 1366.5 5.376E6

20100460 1477.59 5.546E6

*INCONEL-600 - THERMAL CONDUCTIVITY

20100601 366.5 13.85

20100602 477.6 15.92

20100603 588.7 18.17

20100604 700.0 20.42

20100605 810.9 22.50

20100606 922.0 24.92

20100607 1033.2 26.83

20100608 1144.3 29.42

20100609 1477.6 36.06

*INCONEL-600 - VOLUMETRIC HEAT CAPACITY

20100651 366.5 3.908+6

20100652 477.6 4.084+6

20100653 588.7 4.260+6

20100654 700.0 4.436+6

20100656 810.9 4.665+6

20100657 922.0 4.929+6

20100658 1033.2 5.105+6

20100659 1477.6 5.727+6

* CONTROL VARIABLES

B-31
*001-010 LEVEL CALCULATORS

*001 STEAM GENERATOR LEVEL

20500100 SGLVL SUM 1.0 0.0 1

20500101 0.0 0.4445 VOID? 503010000

20500102 1.2131 VOID? 505010000

20500103 0.6096 VOIDF 503010000

20500104 0.6096 VOID? 510010000

20500105 0.6096 VOIDF 510020000

20500106 0.6096 VOID? 5100300010

* 002 PRESSURIZER LEVUL

20500200 PZRLVL SUM 1.0 0.0 1

20500201 0.0 0.1815 VOID? 415010000

20500202 0.1524 VOID? 415020000

20500203 0.3967 VOID? 415030000

20500204 0.5289 VOID? 415040000

20500205 0.3967 VOIDF 415050000

20500206 0.1943 VOIDF 415060000

20500207 0.1029 VOID? 420010000

20500208 0.1029 VOIDF 420020000

* 003 REACTOR VESSEL LEVEL

20500300 RVLVL SUM 1.0 0.0 1

20500301 0.0 0.84888 VOID? 260010000

20500302 0.24333 VOID? 255010000

20500303 0.9285337 VOID? 250010000

20500304 0.4933248 VOID? 245010000

20500305 0.4933248 VOID? 240010000

20500312- 0.4269792 VOID? 225010000

20500313 0.3533183 VOID? 215010000

20500314 0.3741720 VOID? 220010000

* 004 ACCUMIULATOR LEVEL

*20500400 ACCIILVL INTEGRAL -6.3480-3 2.0447 0

*20500401 VELEJ 620010000

* 007 REACTOR VESSEL DOWNCOIIER LEVEL INTACT SIDE

20500700 RVDCLVLIN SUN 1.0 0.0 1

20500701 0.0 0.3302040 VOID? 700010000

20500702 0.3951272 VOID? 702010000

20500703 1.5200561 VOID? 704010000

20500704 1.2616333 VOID? 706010000

20500705 1.0792591 VOID? 708010000

20500706 0.3533183 VOID? 215010000

20500707 0.3741720 VOID? 220010000

* 008 REACTOR VESSEL DOWNCOIIER LEVEL BROKEN SIDE

20500800 RVDCLVLBK SUN 1.0 0.0 1

20500801 0.0 0.3302040 VOID? 710010000

20500802 0.3951272 VOIDF 712010000

20500803 1.5200561 VOID? 714010000

20500804 1.2616333 VOID? 716010000

20500805 1.0792591 VOIDF 718010000

20500806 0.3533183 VOID? 215010000

20500807 0.3741720 VOID? 220010000

*CORE LEVEL :HOT CHANNEL 009, AVERAGE 010

*HOT LEVEL

20500900 HOTLVL SUN 1.0 0.0 1

20500901 0.0 0.279404 VOID? 021010000

20500902 0.0279404 VOID? 022010000

20500903 0.0279404 VOID? 023010000

20500904 0.0279404 VOID? 024010000

B-32
20500905 0.0279404 VOIDF 025010000

20500906 0.0279404 VOIDE 026010000

* AVERAGE LEVEL

20501000 HOTLVL SUM 1.0 0.0 1

20501001 0.0 0.0279404 V0IDF 011010000

20501002 0.0279404 VOIIIF 012010000

20501003 0.0279404 VOIDF 013010000

20501004 0.0279404 VOIOF 014010000

20501005 0.0279404 VOIDF 015010000

20501006 0.0279404 VOIDF 016010000

*061-072 PRIMARY SYSTEM MASS CALCULATOR

*061 INTACT LOOP HOT LEG MASS

20506100 [LHLMASS SUM 1.0 0.0

20506101 0.0 0.102752 RHO 100010000

20506102 7.57291-2 RHO 105010000

20506103 6.43178-2 RHO 110010000

20506104 7.96973-2 RHO 112010000

20506105 5.79614-2 RHO 112020000

* 062 STEAM GENERATOR PRIMARY MASS

20506200 SUPRIMASS SUM 1.0 0.0

20506201 0.0 0.335320 RHO 114010000

20506202 0.136356 RHO 115010000

20506203 9.21538-2 RHO 115020000

20506204 9.21538-2 RHO 115030000

20506205 6.99783-2 RHO 115040000

20506206 6.99783-2 RHO 115050000

20506207 9.21538-2 RHO 115060000

20506208 9.21538-2 RHO 115070000

20506209 0.136356 RHO 115080000

20506210 0.335320 RHO 116010000

* 063 PUMP SUCTION PIPING MASS

20506300 PMPSUKASS SUM 1.0 0.0

20506301 0.0 4.45625-2 RHO 118010000

20506302 4.45137-2 RHO 118020000

20506303 3.54278-2 RHO 118030000

20506304 4.87901-2 RHO 120010000

20506305 6.40548-2 RHO 125010000

20506306 1.77444-2 RHO 130010000

20506307 6.-40548-2 RHO 155010000

20506308 1.77444-2 RHO 160010000

* 064 INTACT LOOP COLD LEG MASS

20506400 ILCLMASS SUM 1.0 0.0

20506401 0.0. 9.91000-2 RHO 135010000

20506402 1.83849-2 RHO 140010000

20506403 6.33861-2 RHO 145010000

20506404 3.16011-2 RHO 150010000

20506405 9.91000-2 RHO 165010000

20506406 1.92958-2 RHO 170010000

20506407 3.54280-2 RHO 175010000

20506408 3.88950-2 RHO 17502000W

20506409 7.30598-2 RHO 180010000

20506410 6.44920-2 RHO 185010000

* 065 DOWNCOMERILOWER PLENUM MASS

20506500 DCLPNASS SUM 1.0 0.0

20506501 0.0 0.0432082 RHO 700010000

20506502 0.0578606 RHO 702010000

20506503 0.1581866 RHO 704010000

20506504 0.1217000 RHO 706010000

B-33
20506505 0.098686 RHO

20506506 0.0432082 RHO

2050650Y7 0.0578606 RHO

20506508 0.1581866 RHO

20506509 0.1217000 RHO

20506510 0.0O98686 RHO

20506511 0.24520 RHO

20506512 0.29656 RHO

* 067 CORE/UPPER PLENUMI MASS

20506700 CRUPMASS SUN 1.0

20506701 0.0 0.12094 RHO

*20506702 0.0683340 RHO

*20506703 0.0478582 RHO

*20506704 0.0483329 RHO

*20506705 0.0479138 RHO

*20506706 0.0479052 RHO

*20506707 0.0750459 RHO

20506708 0.0091280 RHO

20506709 0.0072325 RHO

20506710 0.0088095 RHO

20506711 0.1195494 RHO

20506712 0.128080 RHO

20506713 0.1436936 RHO

20506714 0.1154214 RHO

20506715 0.083595 RHO

20506716 0.310967 RHO

* 068 BROKEN LOOP HOT LEG MASS

20506800 BLHI&PkSS SUN 1.0

20506801 0.0 5.75410-2 RHO

20506802 4.42927-2 RHO

20506803 6.78467-2 RHO

20506804 7.75Z91-3 RHO

20506805 1.72111-1 RHO

20506806 8.97552-2 RHO

20506807 8.97552-2 RHO

20506808 1.72111-1 RHO

20506809 1.82303-2 RHO

20506810 5.46687-2 RHO

20506811 1.82489-2 RHO

20506812 9.15000-2 RHO

20506813 4.80000-2 RHO

20506814 4.89000-2 RHO

* 069 BROKEN LOOP COLD LEG MASS

20506900 BLCLNAS SUM 1.0

20506901 0.0 4.79790-2 RHO

20506902 4.43927-2 RHO

20506903 3.62484-2 RHO

20506904 3.10679-2 RHO

20506907 2.79000-2 RHO

20506908 7.00000-2 RHO

20506909 1.16500-1 RHO

* 070 PRESSURIZER MASS

20507000 PZRNASS SUN 1.0

20507001 0.0 3.33500-3 RHO

20507002 3.33500-3 RHO

20507003 3.33500-3 RHO

20507004 6.84000-2 RHO

20507005 8.38000-2 RHO

20507006 2.24255-1 RHO

20507007 2.98987-1 RHO

20507008 2.24255-1 RHO

708010000

710010000

712010000

714010000

716010000

718010000

215010000

220010000

0.0

225010000

821010000

822010000

823010000

824010000

825010000

826010000

235010000

235020000

235030000

240010000

245010000

250010000

251010000

255010000

260010000

0.0

300010000

305010000

310010000

315010000

315020000

315030000

315040000

315050000

315060000

315070000

315080000

380010000

380020000

380030000

0.0

335010000

340010000

342010000

344010000

370010000

370020000

370030000

1

1

0.0 1

400010000

405010000

405020000

415010000

415020000

415030000

415040000

415050000

B-34
20507009

20507010

20507011

20507012

7.32000-2 RHO

1.42000-2 RHO

1.42000-2 RHO

2.12609-3 RHO

415060000

420010000

420020000

430010000

* 071 REACTOR VESSEL TOTAL

20507100 RVMASS, SUM

20507101 0.0 1.0

20507103 1.0

* 072 PCS TOTAL MASS

MASS

1.0

CNTRL VAR

CNTRL VAR

0.0

65

67

20507200 PCSMASS SUM 1.0 0.0

20507201 0.0 1.0 CNTRLVAR 61

20507202 1.0 CNTRL VAR 62

20507203 1.0 CNTRL VAR 63

20507204 1.0 CNTRL VAR 64

20507205 1.0 CNTRL VAR 68

20507206 1.0 CNTRL VAR 69

20507207 1.0 CNTRL VAR 70

20507208 1.0 CNTRL VAR 71

*----- ---- 1----1------1-------- 1-------- 1----

*RUN STATISTICS DATA

*----- ---- 1----1------1-------- 1-------- 1----

20507800 OLDTIIIE SUM 1. 0. 0

20507801 0. 1. C.NTRLVAR 79

1

1

----1------1----

----1------1----

20507900 NEWTIME SUN

20507901 0. 1.

1.

TIME

0.

0

0

0

78

79

20508100

20508101

20508102

TSTEP

0.

SUM 1. 0.

-1. CNTRLVAR

1. CNTRVAR

*

* GENERAL TABLE DATA *

*-------------1------1------1------1------1------1----

*

*

*

*

*

TABLE

NUM'BER

* 900

20290000 POWER

20290001 -1.0

20290002 0.0

20290003 0.1

20290004 0.2

20290005 0.3

20290006 0.4

20290007 0.5

20290008 0.6

20290009 0.8

20290010 1.0

20290011 1.5

20290012 2.0

20290013 3.0

20290014 4.0

20290015 6.0

20290016 8.0

DESCRIPTION

REACTOR POWER VS TINE AFTER SCRAM

502 1.0 36.016

1.0

1.0

0.900689 *FROM L2-3 POSTTEST

0.274300

0.153171

0.110821

0.091625

0.083212

0.073556

0.062500

0. 063089

0.059854

0.057265

0.055204

0.052085

0.049776

B-35
20290017 10.0 0.047947

20290018 15.0 0.044575

20290019 20.0 0.042176

20290020 30.0 0.038783

20290021 40.0 0.036348

20290022 60.0 0.031546

20290023 1.+5 0.001460 *FROMI IR LO-08-81-173

* PUM'P DATA

*SINGLE PHASE HEAD CURVES

*HEAD CURVE NO. 1

* ------------1--------1 ----

1351100 1

1351101 0.OOOOOOE+0O

1351102 1.906100E-01

1351103 3. 896300E-01

1351104 5.939600E-01

1351105 7. 902000E-01

1351106 1. OOOOOOE+O0 --1 ---------*-- 1 ---- *HEAD CURVE NO. 2

1351200 1

1351201 0. 000000E+00

1351202 2. 000000E-01

1351203 4. 000000E-01

1351204 5. 755400E-O1

1351205 7.443200E-01

1351206 7.734800E-01

1351207 8.631300E-01

1351208 1. 000000E+00

* ------------1--------1 ----

*HEAD CURVE NO. 3

1351300 1

1351301 -1.OOOO0OOE+0O

1351302 -8. 057400E-01

1351303 -6. 069000E-01

1351304 -4. 068300E-01

1351305 -2. 001710E-01

1351306 0.OOOOOOE+00

*------------1 -------- 1 ----

*HEAD CURVE'NO. 4

1351400 1

1351401 -1.OOOOOOE+00

1351402 -8.229700E-01

1351403 -6.333200E-01

1351404 -4. 553400E-01

1351405 -2.710900E-01

1351406 -1.771600E-01

1351407 -9. 073000E-02

1351408 0.OOOOOOE+00

* 1----:l--------1 ---- *HEAD CURVE NO. 5

1351500 1

1.403600E+00

1. 363600E+00

1.318600E+00

1. 232800E+00

1. 133600E+00

1. 000000E+00

2

-6. 7000OOE-01

-5. 000000E-01

-2. 500000E-01

0.000000E+O0

2. 583000E-01

3. 77800E-01

6.326000E-01

1.OOOO0OOE+OO

3

2. 472200E+00

2. 047400E+00

1. 831000E+00

1. 624000E+00

1.470500E+00

1. 403600E+00

4

Z.472200E+00

1. 996800E+00

1. 58970E+00

1.327900E+00

1. 194900E+00

1.060500E+00

1.015600E+00

9. 342790E-01

5

B-36
1351501 0. OOOOOOE+O0 2. 5000O0E-0l

1351502 2. 000000E-Ol 2. 8000O0E -01

1351503 4.OOOOOOE-01 3.400000E-0l

1351504 4. 118000E-01 2. 768000E-01

1351505 5.976300E-01 4.584000E-O1

1351506 7.934670E-01 6.992000E-01

1351507 1.OOOOOOE+00 1. 000000E+OO

*------------1 --------1 ------ I-- ------- 1----

R EAD CURVE NO. 6

1351600 1 6

1351601 O.OOOOOOE+0O 9.342790E-01

1351602 9.109900E-02 9.229000E-01

1351603 1. 865090E-01 8. 963000E -01

1351604 2.717620E-01 8.750000E-01

1351605 4.558720E-01 8.433000E-01

1351606 5.744060E-01 8.355000E-O1

1351607 7.405760E-01 8.466000E-01

1351608 7.666190E-01 8.469000E-01

13516,09 8.714710E-01 8.838000E-01

1351610 1.OOOOOOE+0O 1.OOOOOOE+00

*----- ---- 1----1---- 1--1------ 1-------- 1----

*HEAD CURVE NO. 7

1351700 1 7

1351701 -1.O00000E+00 -1.OOOOOOE+O0

1351702 -8 .OOOOOOE-01 -6. 30O00E-01

1351703 -6. 00000E -01 -3. OOOOOOE-01

1351704 -4.OOOOOOE-01 -5.OO0000E-02

1351705 -2.000000E-O1 1. 500000E-01

1351706 0.000000E+0O 2.500000E-01

*----- ---- 1----1------1-------- 1-------- 1----

*HEAD CURVE NO. 8

1351800 1 8

1351801 -1. OOOOOOE+00 -1. OOOOOOE+00

1351802 -8.OOOOOOE-01 -9.700000E-01

1351803 -6.OOOOOOE-01 -9.500000E-01

1351804 -4.OOOOOOE-O1 -8..8000OOE-O1

1351805 -2. 000000E-01 -8. OOOOOOE-O1

1351806 O.OOOOOOE+O0 -6.7000O0E-01

*SINGLE PHASE TORQUE DATA

*TORQUE CURVE NO. 1

1351900 2 1

1351901 O.OOOOOOE+00 6.O3ZOOOE-01

1351902 1. 930000E-01 6. 325000E-01

1351903 3.930000E-01 7.369000E-01

1351904 5.955200E-01 8.331000E-01

1351905 7.978200E-O1 9.229000E-01

1351906 1.OOOOOOE+O0 1.000000E+00

*----- ---- 1----1---- 1--1------ 1-------- 1----

*TORQUE CURVE NO. 2

1352000 2 2

1352001 0.OO0OOOOE+0O -6.700000E-01

1352002 4.OOOOO`OE-O1 -2.5000O0E-01

1352003 5.OOOOOOE-01 1.500000E-01

1352004 7.372550E-O1 5.265860E-01

B-37

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----
1352005 7. 680490E-01

1352006 8. 672300E-01

1352007 1. OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 3

1352100 2

1352101 -1.OOOOOOE+00

1352102 -8.009600E-O1

1352103 -6. 063800E-01

1352104 -4. 068600E-01

1352105 -1.992800E-01

1352106 O.OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 4

1352200 2

1352201 -1.000000OE+00

1352202 -8. 223400E-01

1352203 -6. 337100E-O1

1352204 -4. 585300E-01

1352205 -2. 670230E-01

1352206 -1. 761070E-01

1352207 -8. 931000E-02

1352208 0. OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 5 *----------- 17--- ----1 ----

1352300 2

1352301 .0.OOOOOE+00

1352302 4.OOOOOOE-01

1352303 5. 0OO000E-01

1352304 1.OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 6

1352400 2

1352401 0.000000E+00

1352402 9. 064300E-02

1352403 1. 885690E-01

1352404 2. 734700E-01

1352405 4. 586690E-01

1352406 5.744800E-01

1352407 7. 381600E-O1

1352408 7.685200E-01

1352409 8. 700570E-01

1352410 1. 00000E+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 7

1352500 2

1352501 -1.OOOOOOE+00

1352502 -3. OOOOOOE-O1

1352503 -1. OOOOOOE-01

1352504 0.000000E+00

* ------------1--------1 ----

*TORQUE CURVE NO. 8

1352600 2

1352601 -1.OOOOOOE+OO

135Z602 -2. 5000O0E-01

6 .065940E-01

7.436600E-O1

1.000000E+O0

3

1.984300E+00

1. 394000E+00

1.097500E+00

8. 220000E-O1

6. 648000E-01

6.032000E-01

4

1. 98430E+O

1. 830800E+00

1.682400E+OO

1. 557000E+00

1.436200E+00

1. 387900E+00

1. 348100E+00

1. 233610E+00

-4. 5000O0E-01

-2. 500000E-01

O0.OOOOOOE+00

3.569000E-01

6

1. 233610E+00

1. 196500E+00

1. 109600E+00

1.041600E+00

8. 958000E-O1

7.W87000E-01

6. 134000E-O1

5.849000E-01

4. 877000E-O1

3. 569000E-01

7

-1. 000000E+0

-9. OOOOOOE-O1

-5. OOOOO4JE-01

-4. 500000E-01

-1.000000OE+00

-9 .OOOOOOE-01

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1---

B-38
1352603 -8.000000E-02 -8.000000E-01

1352604 0. OOOOOOE+00 -6. 7000O0E-01

*TWO - PHASE MIULTIPLIER DATA FROMI L3-6 TEST DATA

*------------ 1--------1 ----

*HEAD CURVE

1353000 0

1353001 0. OOOOOOE+00

1353002 1.OOOOOOE-O1

1353003 2 .OOOOOOE-01

1353004 3.OOOOOOE-01

1353005 3.5OOOOOE-01

1353006 4. OOOOOOE -01

1353007 5.'OOOOOOE-01

1353008 6.OOOOOOE-01

1353009 7. OOOOOOE-01

1353010 8.OOOOOOE-01

1353011 9.OOOOOOE-01

1353012 1.OOOOOOE+00

*-----------I-1--- ---- 1I----

*TORQUE CURVE

1353100 0

1353101 0.OOOOOOE+00

1353102 1.OOOOOOE-01

1353103 2.OOOOOOE-01

1353104 3.OOOOOOE-01

1353105 3. 5000OOE-01

1353106 4.OOOOOOE-O1

1353107 5. 000000E-01

1353108 6. 000000E-01

1353109 7.OOOOOOE-01

1353110 8. OOOOOOE-01

1353M1 9.OOOOOOE-01

1353112 1.000000E+00

*PUMP 2-PHASE DIFFERENCE

*HEAD CURVE NO. 1

1354100 1

1354101 0.000000E+OO

1354102 1.000000E+00

* ------------1--------1 ----

*HEAD CURVE NO. 2

1354200 1

1354201 0. 000000E+00

1354202 1.OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 3

1354300 1

1354301 -1.OOOO0OOE+00

1354302 -9. OOOOOOE-01

1354303 -8. OOOOOOE -01

1354304 -7.000000E-01

1354305 -6. OOOOOOE-01

1354306 -5. 00000E -01

1354307 -4. 00000E -01

0. 000000E+00

0. 000000E+O0

1.OOOOOOE-01

3. 000000E-01

6. OOOOOOE-01

6. 000000E-01

6. OOOOOOE-01

6. 0000010E-01

5.OOOOOOE-01

3. 000000E+00

0. OOOOOOE+00

0. OOOOOOE+00

0.OOOOOOE+00

1. 000000E-O1

3. OOOOOOE-01

75. OOOOOE -01

7. 500000E-01

7. 5000OOE-01

7. 500000E-01

7. 500000E-01

5. OOOOOOE -01

0. 000000E+00

DATA

1. 00000E+00

1. 00000E+00

2

1. 000000E+00

1.OOOOOOE+0O

3

-1. 160000E+OO

-1. 240000E+00

-1. 770000E+00

-2. 360000E+00

-2. 790000E+00

-2. 91OOOOE+00

-2. 670000E+OO

B-39

----1------1----

----1------1----

----1------1----

----1------1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----
1354308 -2.500000E-Ol

1354309 -1.OOOOOOE-O1

1354310 0. OOOOOOEfOO

*HEAD CURVE NO. 4

1354400 1

1354401 -1.OOOOOOE+OO

1354402 -9.OOOOOOE-O1

1354403 -8.OOOOOOE-O1

1354404 -7.OOOOOOE-O1

1354405 -6.OOOOOOE-O1

1354406 -5.OOOOOOE-O1

1354407 -3. 500000E-O1

1354408 -2.OOOOOOE-O1

1354409 -1.OOOOOOE-01

1354410 0. OOOOOOE+00

*------------1 -------- 1 ----

R EAD CURVE NO. 5

1354500 1

1354501 0. OOOOOOE+00

1354502 2. OOOOOOE-O1

1354503 4.OOOOOOE-01

1354504 6.OOOOOOE-01

1354505 8.OOlOOOOE-01

1354506 1. OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 6

1354600 1

1354601 0.OOOOOOE+00

1354602 1.OOOIOOOE-O1

1354603 2. 500000E-O1

1354604 4. OOOOOOE-O1

1354605 5.OOOOOOE-O1

1354606 6.OOOOOOE-01

1354607 7.OOOOOOE-01

1354608 8.OOOOOOE-01

1354609 9. OOOOOOE-01

1354610 1.O0OOOOOE+OO

* ------------1--------1 ----

*HEAD CURVE NO. 7

1354700 1

1354701 -1.OOOOOOEI-00

1354702 0. OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 8

1354800 1

1354801 -1. OOlOOOOE+0O

1354802 O.OOOOOOE+00

* ---- ------ ---1------1-....

*TORQUE CURVE No. 1

1354900 2

1354901 0.00000E4OOE0

1354906 1. 000000E+O0

* ------------1--------1 ----

* TORQUE CURVE NO. 2

-1. 690000E+00

-5. 000000E-01

0. 000000E+00

4

-1. 160000E+0

-7. 8000OOE-01

-5.O0O0O0E-01

-3. 100000E-01

-1. 700000E -01

-8. OOOOOOE-02

0. 0OO00OE+0

5.00OOCOOE -02

8. OOOOOOE-02

1. 10000E-01

0.OO0OOOOE+O0

-3.400000E-O1

-6. 500000E-01

-9. 300000E-01

-1. 190000E+00

-1.470000E+00

6

1. 10000E-O1

1. 30000E-01

1. 5000OOE-01

1. 3000OOE-01

7.OOCOOOE-02

-4. OOOOOOE-02

-2. 3000OOE-01

-5. 100000E-01

-9. 100000E -01

-1. 470000E+OO

7

0.OOOOOOE+00

0. OOOOOOE+00

0.OOOOOOE+0O

1O00000E+00

B-40
* -- -- 1 -- -- 1 ----

1355000 2

1355001 O.OOOOOOE+00

1355007 1.000000E+00

*TORQUE CURVE NO. 3

1355100 2

1355101 -1.OOOOOOE+OO

1355102 -8. 009600E-01

1355103 -6. 063800E-01

1355104 -4. 068600E-01

1355105 -1. 992800E-01

1355106 0. 000000E+00

*TORQUE CURVE NO. 4

1355200 2

1355201 -1.0O0000E+00

1355202 -8. 223400E-01

1355203 -6. 337100E-01

1355204 -4. 585300E -01

1355205 -2. 670230E-01

1355206 -1. 761070E-01

1355207 -8. 931000E-02

1355208 O.OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 5

1355300 2

1355301 O.OOOOOOE+0O

1355302 4.OOOOOOE-01

1355303 5. 000000E-01

1355304 1.000000E400

* ------------1--------1 ----

*TORQUE CURVE NO. 6

1355400 2

1355401 0.OOOOOOE+O0

1355402 9.064300E-02

1355403 1 .885690E-01

1355404 2.734700E-01

1355405 4.586690E-01

1355406 5.744800E-01

1355407 7. 381600E-01

1355408 7-685200E-01

1355409 8. 700570E-01

1355410 1.OOOOOOE+0O

*------------ 1--------1 ----

*TORQUE CURVE NO. 7

1355500 2

1355501 -1.DOOOOOE+OO

1355502 -3. 000000E-O1

1355503 -1.OOOOOOE-O1

1355504 0. OOOOOOE+OO

* ------------1--------1 ----

*TORQUE CURVE NO. 8

1355600 2

1355601 -1. 000000E+00

2

1.OOOOOOE+00

1. OOOOOOE+O0

3

1. 984300E+00

1. 394000E+00

1. 097500E+00

8. 220000E-01

6. 648000E -01

6. 032000E -01

4

1. 984300E+00

1. 830800E+00

1. 682400E+00

1. 557000E+00

1.436200E4-00

1. 387900E+00

1. 348100E+00

1. 233610E+00

5

-4. 500000E-O1

-2. 5000OOE-01

0. OOOOOOE+0O

3.569000E-01

6

1.233610E+00

1. 196500E+00

1. 109600E+00

1. 041600E+00

8. 958000E-01

7. 807000E-01

6. 134000E-01

5 .849000E-O1

4.877000E-01

3. 569000E-01

7

-1. OOOOOOE+OO

-9. 000000E-01

-5. OOOOOOE-01

-4. 500000E-01

8

-1.000000OE+00

B-41I

----1------1----

----1------1----

----1------1----

----1---- ----1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1---

----1------1----

----1------1----
1355602 -2. 500000E-01 -9. 000000E-01

1355603 -8. 000000E-02 -P . 00000E-01

1355604 0. OOO0OO0E+0O -6. 700000E-Ol

*$$$ REMOVE ALL REMAINING DATA~CARDS AFTER ACHIEVING STEADY STATE

* PUMP DATA

*SINGLE PHASE HEAD CURVES

*HEAD CURVE NO. 1

* ------------1--------1 ----

1651100 1

1651101 0.000000E+00

1651102 1.9061O0E-01

1651103 3. 896300E-O1

1651104 5.939600E-01

1651105 7. 9020O0E-01

1651106 1.OOOOOOE+00

* ---- ------ ---1------1-..--

*HEAD CURVE NO. 2

1651200 1

1651201 0.OOOOOOE+0O

1651202 2.OOOOOOE-01

1651203 4.OOOOOOE-O1

1651204 5. 7554O0E-01

1651205 7.443200E-O1

1651206 7.734800E-01

1651207 8. 631300E-01

1651208 1. 000000E+00

* ------------1--------1 ----

*HEAD CURVE NO. 3

1651300 1

1651301 -1. OOOOOOE+00

1651302 -8. 0574O0E -01

1651303 -6. 069000E-01

1651304 -4.068300E-01

1651305 -2 .001710E-01

1651306 0.OOOOO0E+00 --- --- 1--------1 ----

*HEAD CURVE NO. 4

1651400 1

1651401 -1. OOOOOOE+00

1651402 -8. 229700E-01

1651403 -6. 333200E-01

1651404 -4. 553400E-01

1651405 -2.710900E-01

1651406 -1. M16DOE-01

1651407 -9. 073000E-02

1651408 0. 000000E+00

* ----- 1 -------- 1 ----

*HEAD CURVE NO. 5

1651500 1

1651501 0.000000E+O0

1651502 2.000000E-O1

1651503 4.O00000E-01

1I.403600E+00

1. 363600E+00

I.318600E+00 1.2328O0E+00

1. 133600E+00

1.000000OE+00

-6. 700000E-01

-5 .OOOOOOE-01

-2*.500000E-01

0. 000000E+O0

2. 583000E-01

3. 778000E-01

6.326000E-O1

1. OOOOOOE+00

3

2.472200E+00

2. 047400E+00

S.6241000E+00

1 1.470500E+00 831000E+00

'.403600E+00

4

2. 472200E+O0

11. 996800E+00

11. 589700E+00

11. 327900E+00

11. 194900E+00

,1. 060500E+00

11.015600E+00

9.342790E-01

5

2. 5000OOE-01

ý2.800000E-01

,3.4000O0E-01

B-42

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----
1651504 4. 118000E-01 2. 768000E-O1

1651505 5.976300E-01 4.584000E-O1

1651506 7.934670E-01 6.992000E-01

1651507 1.000000E+0O 1.OOOOOOE+O0

*HEAD CURVE NO. 6

1651600 1 6

1651601 0. 000000E+00 9. 342790E-01

1651602 9. 109900E-02 9. 229000E-01

1651603 1.865090E-01 8.963000E-O1

1651604 2.717620E-01 8.750000E-01

1651605 4.558720E-01 8.433000E-01

1651606 5.744060E-01 8.3550'OE-01

1651607 7.405760E-01 8.466000E-01

1651608 7.666190E-01 8.469000E-O1

1651609 8.714710E-01 8.&38000E-01

1651610 1. OOOOOOE+O0 1.OOOOOOE+0O

R EAD CURVE NO. 7

1651700 1 7

1651701 -1.OOOOOOE+00 -1.OO0OOOOE+O0

1651702 -8. OOOOOOE-01 -6. 300000E-O1

1651703 -6.0OO0000E-01 -3. OOOOOOE -01

1651704 -4.OOOOOOE-01 -5.OOOOOOE-02

1651705 -2. OOOOOOE-01 1. 500000E-O1

1651706 O.OOOOOOE+0O 2.500000E-O1

*READ CURVE NO. 8

1651800 1 8

1651801 -1. OOOOOOE+00 -1. OOOOOOE+O0

1651802 -8.OOOOOOE-O1 -9.7000O0E-O1

1651803 -6.OOOOOOE-O1 -9. 500000E-O1

1651804 -4.OOOOOOE-O1 -8.800000E-O1

1651805 -2.OOOOOOE-01 -8.OOOOOOE-O1

1651806 0. OOOOOOE+OO -6. 700000E-O1

*SINGLE PHASE TORQUE DATA

*TORQUE CURVE NO. 1

1651900 2 1

1651901 0. 000000E+00 6. 032000E-O1

1651902 1. 930000E-O1 6. 325000E-01

1651903 3. 930000E-01 7. 369000E-O1

1651904 5. 955200E-01 8. 331000E-01

1651905 7.978200E-O1 9.229000E-O1

1651906 1.OOOOOOE+OO 1.000000E+0O

*TORQUE CURVE NO. 2

1652000 2 2

1652001 0. OOO0OOOE+0O -6. 7000O0E-01

1652002 4. OOOOOOE-O1 -2. 500000E-O1

1652003 5. OOOOOOE-O1 1. 5000OOE-01

1652004 7.372550E-01 5.265860E-O1

1652005 7.680490E-01 6.065940E-01

1652006 8.672300E-O1 7.436600E-01

1652007 1. OOOOOOE+00 1. 000000E+OO

B-43
*TORQUE CURVE NO. 3

1652100 2

1652101 -1.OOOOOOE+OO

1652102 -8.009600E-01

1652103 -6. 063800E-01

1652104 -4. 068600E -01

1652105 -1. 992B00E-01

1652106 0. OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 4

1652200 2

1652201 -1.OOOOOOE4AOO

1652202 -8. 223400E-O1

1652203 -6. 337100E-01

1652204 -4. 585300E-01

1652205 -2. 670230E-01

1652206 -1. 761070E-01

1652207 -8. 931000E-02

1652208 O.OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 5

1652300 2

1652301 0. OOOOOOE+00

1652302 4.OOOOOOE-01

1652303- 5. OOOOOOE-01

1652304 1.OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 6

1652400 2

1652401 0. OOOOOOE+0O

1652402 9. 064300E-02

1652403 1. 885690E -01

1652404 2.734700E-01

1652405 4. 586690E-01

1652406 5.744800E-01

1652407 7.381600E-01

1652408 7.685200E-01

1652409 8. 700570E-01

1652410 1.OOOOOOE+0O

* ------------1--------1 ----

*TORQUE CURVE NO. 7

1652500 2

1652501 -1.OOOOOOE+00

1652502 -3. OOOOOOE-01

1652503 -1.OOOOOOE-01

1652504 0.OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 8

1652600 2

1652601 -1.OOOOOOE+00

1652602 -2.5OOOOOE-01

1652603 *-8.OOOOOOE-02

1652604 0. OOOOOOE+0O

*------------ 1--------1 ----

3

1. 98400E00O

1.394000E+00

1. 097500E+00

8. 220000E-01

6. 648000E-01

6. 032000E-O1

4

1. 994300E+00

1. 830800E+00

1.682400E+00

1. 557000E+00

1. 436200E+00

1. 387900E+00

1. 348100E+00

1. 23361OE+O0

5

-4. 500000E-01

,-2. 500000E-01

0.OOOOOOE+00

3. 569000E-01

6

1. 233610E+00

1.196500E+00

1. 109600E+00

1. 041600E+00

8.958000E-01

7. 807000E-01

6. 134000E-O1

5. 849000E-01

4. 877000E-01

3.569O00E-01

7

-1. OOOOOOE+0O

-9.OOOOOOE-01

-4500OOOOE-01

8

-1. OOOOOOE+0O

-9. OOOOOOE-01

-8. OOOOOOE-01

-6. 700000E-01

B-44
*TWO - PHASE MULTIPLIER DATA FROM L3-6 TEST DATA

*HEAD CURVE

* ------------1--------1 ----

1653000 0

1653001 O.OOOOOOE+00

1653002 1.OOOOOOE-01

1653003 2. 000000E-01

1653004 3. OOOOOOE-01

1653005 3.5ODOOCE-01

1653006 4. OOOOOOE -01

1653007 5. OOOOOOE-01

1653008 6.000000E-01

1653009 7.000000E-01

1653010 8.OOOOOOE-01

1653011 9. OOOOOOE-01

1653012 1. OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE

1653100 0

1653101 0.OOOOOOE+00

1653102 1.OOOOOOE-O1

1653103 2.000000E-O1

1653104 3. 000000E-01

1653105 3.500000E-01

1653106 4.OOOOOOE-O1

1653107 5. 000000E-01

1653108 6. OOOOOOE-O1

1653109 -7.OOOOOOE-01

1653110 8.000000E-01

1653111 9.OOOOOOE-01

1653112 1.OOOOOOE+O0

*PUMP 2-PHASE DIFFERENCE

*HEAD CURVE NO. 1

1654100 1

1654101 0. 000000E+O0

1654102 1.000000E+00

*------------1 -------- 1 ----

*HEAD CURVE NO. 2

1654200 1

1654201 O.OOOOOOE+00

1654202 1 .OOOOOOE+00

*------------1 -------- 1 ----

*HEAD CURVE NO. 3

1654300 1

1654301 -1.OOOOOOE+00

1654302 -9.OOOOOOE-01

1654303 -8. OOOOOOE -01

1654304 -7.000000E-01

1654305 -6. OOOOOOE-O1

1654306 -5. OOOOOOE-01

1654307 -4.OOOO00E-O1

1654308 -2. 500000E -01

1654309 -1.OOOOOOE-01

1654310 0.OOOOOOE+00

----1------1------1------1----

O.OOOOOOE+00

0. OOOOOOE+00

1. 00000E -01

2. 00000E -01

3. 000000E-01

6. OOOOOOE-01

6. OOOOOOE-01

6. OOOOOOE-01

6. 00000E -01

5. 000000E-01

3. OOOOOOE-01

0. OOOOOOE+00 --1 -------- 1 ---- ----1------1----

----1------1------1------1----

0. 000000E+00

0. OOOOOOE+00

1. OOOOOOE-O1

3. OOOOOOE-01

5. OOOOOOE-01

7. 500000E -01

7. 5000OOE-01

7. 500000E-01

7. 5000O0E-01

7. 500000E-01

5 .OOOOOOE-01

0. OOOOOOE+00 --------- DATA ----1------1----

----1------1------1------1----

1. 000000E+00

1. OOOOOOE+O0

2

1.OOOOOOE+00

1. 000000E+00

----1------1----

----1------1----

----1------1----

----1------1----

3

-1. 160000E+0O

-1. 240000E+00

-1.770000E+OO

-2. 36O000E+0O

-2. 790000E+O0

-2. 910000E+00

-2. 670000E+00

-1. 690000E+00

-5. 00000E -01

0. OOOOOOE+00

B-45
*HEAD CURVE NO. 4

1654400 1

1654401 -1.OOOOOOE+O0

1654402 -9.OOOOOOE-01

1654403 -8. OOOOOOE-01

1654404 -7.)OOOOOE-01

1654405 -6. OOOOOOE-01

1654406 -5.000000E-O1

1654407 -3. 5000O0E -01

1654408 -2. 00000E -01

1654409 -1.OOOOOOE-01

1654410 0.OOOOOOE+00O

*HEAD CURVE NO. 5

1654500 1

1654501 O.OOOOOOE+00

1654502 2.OOOOOOE-01

1654503 4.OOOOOOE-01

1654504 6.000000E-O1

1654505 8. OOOOOOE-01

1654506 1.OOOOOOE+00

* -----------1--------1 ----

*HEAD CURVE NO. 6

1654600 1

1654601 0. OOOOOOE+00

1654602 1.OOOOOOE-01

1654603 2. 5000O0E-0l

1654604 4.OOOOOOE-O1

1654605 5.OOOOOOE-01

1654606 6. OOOOOOE-01

1654607 7.OOOOOOE-01

1654608 8. OOOOOOE-O1

1654609 9.OOOOOOE-01

1654610 1. OOOOOOE+00

* -----------1--------1 ----

*HEAD CURVE NO. 7

1654700 1

1654701 -1.OOOOOOE+0O

1654702 0.OOOOOOE+OO

* -----------1--------1 ----

*HEAD CURVE NO. 8

1654800 1

1654801 -1.000000E+00

1654802 0. OOOOOOE+00

* -----------1--------1 ----

*TORQUE CURVE NO. 1

1654900 2

1654901 0.OOOOOOE+00

1654906 1.OOOOOOE+OO

* -----------1--------1 ----

*TORQUE CURVE NO. 2

1655000 2

1655001 0. 000000E+00

4

-1. 160000E+00

-7.8000OOE-01

-5. OOOOOOE-01

-3. 10000E-O1

-1. 7000OOE-01

-8. OOOOOOE-02

O.OOOOOOE+0O

5. OOOOOOE-02

8. OOOOOOE-02

1. 100000E -01

0. OOOOOOE+00

-3 .400000E-01

-6. SOOOOOE-01

-9. 300000E-O1

-1. 19O000E+OO

-1.470000E+00

6

MO10000E-O1

1. 3000O0E-01

1. 500000E-01

1. 300000E-01

7. OOOOOOE-02

-4.O0O0O0E-02

-2. 300000E-01

-5. 100000E-01

-9. 100000E-01

-1. 470000E+00

7

0. OOOOOOE+00

0. 000000E+O0

0. OOOOOOE+00

1.OOOOOOE+00

,2

1. OOOOOOE+00

B-46

----I-------1----

----1------1----

----1------1----

----1------1----

----1---- --- 1----

----1------1----

----1----

----1----

----1----

----1----

---- 1---

---- 1---

----1----

----1----

----1----

----1----

----1----

----1----*

---- 1---

----1----

--- 1----

----1----
1655007 l.OOOOOOE400

*TORQUE CURVE NO. 3

1655100 2

1655101 -1.000000E+00

1655102 -8. 009600E-O1

1655103 -6. 063800E-01

1655104 -4. 068600E-01

1655105 -1. 992800E -01

1655106 0. OOOOOOE+00

* ------------1---- --- 1I----

*TORQUE CURVE NO. 4

1655200 2,

1655201 -1. OOOOOOE+0O

1655202 *-8. 223400E -01

1655203 -6. 337100E-01

1655204 -4. 585300E-O1

1655205 -2. 670230E-01

1655206 -1. 761070E -01

1655207 -8. 931000E-02

1655208 0.OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 5

1655300 2

1655301 O.OOOOOOE+0O

1655302 4. OOOOOOE-O1

1655303 5. OOOOOOE -01

1655304 1. OOOOOOE+00

* ------------1--------1 ----

*TORQUE CURVE NO. 6

1655400 2

1655401 0. OOOOOOE+00

1655402 9 .064300E -02

1655403 1. 885690E-01

1655404 2. 734700E -01

1655405 4. 586690E -01

1655406 5.744800E-O1

1655407 7.381600E-O1

1655408 7. 685200E-01

1655409 8. 700570E -01

1655410 1. OOOOOOE+0O

* ----------------- ---- 1 ----

*TORQUE CURVE NO. 7

1655500 2

1655501 -1.OOOOOOE+OO

1655502 -3.OOOOOOE-01

1655503 -1.OOOOOOE-O1

1655504 O.OOOOOOE+OO

* ------------- 1--- ---- 1 ----

*TORQUE CURVE NO. 8

1655600 2

1655601 -1. 000000E+00

1655602 -2. 500000E-01

1655603 -8. 00000E -02

1655604 0. OOOOOOE+00

1. OOOOOOE+00

3

1. 984300E+00

1. 394000E+00

1. 097500E+00

8. 220000E-01

6. 648000E -01

6. 032000E-O1

----1------1----

----1------1----

----1------1----

4

1. 984300E+00

1.830800E+00

1. 682400E+00

1. 557000E-1-0

1. 436200E+00

1. 387900E+00

1. 348100E+00

1. 233610E+00

5

-4. 500000E-O1

-2. 500000E-01

0. OOOOOOE+00

3. 569000E-01 --1-------1-----

6

1. 233610E+00

1.196500E+00

1. 109600E+00

1. 041600E+00

8.958000E-01

7. 8070O0E-01

6. 134000E-01

5. 849000E-01

4. 877000E-01

3. 569000E-O1

7

-1. OOOOOOE+OO

-9.DOOOOOE-01

-5.OOOOOOE-O1

-4. 500000E-O1

8

- . OOOOOOE-01

-8. OOOOOOE-O1

-6. 7000OOE-01

----1------1----

----1------1----

----1------1----

----1------1----

B-47
* STEADY STATE CONTROL SYSTEM

*PRIMARY COOLANT PUMP SPEED CONTROLLERS

*CALCULATE MASS FLOW ERROR

20590100 NSSERR SUM 1.0 0.0 1

20590101 199.00 -1.0 MFLOWJ 100010000

*------------ 1------1--I------- 1----

*PUMP 1 SPEED

20590200 PCP1SPD INTEGRAL 0.34482 133.000 1

20590201 CNTRL VAR 901

*----- ---- 1----1------1-------- 1----

*PUPi PUMP VELOCITY TABLE

1356100 510 CNTRL VAR 902

1356101 0.0 0.0

1356102 369.0 369.0

*----- ---- 1----1------1-------- 1----

*MODIFY PCP1 PUMP DATA

1350301 0 0 0 -1 0 695 0

*----- ---- 1----1------1-------- 1----

*PUMP 2 SPEED *---- ---- 11------1 ---- -----1 ----

20590300 PCP2SPD INTEGRAL 0.34482 139.790 1

20590301 CNTRL VAR 901

*----- ---- 1----1------1-------- 1----

*PCP2 PUMP VELOCITY TABLE

*----- ---- 1----1------1 -------- 1----

1656100 510 CNTRL VAR 903

1656101 0.0 0.0

1656102 369.0 369.0

*----- ---- 1----1------1-------- 1----

*MODIFY PCP2 PUMP DATA

1650301 0 0 0 -1 0 697 0

* ---- ---- 1-----1------1-------- 1-------- 1-------- 1-------- 1----

*PRESSURIZER SPRAY VALVE CONTROLLER

*SPRAY LINE

4300000 "SPRAY "BRANCH

4300001 1 0

4300101 0.0003363 6.322 0.0 0.0 90.0 2.9905

4300102 4.0-5 0.0 00

4300200 0 15037900. 123820. 2459550. .00000000

4301101 150000000 430000000 0.0 0.0 0.0 0000

4301.201 .777018-4 .777018-4 0.0

* ----- 1 -----1 -------- 1 -------- 1 -------- 1 -------- 1 ----

*SPRAY VALVE

4350000 "SPRVLV "VALVE

4350101 430010000 415010000 3. 3451E-4 1. 5432E01 1. 5432E01 0100

4350201 0 .00000000 .00000000 0.0

4350300 SRVVLV

B-48
4350301 904 999

*SPRAY VALVE POSITION CALCULATOR

20590400 SPRAY sum -1.0 0.0

+1 3 0.0 1.0

20590401 15.06+6 -1.0 p 420010000

*----- ---- 1----1------1-------- 1----

*POSITION VS AREA TABLE

20299900 NORIAREA

20299901 0.0 0.0

20299902 0.0001 0.0

20299903 1.0 1.0

*------------1 -------- 1-------- 1------1--I------

*PRESSURIZER HEATERS IN INITIALIZATION

*PRESSURIZER HEATER TRIPS

* T 693 CYLCING HEATERS CARD 20241700

0000585 P 420010000 GT NULL 0

0000586 P 420010000 LT NULL 0

0000666 586 OR 693 N

0000667 -585 AND 666 N

0000693 -503 AND 667 N

* T 694 BACKUP HEATERS CARD 20241800

0000587 P 420010000 GT NULL 0

0000588 P 420010000 LT NULL 0

0000668 588 OR 694 N

0000669 -587 AND 668 N

0000694 -503 AND 669 N

1 * CONTIN

15.06+6 N

15.0599+6 N

15.01+6 N

15.0099+6 N

* ------------1--------1 -------- 1 ------ 1--I------- 1--------1----

*PRESSURIZER HEATERS

14172000 2

14172100 0

14172101 8

14172201 4

14172301 1.0

14172401 615.0

14172501 0

14172502 0

14172601 415040000

14172602 415040000

14172701 417-

14172702 418

14172901 0

14172902 0

9

1

8. 3820E-3

8

8

9

0

0

0

0

1.0

1.0

1.6764E-2

1.6764E-2

2 1 0.0

0 1

0 1

0.0 0.0

0.0 0.0

1.6764E-2 5.4864

1.6764E-2 1.8288

5.4864

1.8288

5.4864

1.8288

1

2

1

2

1

2

1

2

" CYCLING

" BACKUP

*PRESSURIZER CYCLING HEATERS

20241700 POWER 693

20241701 0.0 0.0

20241702 1.0 3.6+4

*----- ---- 1----1------1--------1I----

*PRESSURIZER BACKUP HEATERS

20241800 POWER 694

20241801 0.0 0.0

20241802 1.0 1.2+4

----1------1------1----

----1------1------1----

----1------1------1----

B -49
*PRESSURIZER LEVEL CONTROL USING CHARGING AND LETDOWN COMPONENTS

M ODIFY PZR LEVEL CONTROL VARIABLE

20500206 0.1249 VOIDF 415060000

20500207 0.02477 VOIDF 420010000

20500208 0.02477 VOIDF 420020000

*----- ---- 1----1------1-------- 1----

*CHARGING RESERVIOR

9800000 "CHRG RESRV'f TMbDP VOL

9800101 1.0 1.*0 0.0 0.0 0.0 0.0

9800102 4.0-5 0.0 00

9800200 3

9800201 0.0 2.07+07 559.2

*----- ---- 1----1------1-------- 1----

*CHARGING VALVE

9850000 "CHRG VALVE" VALVE

9850101 980000000 185000000 3.8E-05 0.0 0.0 0100

9850201 0 .608458-3 .608458-3 0.0

9850300 SRVVLV

9850301 905 999

*----- ---- 1----1------1-------- 1----

*CHARGING VALVE POSITION CALCULATOR

20590500 CHARGE SUMI 7.7 0.0 1 *CONTIN

+ 3 0.0 1.0

20590501 1.18 -1.0 CNTRLVAR 2

*----- ---- 1----1------1-------- 1----

*LETDOWN SINK

9900000 ,LTnwN SINK TMDP VOL

9900101 1.0 1.0 0.0 0.0 0.0 0.0

9900102 4.0-5 0.0 00

9900200 3

9900201 0.0 1.4+7 559.2 --l--------11- --------1 ----

*LETDOWN VALVE

9950000 vLinwN VLV it VALVE

9950101 185000000 990000000 2.5-5 0.0 0.0 0100

9950201 0 .00000000 .00000000 0.0

9950300 SRVVLV

9950301 906 999

*LETDOWN VALVE POSITION CALCULATOR

20590600 LETDOWN suN -7.7 0.0 1 *CONTIII

+ 3 0.0 1.0

20590601 1.1430 -1.0 CNTRLVAR 2

*----- ---- 1----1---- 1--1------ 1-------- 1---- --- 1---- --- 1----

*STEAM VALVE CONTROLLER

*CHANGES TO STEAM VALVE

5400201 0 13.604000 13.604000 0.0

5400300 SRVVLV`

5400301 910 540

20254000 NORIIAREA

B-50
20254001 0.0 0.0

20254002 0.0001 0.0

20254003 1.0 1.0

* COMPUTE DELTA T ERROR

* -- --1 ----- 17--- ---- 1I----

20590700 "DELTA T" SUN 1.0 0.0

20590701 560.7 -1. TENPF 185010000

*----- ---- 1----1------1-------- 1----

*FILTER DELTA T THRU DEADBAND

20590800 DEADBAND FUNCTION 1.0 0.0

20590801 CNTRL VAR 907 908

20290800 REAC-T

20290801 -100. -100.

20290802 -0.1 -0.1

20290803 -0.1 0.0

20290804 0.1 0.0

20290805 0.1 0.1

20290806 100. 100.

*----- ---- 1----1------1-------- 1----

*INTEGRATE DELTA T ERROR

20590900 "INT D T" INTEGRAL 1.0 0.0

20590901 CNTRL VAR 908

*----- ---- I----1------1-------- 1----

*STEAM VALVE POSITION CALCULATOR

20591000 TCONTROL SUM 1.0 0.44405

+ 3 0.40 0.55

20591001 0.44405 -0.0564 CNTRIVAR 908

20591002 -0.0059 CNTRL VAR 909

*----- ---- 1----1------1-------- 1-------- 1--------

*SIMPLIFIED FEED SYSTEM CONTROLLER

*SIMPLIFIED FEED LOGIC

20591100 SOLVLERR SUM 1.0 0.0

20591101 3.11 -1.0 CNTRLVAR 001

20591200 FEEDFLOW SUM 1.0 0.0

20591201 0.0 1.0 MFLOWJ 540000000

20591202 48.4 -CNTRL VAR 911

*----- ---- 1----1------1-------- 1----

*REPLACE FEED JUNCTION TABLE

5660200 1 0 CNTRL VAR 912

5660201 -100.0 19.15 0.0 0.0

5660202 -1.0 0.0 0.0 0.0

5660203 0.0 0.0 0.0 0.0

5660204 50.0 50.0 0.0 0.0

5660205

5660206

5660207

*----- ---- 1----1------1-------- 1-------- 1--------

*REPLACE REACTOR POWER TABLE

.. RELAP5 END . CARD

1

1

1

0 *CONTI

1

1

1------1----

1------1----

B-51

Appendix C. A Base Case Input Deck for a Transient Calculation

L23BTR2,T5000.

/USER

ATTACH,RSTIN=L23R2.

ATTACH,STH2XT,RE364BX.

DEFINE, RSTPLT=L23RSTT.

FILE,RSTIN,SBF=NO.

FILE, RSTPLT, SBF=NO.

*DEFINE ,PL0TFL=L23HPLO.

RFL,CM=300000,EC=200.

REDUCEH(-

RE364BX, ,*PL=50000.

/EOR

= LOFT L2-3 BASE TRANSIENT TO 100 SEC

0000100 RESTART TRANSNT

0000101 RUN

0000103. 5237

0000105 5.0 10.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

0000201 20.0 1.0-6 0.05 3 2 200 1000

0000202 100.0 1.0-6 0.01 3 10 500 2500

*REMOVE PUMIP SPEED CONTROLLERS

*---------100 ----- 1--D-L -1---.0 -1.0 0 --. 1------1----

20590100 NC~SSER DELETE 0.0 0.0 0.0 0.0 0.0 0.0

20590200 PCP1SPD DELETE 0.0 0.0 0.0 0.0 0.0 0.0

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*RENODALIZE PUMPi

1350000 llPcPUI'P 1 " PUMP

1350101 0.0 0.4572 0.0991 0.0 90.0 0.3171

1350102 0

1350108 130010000 0.0 0.017 0.017 0000

1350109 140000000 0.0 0.05 0.05 0000

1350200 0 1.49288+7 1.23094+6 2.46151+6 0.

1350201 0 3.0790 3.0790 0.0

1350202 0 3.2641 3.2641 0.0

1350301 0 0 0 -1 -1 0 0

1350302 369.00000 .35501355 .31550000 96.000000 500.60000 1.43Y(

1350303 613.60000 .00000000 207.43300 .04440000 19.598700 . 0000

1350310 0.0 0.0 0.0

*PUMP DATA

~0

)000

)000

*----- ---- 1----1------1-------- 1--------1I----

*SINGLE PHASE HEAD CURVES

*HEAD CURVE NO. 1

1351100 1 1

1351101 O.OOOOOOE+00 1.403600E+00

1351102 1.9061OOE-01 1.363600E+00

1351103 3.89630E-01 1.318600E+00

1351104 5.939600E-01 1.232800E+00

1351105 7.902000E-01 1. 133600E+00

1351106 1. OOOOOOE+00 1. OOOOOOE+OO

*----- ---- 1----1------1-------- 1--------1I----

R EAD CURVE NO. 2

1351200 1 2

1351201 0. OOOOOOE+00 -6. 700000E-01

1351202 2.OOOOOOE-01 -5.OOOOOOE-01

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

C-1
1351203 4.OOOOOOE-O1

1351204 5.755400E-01

1351205 7.443200E-O1

1351206 7.734800E-O1

1351207 8. 631300E-01

1351208 1. 000000E+O0

* ------------1--------1 ----

*HEAD CURVE NO. 3

1351300 1

1351301 -1.OOOOOOE+00

1351302 -8. 057400E-01

1351303 -6. 06900CE-01

1351304 -4. 058300E-01

1351305 -2 .001710E-01

1351306 0.OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 4

1351400 1

1351401 -1.OOOOOOE+00

1351402 -8. 229700E-01

1351403 -6. 333200E-01

1351404 -4. 553400E-O1

1351405 -2.710900E-01

1351406 -1. 771600E-01

1351407 -9.073000E-02

1351408 0.00000E4OOE0

* ------------1--------1 ----

*HEAD) CURVE NO. 5

1351500 1

1351501 0.000000E+OO

1351502 2.OO0OOOOE-01

1351503 4. OOOOOOE-01

1351504 4. 118000E-01

1351505 5. 976300E-01

1351506 7.934670E-01

1351507 1.OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 6

1351600 1

1351601 O.OOOOOE+00

1351602 9. 109900E-02

1351603 1.865090E-01

1351604 2. 717620E-01

1351605 4:* 558720E-01

1351606 5. 744060E-01

1351607 7. 405760E-01

1351608 7. 666190E-01

1351609 8.714710E-01

1351610 1.000000E+O0

* ---- --- 1--------1 ----

*HEAD CURVE NO. 7

1351700 1

1351701 -1.OOOOOOE+00

1351702 -8. OOOOOOE-01

1351703 -6. OOOOOOE-01

1351704 -4.OOOOOOE-01

1351705 -2.OOOOOOE-01

1351706 0. OOOOOOE+00

-2. 500000E-01

O.000000E+0O

2. 583000E-01

3. 778000E-01

6. 326000E-01

1.000000E+00

3

2.0474200E+00

1.831000E+00

1. 624000E+00

1.47050E+00

1.403600E+00

----1------1----

----1------1------1------1----

4

2.472200E+00

1. 996800E+00

1. 589700E4-00

1. 327900E+00

1. 194900E+00

1. 060500E+00-

1.015600E+00

9. 342790E-01

5

2. 500000E-O1

2.800000E-01

3. 40000E-01

2.768000E-01

4. 584000E-01

6.992000E-01'

1.OOOOOOE+0O

6

9. 342790E-01

9. 229000E-O1

8. 963000E-01

8.750000E-01

8. 433000E-01

8. 355000E -01

8. 466000E-01

8.469000E-01

8.8800E-01

1. 000000E+0O

7

-1 .OOOOOOE+0O

-6. 300000E -01

-3. OOOOOOE-01

-5. OOOOOOE-02

1. SOOOOOE-01

2. 500000E-O1

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

C-2
*HEAD CURVE NO. 8

1351800 1 8

1351801 -1.OOOOOOE+OO -L.OOOOOOE+OO

1351802 -8.000000E-O1 -9.700000E-01

1351803 -6.000000E-O1 -9. 5000OOE-01

1351804 -4. OOOOOOE -01 -8. 800000E-0l

1351805 -2. OOOOOOE-O1 -8. 000000E-01

1351806 O.0OOOOOOE+00 -6.700000E-01

*SINGLE PHASE TORQUE DATA

*TORQUE CURVE NO. 1

1351900 2 1

1351901 0. OOOOOOE+00 6 .032000E-01

1351902 1.930000E-O1 6.325O00E-01

1351903 3. 930000E-01 7. 369000E-01

1351904 5. 955200E-01 8.331000E-01

1351905 7.978200E-01 9.229000E-01

1351906 1. OOOOOOE+00 1. OOOOOlOE+00

*TORQUE CURVE NO. 2

1352000 2 2

1352001 0 .OO0OOOOE+0O -6. 700000E-O1

1352002 4. 000000E-O1 -2. 5000OOE-01

1352003 5.OGOOOOOE-01 1. 5000O0E-01

1352004 - 7. 372550E-01 5. 26586OE-01

1352005 7.680490E-01 6.06594OE-01

1352006 8.672300E-01 7.436600E-O1

1352007 1. OOOOOOE+00 1. OOOOOOE+0O

*TORQUE CURVE NO. 3

1352100 2 3

1352101 -1.000000E+OO 1.984300E+00

1352102 -8. 009600E-01 1. 394000E+00

1352103 -6. 063800E-01 1. 097500E+00

1352104 -4.068600E-01 8.220000E-O1

1352105 -1.992800E-01 6.648000E-01

1352106 O.OOOOOOE+OO 6.032000E-01

*TORQUE CURVE NO. 4

1352200 2. 4

1352201 -1.OOOOOOE+OO 1.984300E+00

1352202 -8.223400E-01 1.830800E+00

1352203 -6.337100E-O1 1.682400E+00

1352204 -4. 585300E-01 1. 557000E+00

1352205 -2. 670230E-01- 1.436200E+00

1352206 -1.761070E-01 1.387900E+00

1352207 -8.931000E-02 1.348100E+00

1352208 O.OOOOOOE+OO 1.233610E+00

*TORQUE CURVE NO. 5

1352300 2 5

1352301 0. OOOOOOE+OO -4. 5000OOE-01

1352302 4. OOOOOOE-01 -2. 500000E-01

1352303 5.OOOOOOE-01 0.000000E+O0

1352304 1. 000000E+00 3. 569000E-01

c-3
*TORQUE CURVE NO. 6

1352400 2

1352401 0. OOOOOOE+OO

1352402 9. 064300E -02

1352403 1.885690E-01

1352404 2.734700E-01

1352405 4. 586690E-01

1352406 5.744800E-01

1352407 7.381600E-01

1352408 -7. 685200E-01

1352409 8. 700570E-01

1352,410 1.OOOOOOE±00

*------------ 1--------1 ----

*TORQUE CURVE NO. 7

1352500 2

1352501 -1.000000E+00

1352502 -3. OOOOOOE-O1

1352503 -1. OOOOOOE-O1

1352504 0. OOOOOOE+0O

* ------------1--------1 ----

*TORQUE CURVE NO. 8

1352600 2

1352601 -1.OOOOOOE+00

1352602 -2. 500000E-01

1352603 -8. 000000E-02

1352604 0 .OOOOOOE+0O

*------------ 1--------1 ----

----1------1------1------1----

6

1. 233610E+00

1. 196500E+00

1. 109600E+00

1. 041600E+00

8.958000E-01

7. 807000E-O1

6. 134000E-O1

5. 849000E-01

4. 877000E-01

3. 569000E-01

7

-1. OOOOOOE+O0

-9. OOOOOOE-01

-5. OOOOOOE-O1

-4. 500000E-01

8

-1. OOOOOOE+OO

-9. OOOOOOE-01

-8. OOOOOOE-01

-6. 700000E-01 --1 -------- 1 ----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

----1------1----

* TWO - PHASE MIULTIPLIER DATA FROM1 L3-6 TEST DATA

*------------ 1--------1 ----

*HEAD CURVE

1353000 0

1353001 0. OOOOOOE+00

1353002 1. OOOOOOE-01

1353003 2. 000000E-01

1353004 3.OOOOOOE-01

1353005 3. 500000E-01

1353006 4. 000000E-01

1353007 5.000000E-01

1353008 6.OOOO0OOE-O1

1353009 7.OOOOOOE-01

1353010 8. 000000E-01

1353011 9.OOOOOOE-01

1353012 1.OOOOOOE+00

*------------1 -------- 1 ----

*TORQUE CURVE

1353100 0

1353101 O.OOOOOOE+00

1353102 1.OOOOOOE-01

1353103 2.000000E-01

1353104 3.000000E-01

1353105 3. 500000E-01

1353106 4.000000E-01

1353107 5.000000E-01

1353108 6.000000E-01

1353109 7.000000E-01

1353110 8. 00000E -01

1353111 9. 00000E -01

----1------1------1------1----

----1------1------1------1----

0. OOOOOOE+Oo

0.OOOO0OOEI-00

1.OOOO00E-01

2. 000000E-01

3. 000000E-01

6.OO0O0OE-01

6. 000000E-01

6.OOOOOOE-01

6. 000000E-01

5. 000000E-01

3. 000000E-01

O .00000E+0O --1 -------- 1 ---- ----1------1----

0.OOOOOOE+00

0.OOOOOOE+Oo

1.OOOOOOE-01

3.OOOOOOE-01

75.000000E-01

7.5000O0E-01

7. 500000E-01

7.500000E-01

7. 500000E-01

7. 500000E-01

C-4
M.33112 1.OOOOOOE+OO

*PUMP 2-PHASE DIFFERENCE

*HEAD CURVE NO. 1

1354100 1

1354101 0.000000E+00

1354102 1.OOOOOOE+O0

*------------ 1--------1 ----

*HEAD CURVE NO. 2

1354200 1

1354201 0.OOOOOOE+00

1354202 1. OOOOOOE+00

* ------------1--------1 ----

*HEAD CURVE NO. 3

1354300 1

1354301 -1. 00000E+OO

1354302 -9. OOOOOOE-01

1354303 -8. OOOOOOE -01

1354304 -7.000000E-01

1354305 -6. 000000E-01

1354306 -5. 000000E-01

1354307 -4. 000000E-O1

1354308 -2. 5000O0E-01

1354309 -1.OOOOOOE-01

1354310 0. OOOOOOE+00

*------------ 1--------1 ----

*HEAD CURVE NO. 4

1354400 1

1354401 -1. 000000E+00

1354402 -9. 000000E-01

1354403 -8.OOOOOOE-01

1354404 -7. OOOOOOE-01

1354405 -6. OOOOOOE-01

1354406 -5. OOOOOOE-01

1354407 -3. 500000E-01

1354408 -2.OOOOOOE-O1

1354409 -1.OOOOOOE-01

1354410 0. OOOOOOE+00

*------------ 1--------1 ----

*HEAD CURVE NO. 5

1354500 1

1354501 O.OOOOOOEI-00

1354502 2. 000000E-01

1354503 4.OOOOOOE-01

1354504 6.OOOOOOE-O1

1354505 8.0OOOOOE-O1

1354506 1.OOOOOOE+00

* ------------- 1--- ---- 1 ----

*HEAD CURVE NO. 6

1354600 1

1354601 0. OOOOOOE+00

1354602 1.OOOIOOOE-01

1354603 2. 500000E-01

1354604 4.000000E-01

1354605 5. 000000E-01

1354606 6. OOOOOOE-01

0. 000000E+00

DATA

1.OOOOOOE+00

1.OOOOOOE+00

2

1.OOOOOOE+00

1.OOOOOOE+Oo

3

-1. 160000E+00

-1. 240000E+00

-1. 770000E+00

-2. 360000E+00

-2. 790000E+O0

-2. 910000E+00

-2. 670000E+00

-1. 690000E+00

-5. OOOOOOE -01

0.OOOOOOE+00

4

_1. 160000E+OO

-7. 800000E-01

-5. 000000E-01

-3. 100000E-01

-1. 700000E-O1

-8. OOOOOOE-02

0. 000000E+00

5.OOOOOOE-02

8. OOOOOOE-02

5

0.OOOOOOE+00

-3. 400000E-01

-6. 5000OOE-01

-9. 300000E-01

-1. 190000E+00

-1.470000E+OO

6

1.300000E-01

1. 500000E-01

1. 300000E-01

7. 000000E-02

-4. OOOOOOE-02

C-5
1354608 8.000000E-01

1354609 9.OOGOOOOE-O1

1354610 1.OOOOOOE+00

*HEAD CURVE NO. 7

1354700 1

1354701 -1. OOOOOOE+0O

1354702 0.000000E+0O

* -- -- 1 ---1---1---

*HEAD CURVE NO. 8

1354800 1

1354801 -1.000000E~-LO

1354802 O.00000E.L00

* ------------1---- --- 1I----

*TORQUE CURVE NO. 1

1354900 2

1354901 0.000000Ek00

1354905 1.000000E+00

* ------------1---- -- 1-I----

*TORQUE CURVE NO. 2

1355000 2

1355001 0. OOOOOOE+00

1355007 1.000000E+00

* ------------1--------1 ----

*TORQUE CURVE NO. 3

1355100 2

1355101 -1. OOOOOOE+00

1355102 -8. 009600E-01

1355103 -6. 063800E-01

1355104 -4. 068600E-O1

1355105 -1.992B00E-01

1355106 0. 000000E+00

* ------------1--------1 ----

*TORQUE CURVE NO. 4

1355200 2

1355201 -1.OOOOOOE+00

1355202 -8. 223400E-O1

1355203 -6. 337100E-O1

1355204 -4. 585300E-O1

1355205 -2.670230E-01

1355206 -1. 761070E-01

1355207 -8. 931000E-02

1355208 0.OOOOOOE+00

*------------ 1--------1 ----

TO~RQUJE CURVE NO. 5

1355300 2

1355301 0. 000000E+00

1355302 4.OOOOOOE-01

1355303 5.000000E-01

1355304 1.000000E400

* ------------1--------1 ----

*TORQUE CURVE NO. 6

1355400 2

1355401 0. OOOOOOE+00

-f.. %)uubMJUL

-5. 100000E-01

-9. 100000E-01

-1 .470000E+00

7

0. OOOOOOE+00

O . 00000E+0O

8

O .OOOOOOE+00

0. OOOOOOE+00

1.OOOOOOE+OO

1. OOOOOOE+OO

1.OOOOOOE+00

1. 000000E+00

1. 9843E+00

1.6824000E+00

1.5509700E+00

81.432200E+00

6.3648100E+00

64.50300OOE-01

12.59400E+OOE0

1. 830800E+00

1.538900OE+01

1.6 80E0

1. 233610E+00

---- C-- 16 -

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

----1----

---1----

----1----

----1----

----1----

----1------1----

----1------1----

----1------1----

---1------1---

----1------1----

----1------1----
iJbAUZJ 9).0Ib4300E -02

1355403 1. 885690E -01

1355404 2.734700E-01

1355405 4. 586690E-01

1355406 5.744800E-01

1355407 7. 381600E -01

1355408 7. 685200E-01

1355409 8.700570E-01

1355410 1. OOOOOOE+00

*------------ 1--------1 ----

*TORQUE CURVE NO. 7

1355500 2

1355501 -1. OOO0OOE+O0

1355502 -3.OOOOOOE-01

1355503 -1. OOOOOOE-01

1355504 0. 000000E+00

* ------------1--------1 ----

*TORQUE CURVE NO. 8

1355600 2

1355601 -1. OOOOOOE+00

1355602 -2. 500000E-O1

1355603 -8. OOOOOOE -02

1355604 0.OOOOOOE+O0

* ------------1--------1 ----

*RENODALIZE PUMP 2

1650000 "PCPUMP2 "

1650101 0.0 0.514

1650102 0

1. 196500E+00

1. 109600E+00

1. 041600E+00

8. 958000E-01

7. 807000E-01

6. 134000E-01

5. 849000E-01

4. 877000E-01

3. 569000E-O1

7

-1. O00000E+00

-9. OOOOOOE-01

-5. OOOOOOE -01

-4. 5000G0E -01

8

-1. OOOOOOE+00

-9. OOOOOE -01

-8. 000000E-01

-6. 7000O0E-01

PUMP'

0.0991 0.0

----1------1----

----1------1----

----1------1----

----1------1----

----1---- ----1----

----1------1----

90.0 0.317900

1650108 160010000 0.0 0.017 0.017 0000

1650109 170000000 0.0 0.1 0.1 0000

1650200 0 1.49287+7 1.23094+6 2.46151+6 0.

1650201 0 3.4623 3.4623 0.0

1650202 0 3.5798 3.5798 0.0

1650301 135 135 135 -1 -1 0 0

1650302 369.00000 .36859079 .31550000 96.000000 500.60000 1.4310000

1650303 613.60000 .00000000 207.43300 .04440000 19.598700 .00000000

1650310 0.0 0.0 0.0

* ------------1--------1 --------1 ------ 1--I------- 1--------1----

*REMOVE S PRA Y LINE, SPRAY VALVE, AND CALCULATOR

4300000---1----1--------1----1----1TE

4300000 SPRAYV DELETE

20590400 SPRAY DELETE 0.0 0.0 0.0 0.0 0.0 0.0

*------------ 1-~-------1 --------1 --------1 ------ 1--I-------1---- *RENODALIZE PRESSURIZER MASS CALCULATOR

20507000 PZRMASS SUM 1.0 0.0 1

20507001 0.0 3.33500-3 RHO 400010000

20507002 3.33500-3 RHO 405010000

20507003 3.33500-3 RHO 405020000

20507004 6.84000-2 RHO 415010000

20507005 8.38000-2 RHO 415020000

20507006 2.24255-1 RHO 415030000

20507007 2.98987-1 RHO 415040000

20507008 2.24255-1 RHO 415050000

20507009 7.32000-2 RHO 415060000

20507010 1.42000-2 RHO 420010000

20507011 1.42000-2 RHO 420020000

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

* REPLACE PRESSURIZER BACKUP/CYCLING HEATERS POWER TABLE

C-7
- - a & uUAJ%09%LUA* 11LAn±LA-ur fUf rxb.

* INSTEAD OF REMOVING PRESSURIZER HEAT STRUCTURE CO1IPNENTS

20241700 POWER 693

20241701 0.0 0.0

20241702 1.0 0.0

20241800 POWER 694

20241801 0.0 0.0

20241802 1.0 0.0

* -----------1--------1 -------- 1 -------- 1 -------- 1--------1----

* REMOVE PRESSURIZER LEVEL CONTROLLERS, CHARGING COMPONENT, AND

" LETDOWN COMPONENT

* -----------1--------1 -------- 1 ------ 1--I------- 1--------1----

20500200 PZRLVL SUIM 1.0 0.0 1

20500201 0.0 0.1815 VOIDF 415010000

20500202 0.15Z4 VOIOF 415020000

20500203 0.3967 VOIDF 415030000

20500204 0.5289 VOIDF 415040000

20500205 0.3967 VOIDF 415050000

20500206 0.1943 V0IDF 415060000

20500207 0.1029 VOIDF 420010000

20500208 0.1029 VOIDF 420020000

9800000 "CHRG R" DELETE

9850000 "CHEG V"t DELETE

20590500 CHARGE DELETE 0.0 0.0 0.0 0.0 0.0 0.0

9900000 "LTDWN S" DELETE

9950000 "LTDWN V" DELETE

20590600 LETDOWN DELETE 0.0 0.0 0.0 0.0 0.0 0.0

* -----------1--------1 --------1 --------1 ------ 1--I-------1---- *REMOVE STEAM VALVE CONTROLLER

5400000 "C V-P4-10 "VALVE

5400101 530010000 541000000 0.0047772 0.0 0.0 0100

5400201 0 14.541 13.536 0.0

5400300 MTRVLV

5400301 685 686 0.05 .416170 540

20254000 NORMAREA

20254001 0.0 0.0

20254002 9.25-4 9.25-4

20254003 1.0 1.0

20590700 "DELTA T" DELETE 0.0 0.0 0.0 0.0 0.0 0.0

20590800 DEADHAND DELETE 0.0 0.0 0.0 0.0 0.0 0.0

20590900 "INT D T" DELETE 0.0 0.0 0.0 0.0 0.0 0.0

20591000 TCONTROL DELETE 0.0 0.0 0.0 0.0 0.0 0.0

20290800 DELETE

*----- ---- 1--1------ 1---- -- 1--I-------1 -------- 1--- 1----J-

*REMOVE FEED SYSTEM CONTROLLER

2059----1 ------ 1------1------1------1------1.0-0.

20591100 SGLVLERR DELETE 0.0 0.0 0.0 0.0 0.0 0.0

5660000 "FEED it TMDPJIJN

5660101 565000000 508000000 0.05

5660200 1 502

5660201 -100.0 19.150 0.0 0.0 4L2-5

5660202 0.0 19.150 0.0 0.0 4L2-5

5660203 0.5 10.0 0.0 0.0 4L2-5

5660204. 1.0 2.50 0.0 0.0 4L2-5

5660205 1.5 1.00 0.0 0.0 4L2-5

5660206 2.0 0.25 0.0 0.0 42Z-5

5660207 2.5 0.00 0.0 0.0 4-

*REPLACE TRIPS FOR L2-3 TRANSIENT

* -----------1--------1-------- 1-------- 1-------- 1--------1----

C-8
0000501

0000502

0000503

0000504

TIME

TIME

TIME

TIME

0

0

0

0

GE

GE

GE

GE

NULL 0

NULL 0

NULL 0

NULL 0 ---- 1----

0.0 L * BRFEAKJOPEN

0.103 L * REACTOR SCRAM

14.0 N * HPIS STRAT

29.0 N * LPIS START

*------------1 --------1 ----

*------------ 1--------1 ----

*MINOR EDIT VARIABLES ---- 1----

0000301

0000302

0000303

0000304

0000305

0000306

0000307

0000308

0000309

0000310

0000311

0000312

0000313

0000314

0000315

0000316

0000317

0000318

0000319

0000320

0000321

0000322

0000323

0000324

0000325

0000326

0000327

0000328

0000329

0000330

0000331

0000332

0000333

0000334

0000335

0000336

0000337

0000338

0000339

0000340

0000341

0000342

0000343

0000344

0000345

0000346

0000347

0004

0000349

0000350

0000350

0000351

0000352

0000353

p

P

TEMPF

TEMPF

MFLOWJ

MFLOWJ

RHO

RHO

RHO

RHO

RHO

MFLOWJ

MFLOWJ

MFLOWJ

IIFLOWJ

CNTRL VAR

PMPVEL

P 101

VOIDGJ

VOIDGJ

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CNTRL VAR

CPUTIME

MFLOWJ

MFLOWJ

NFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

MFLOWJ

VOIDG (

VOIDG

VOIDO

VOIDGC

VOIDGC

VOIDG 22

VOIDG 24

25001

53001'

25001

21501'

34001

30501

10001'

34001'

30501

18501

18001'

6300001

6400001

600001

610001

4

135

0010004

3170001

347000'

2

1

7

8

9

10

12

59

60

71

72

75

77

81

0

180010(

185010(

01000(

731000

WOO00

724000

726000(

728000

T19000(

~25010

25020

~25030

)21010

)23010

)25010(

)13010(

)15010(

~50100(

~00100(

---- 1--------1 --------1 --------1 ---- 0000 - PRIMARY PRESSURE PE-1UP-001

0000 * SECONDARY PRESSURE

0000 * UPPER PLENUM TEMP.

0000 * LOWER PLENUM TEMP.

0000 * BLCL MASS FLOW

0000 * BLHL MASS FLOW

0000 * ILHL DENSITY

0000 * BLCL DENSITY

0000 * BLHL DENSITY

0000 * ILCL DENSITY

0000 * PUMhP EXIT DEN.

000 * LPSI MASS

000 * HPSI

0000 * ECC MASS

000 .* ACCUII MASS FLOW

ACCUMULATOR LEVEL

* PUMP 1 SPEED

0* ILHL PRESSURE

00 * HlL BREAK JUNC VOID

000 * CL BREAK JUNC VOID

* PZR LEVEL

*S/G LEVEL

" DC LEVEL (INTACT)

" DC LEVEL (BROKEN)

" HOT CORE LEVEL

" AVER CORE LEVEL

" TOTAL COLLAPSED LEVEL

" AVERAGE CORE MASS

" HOT CORE MASS

" CORE MASS

" PCS TOTAL MASS

" TOTAL INJECTED MASS

" TOTAL DISCHARGED MASS

" TIME STEP SIZE

000

)0

)000

)0

)00

)00

)0

)00

)0

)00

)00

100

)00

)00

)0

)00

)00

10

10

" PUMP DISCHAGE MASS

" ILCL MASS FLOW

" DC UPPER ANNDLUS MASS

" DC DOWNWARD MASS

" CROSS FLOW 1

" CROSS FLOW 2

" CROSS FLOW 3

" CROSS FLOW 4

" BR.SIDE DC DOWNWARD MASS

" AVER CORE MASS FLOW

" HOT CORE MASS FLOW

" CORE BYPASS FLOW

*

*

*

*

*

*

*

HOT CH 5 INCH VOID

HOT CH 28 INCH VOID

HOT CH 39 INCH VOID

AVER CH 28 INCH VOID

AVER CH 39 INCH VOID

LOWER PLENUM VOID

UPPER PLENUM VOID

C-9
0000355 HTTENP 231100110 * TE-5H5-002

0000356 HTTEMP 231100210 * TE-5J9-005

0000357 HTTENP 231100310 * TE-518-008

0000359 HTTEMP 231100410 * TE-5J7-011

0000360 HTTEMP 231100510 * TE-5H5-015

0000361 HTTEMP 231100610

0000362 HITEMP 230100110

0000363 HTTEMP 230100210 * TE-4E8-011

0000364 IITTEMP 230100310 * TE-4F7-015

0000365 HTTEMP 230100410 * TE-4G8-021

0000366 HTTEMP 230100510 * TE-4F8-028

0000367 HTTEMP 230100610 * TE-4F8-032

0000368 TEMPF 712010000 * TE-1ST-001

0000369 TEMPF 714010000

0000370 TEIIPF 716010000

0000371 TEIIPF 718010000

0000372 TENPF 225010000

* ACCUMULATOR, TRIPS, AND CONTROL VARIABLE

*ACCUMULATOR VALVE TRIPS

0000579 HFLOWJ 610000000 GE NULL 0 0.0 N

0000580- CNTRLVAR 4 LT NULL 0 1.0 L

0000682 579 AND -580 N

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*ACCUMULATOR LEVEL CONTROL VARIABLE

20500400 ACCIILVL INTEGRAL -4.776E-3 2.04 0

20500401 VELF.J 610000000

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*ECC CHECK VALVE

6000000 "EGG CHKVLV" VALVE

6000101 605010000 185000000 0.0 1.3869 1.3869 0100

6000201 0 0.0 0.0 0.0

6000300 TRPVLV

6000301 681

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*ECCS HEADER TO PCS

6050000 "ECCS HEADR" SNGL VOL

6050101 5.989E-3 4.8247 0.0 0.0 90.0 2.2061

6050102 1.0165-5 0.0 10

6050200 0 4.18E+6 125472. 2600290. 0.0

* ------------1------1--I------- 1--------1 -------- 1 -------- 1----

*ACCUMULATOR VALVE

6100000 "ACCUM VLV ' ~ VALVE

6100101 615010000 605000000 0.0 8.1009 8.1009 0000

6100201 0 0.0 0.0 0.0

6100300 TRPVLV

6100301 682

* ------------1--------1 ------ 1--I------- 1--------1 -------- 1----

*ACCUMULATOR PIPE

6150000 "ACC PIPE "SNGL VOL

c-1 0
6150101 0.01608 24.5486 0.0 0.0 0.0 0.0

6150102 1.0165-5 0.0 10

6150200 3 4.18E+6 303.2

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

*ACCUMULATOR VESSEL

6200000 "ACCUMULATR" ACCUM

6200101 1.254 1.8261563 0.0 0.0 -90.0 -1.8261563

6200102 2.286-5 0.0 10

6200200 4.18E+6 303.2

6201101 615000000 8.213E-3 40.0000 40.0000 0

6202200 1.45 0.0 4.0251 0.67056 0.04445 0 0 0 0

*----- ---- 1----1------1-------- 1-------- 1-------- 1--------1I----

*ZIRCALOY-4 - THERMAL CONDUCTIVITY FROM MATPRO

20100300 TBL/FCTN 1 1

20100301 300.0 12.68

*20100301 380.4 13.6

20100302 469.3 14.6

20100303 577.6 15.8

20100304 .685.9 17.3

20100305 774.8 18.4

20100306 872.0 19.8

20100307 973.2 21.8

20100308 1073.2 23.2

20100309 1123.2 25.4

20100310 1152.3 24.2

20100311 1232.2 25.5

20100312 1331.2 26.6

20100313 1404.2 28.2

20100314 1576.2 33.0

20100315 1625.2 36.7

20100316 1755.2 41.2

20100317 2273.2 55.0

*---------l------ ---1 I--------1 --------1 --------1 --------1 ----

*ZIRCALOY-4 - VOLUMETRIC HEAT CAPACITY FROM MATPRO

20100351 300.0 1. 841E6

20100352 400.0 1.978E6

20100353 640.0 2.168E6

20100354 1090.0 2.456E6

20100355 1093.0 3.288E6

20100356 1113.0 3.865E6

20100357 1133.0 4.028E6

20100358 1153.0 4.709E6

20100359 1173.0 5.345E6

20100360 1193.0 5.044E6

20100361 1213.0 4.054E6

20100362 1233.0 3.072E6

20100363 1243.0 2.332E6

20100364 1477.0 2.332E6

*----- ---- 1----1------1-------- 1

*PLOT EDIT REQUEST

*----- ---- 1----1------1-------- 1-------- 1-------- 1-------- 1----

20300100 P 250010000 * PRIMARY PRESSURE PE-1UP-001

20300200 P 530010000 * SECONDARY PRESSURE

20300300 TEMPE 250010000 * UPPER PLENUM TEMP.

20300400 TEMPF 215010000 * LOWER PLENUM TEMP.

20300500 MFLOWJ 340010000 * BLCL MASS FLOW

20300600 IIFLOWJ 305010000. * BLAL MASS FLOW

20300700 RHO 100010000 * ILHL DENSITY

20300800 RHO 340010000 * BLCL DENSITY

20300900 RHO 305010000 * BLIII DENSITY

C-1 I
tijU.JU±UU

20301100

20301200

20301300

20301400

20301500

20301600

20301700

20301800

20301900

20302000

20302100

20302200

20302300

20302400

20302500

20302600

20302700

20302800

20302900

20303000

20303100

20303200

20303300

20303400

20303500

20303600

20303700

20303800

20303900

20304000

20304100

20304200

20304300

20304400

20304500

20304600

20304700

20040

20304900

203049000

203051000

20305100

20305200

20305300

20305400

20050

20305500

20305600

20305700

203058000

20305900

.203062000

20060

20306100

20306200

20306300

20306400

20306500

20306600

RHO 180010000 *PUMP EXIT DEN.

NFLOWJ 630000000 * PSI MASS

MFLOWJ 640000000 *HPSI

IIFLOWJ 600000000 *ECC MASS

MFLOWJ 610000000 *ACCUM MASS FLOW

CNTRL VAR 4 *ACCUMULATOR LEVEL

PMPVEL 135 * PUMP 1 SPEED

P 100010000 * ILHL PRESSURE

VOIDGJ 317000000 * HL BREAK JUNG VOID

VOIDGJ 347000000 * CL BREAK JUJNG VOID

CNTRL VAR Z * PZR LEVEL

CNTRL VAR 1 *SIG LEVEL

CNTRL VAR 7 * DC LEVEL (INTACT) CNTRLVAR 8 * DC LEVEL (BROKEN)

CNTRL VAR 9 * HOT CORE LEVEL

CNTRLVAR 10 * AVER CORE LEVEL

CNTRLVAR 12 * TOTAL COLLAPSED LEVEL

CNTRLVAR 59 * AVERAGE CORE MASS

CNTRLVAR 60 * HOT CORE MASS

CNTRLVAR 71 * CORE MASS

CNTRLVAR 72 * PCS TOTAL MASS

CNTRLVAR 75 * TOTAL INJECTED MASS

CNTRLVAR 77 * TOTAL DISCHARGED MASS

CNTRLVAR 81 * TIME STEP SIZE

CPUTIME 0

MFLOWJ 180010000 * PUMP DISCHAGE MASS

MFLOWJ 185010000 * ILUL MASS FLOW

[IFLOWJ 701000000 * DC UPPER ANNULUS MASS

MFLOWJ 731000000 * DC DOWNWARD MASS

NFLWJ 722000000 * CROSS FLOW 1

MFLOWJ 724000000 * CROSS FLOW 2

MFLOWJ 725000000 * CROSS FLOW 3

MFLOWJ 728000000 * CROSS FLOW 4

?IFLOWJ 719000000 * BR.SIDE DC DOWNWARD MASS

MFLOWJ 225010000 * AVER CORE MASS FLOW

ILFLOW3 225020000 * HOT CORE MASS FLOW

NFLOWJ 225030000 * CORE BYPASS FLOW

VOIDG

VOIDG

VOIDG

VOIDG

VOIDG

VOIDG

VOIDG

HITEMP

HTTEMP

HTTEMP

HTTEMP

HTTEMP

HTTEMP

HTTEMP

HTTEMP

HITEEMP

HTTEMP

HTTEIIP

HTTEMP

TENPF

TEMPF

TENPF

021010000

023010000

025010000

013010000

015010000

225010000

240010000-

231100110

231100210

231100310

231100410

231100510

231100610

230100110

230100210

230100310

230100410

230100510

230100610

712010000

714010000

716010000

*

*

*

*

*

*

*

HOT CH 11 INCH VOID

HOT CH 21 INCH VOID

HOT CHi 45 INCH VOID

AVER CH 21 INCH VOID

AVER CHi 45 INCH VOID

LOWER PLENUM VOID

UPPER PLENUM VOID

" TE-5H5-002

" TE-5J9-005

" TE-518-008

" TE-5J7-311

" TE-5H5-015

" TE-4E8-011

" TE-4F7-015

" TE-468-021

" TE-4F8-028

" TE-4F8-032

" TE-iST-00i

C-12'
20307000 TEMPF 718010000

20307100 TEMPF 225010000

*ADDED OR CHANGED CONTROL VARIABLE IN TRANSIENT

*012 TOTAL COLLAPSED CORE LEVEL

20501200 CCCLEVEL SRII 1.0 0.0 1

20501201 0.0 1.0 CNTRLVAR 3

20501202 1.0 CNTRLVAR 9

* 013 BOTTOM BASE LEVEL

20501300 BBLEVEL SUN 1.0 0.0 1

20501301 1.298489 -1.0 CNTRLVAR 12

*CHANGED OR ADDED CCONTROL VARIABLES

20505900 AVCOMS SUM 1.0 0.0 1

20505901 0.0 0.044204786 RHO 011010000

20505902 0.0442044786 RHO 012010000

20505903 0.044204786 RHO 013010000

20505904 0.044204786 RHO 014010000

20505905 0.044204786 RHO 015010000

20505906 0.044204-786 RHO 016010000

20506000 HCOMS SUM 1.0 0.0 1

20506001 0.0 0.006997366 RHO 021010000

20506002 0.006997366 RHO 022010000

20506003 0.006997366 RHO 023010000

20506004 0.006997366 RHO 024010000

20506005 0.006997366 RHO 025010000

20506006 0.006997366 RHO 026010000

*REACTOR VESSEL MASS

20507100 WVASS SUM 1.0 0.0 1

20507101 0.0 1.0 CNTRLVAR 59

20507102 1.0 CNTRLVAR 60

20507103 1.0 CNTRLVAR 65

20507104 1.0 CNTRL VAR 67

* PRIMARY COOLANT TOTAL MASS

20507200 PCSMASS SUM 1.0 0.0 1

20507201 0.0 1.0 CNTRLVAR 61

20507202 1.0 CNTRLVAR 62

20507203 1.0 CNTRLVAR 63

20507204 1.0 CNTRLVAR 64

20507205 1.0 CNTRLVAR 68

20507206 1.0 CNTRL VAR 69

20507207 1.0 CNTRLVAR 70

20507208 1.0 CNTRL VAR 71

*TOTAL INJECTION MASS

20507400 TOINFL SUN 1.0 0.0 1

20507401 0. 1.0 NELOWJ 600000000

20507402 1.0 MFLOWJ 640000000

20507500 INJMASS INTEGRAL 1.0 0.0 1

20507501 CNTRL VAR 74

*TOTAL DISCHARGE MASS

20507600 TOBRFL SUM 1.0 0.0 1

20507601 0. 1.0 MFLOWJ 317000000

20507602 1.0 MFLOWJ 347000000

C-1 3
20507700 BRIIAS INTEGRAL 1.0 0.0

20507701 CNTRL VAR 76

20507701 CNTRL VAR 76

* END OF INPUT

M~OR

MIOR

C-i14
Appendix D. Updat List for PSI-EIR 83 based on RELAP5/110D2 Cycle 36.04

APPENDIX D Update list for a updated RELAP5/110D2 Cycle 36.04

/JOB

R?1364T,T200.

/USER

ATTACH,OLDPL=REL354S.

PIJRGE,RE364TS/NA.

PURGE,RE364TX/NA.

PURGE, RE364TL/NA.

*IMPORTANT N! * THE UPDATE DIRECTIVE *

* SHOULD HAVE *COMPILE DEFINE * AS THE FIRST DIERECTIVE

UPDATE, N=RE364TS.

UPDATE ,P=RE364TS,Q,C=R5SEG.

RELC,R5SEG.

RETURN,OLDPL.

*DEFINE,RE364TS.

RETIJRN,RE364TS.

ATTACH ,ENVRLX=ENVR4IX.

LIBRARY,ENVRLX.

SELECTA ,COMPILE, COMP.

LIBRARY.

RETURN, ENVRLX.

REWIND,COMP.

FTN5,I=COMP,DO,ET,STATIC,OPT=2,ROUND,LO=M/A/R/S.

RETIIRN,COMP.

REWIND,LGO.

ATTACH ,RELAP5I=REL36IL.

GTR,RELAP5I ,ADD .REL/*

*DEFINE ,RELAP5O=RE364TL.

LIBEDIT,P=RELAP50, I=O,B=ADD,LO=F,U,C.

LIBEDIT,P=RELAP5O,B=4GO, I=0,LO=F,U,C.

RETURN,NULL,LGO,RELAP5I.

RETURN, RLP5F1, RLP5F2.

ATTACH, ENVRL=ENVR41L.

FILERSTIN,RT=S,SBF=NO,USE, FO=SQ.

RFL,EC=200.

DEFINE, RE364TX.

SEGLOAD, I=R5SEG,B=RE364TX.

LDSET,LIB=RELAP5O/ENVRL.

LDSET,PRESETA=NGINDEF ,ERR=NONE ,MAP=SB.

LDSET,STAT=RSTIN.

LIBLOAD,ENVRL, $HDR=$.

LIBLOAD,FTN5LIB,$FERCAP.$,$RPVCAP.$,$FTNRPZ.$,$Q2NM Y.$.

NOGO.

RETUJRN,RELAP50, ENVRL,COM1PIL~E.

SKIP,WK.

EXIT.

ENDIF,KKK.

DAYFILE,1(M RDAY.

REPLACE, KMRRDAY.

/EOR

*COMPILE DEFINE

*ID CBD3604

*D DMK36Ol.484

*D PLOTMD .24

D-1
901 FORMAT ('OPLOTFL SCRACH FILE GENERATED.)

*COMPIILE DEFINE ,SEGDIR

*COMPILE RELAP5

*D RJW36O3.23

DATA PTTE"EAP//' '60-S""REACTOR O, "55 OF COOL".

*f ENDIF

*ID XWUO1 ALREADY IMPLEMENTED IN RELAP5OLDPL36O4C,

WHICH IS USED AS BASIS

*/ CORRECTIONS OF INDEX IN SUBROUTINE RACCUN

*I RACCUM.618

IELV4I

*B DMK36OZ. 581

I=IELV

*COMPILE DEFINE ,SEGDIR ,RACCUN

*ID KWU01

*I RACCUII.618

IELV=I

*B DMK3602.581

I=IELV

*/ END OF KWU-UPDATES TO CYCLE 3604

*COMPILE DEFINE ,SEGDIR

*IDENT SKI101

THESE UPDATES ARE RECOMMENDED BY SKI TO BE

IMPLEMENTED IN RELAP5/MOD2-36.04

SOURCE: LETTER FROM SrUDSVII( (MR.SANDERVAG)

TO KWh] (IIR.GRUBER)

1987-06-25

COMPILE RELAP5

*COMPILE IHTCMP

FIX AN INDEXING ERROR IN IHTCMP

ERROR CAUSED ROD PLENUM VOLUME FOR GAP-GAS PRESSURE CALCULATION

TO BE INCORRECT. FOUND AND FIXED BY D.CARAHER 20MAY87

FIX ONLY CDC-VERSION CODING

*D IHTCMP.1041

L=( .NOT.MASX(43)*.AN'D.IHTPTR(J))+FILNDX(8)

*/ UPDATE ROUTINE IRFLHT TO ALLOW REFLOOD TO WORK

*/ HEAT STRUCTURE FILE GETS CHANGED ON RESTART (FOR

*/ EXAMPLE BY DELETING OR ALTERING SOME STRUCTURES)

*/NOTE.. HAT STRS ASSOCIATED WITH REFLOOD CANNOT BE ALTERED

*1 ON RESTART AS IRPLHT IS NOW PROGRAMMED

*COMPILE IRFLHT

*I IRFLHT.330

C, UPDATE THE GEOMETRY POINTER IN IGLRFL BITS 44-60 IN CASE THE

C HEAT STRUCTURE FILE CHANGED ON RESTART.

J=(.N0T.MASX(43).ANlD.IH) + lIHT

J=(.NOT.MASK(43).AND.IHTPTR(J)) + lIHT

NCOLS=.NOT.MlASK(43) .AND.INXGON(J)

IGLRFL(I)=(MASK(43) .AND.IGLRFL(I)).OR.NCOLS

*/ END OF UPDATES S1(I01

*/START OF PSI UPDATE

D-2
*ID MARTIN

*I PHAINT.9

COMIION/IFLG2/IFLAG2( 1000)

DIMENSION IFLAG1( 100)

*I PHAINT.151

IIFL1=( I-IV4-IVSHP)/IVSKP

IFLAG1( IIFL1)=O

*I PHAINT.294

TGSAT=TGSAT-40.*VOIDF( I)

*I PIIAINT.370

IF(FBLrB.GT.0.0.OR.FSLUG.GT.0.0.AND.DIAMV(I) .LT.0.018)

1 IFLAG1(IIFL1)=1

*1 PHAINT.390

IF(DIAMV(I).LT.0.018) THEN

FIC=65.O*VOIDG( I)*VOIDF(I)**3.0*RHOG(I)/DIAMV(I)

ENDIF

*I PHAINT.421

IF(DhIAMV(I).LT.O.018) THEN

FIC1=65.O*VOIDG( I)*VOIDF(I )**3'.O*RHG( I )/DIAIV( I)

ENDIF

*I PIIAINT.424

IF(DIAMbV(I).GE.O.018) THEN

*I PHAINT.425

ENDIF

*1 PHAINT.495

IF(DIAMV(I).LT.0.018) FIC1=FIC1*O.5

*I PHAINT.633

IF(DIAMV(I).LT.O.018) THEN

FIC1=VOID*(FIC1*0. 541. 225*O.4*RHOG I )*SLSLfS*VOID**2.)

ELSE

*I PHAINT.634

ENDIF

*I PHAINL.656

IF(DIAMV(I).LT.O.018) FIC=FIC*0.5

*I PHAIT.462

IF(DIAIIV(I).LT.O.018) FIC=F.IC*0.5

*1 PHAINT.855

IIFL2= (I-IJ+IJSEP)/IJSKP

IFLAG2( IIFLZ)=O

*I PHAINT.919

INDI{=(K-IV+IVSEP)/IVSKP

INDL=( L-IV+IVSKP)/IVSKP

IF(IFLAG1(INDK) .EQ.1.OR.IFLAG1(INDL) .EQ.1) IFLAG2(IIFL2)=l

*D QFHTRC.156

HTV2( INDZ) =HCCHFA*EXCP( -O.0175*TERI)+GTERM*EXP( -0. 012*TERM) *D QFHTRC. 178

FACBR = (1.+O.025*AMAX1(0. ,SATT(IDX)-TEMIPF(IDX)))

HCBR=AMAX1(HTV2(INDZ).(C0NVAP*TERM1*TERIIZ*( (SATHG(IDX)-SATHG( IDX))

*D QFHTRC.179

1/AIIX1(THPBDY-SATT(IDX) ,O.01)+0.68*CSUBPG(IDX) )*9.81/(2.*3.14159)

*D QFTc. 180

2 *SQRT(9.81*TEJRflVSIGMA(IDX) )/VISCG(IDX))**0.25*0.62*FACBR)

VELD=AIIAX(VELG( IDX)-VELF( IDX) ,0.001)

DDROP=3.*SIGMA(IDX)/(RHOG( IDX)*VELD**2)

IF( DDROP. LT. 1. 5E-4)DDROP=1. 5E-4

IF(DDROP.GT. 3.OE-3)DDROP=3.OE-3

TERM5=1./(1.+O.35*CSUBPG(IDX)*AMAX1(TMPBDY-SATT(IDX) ,0.OOO1)

1 /AMAX1(SATHG(IDX)-SATHF(IDX),O.O1))**3.

HCFO=0.4*3.14159/4.*(6.*(1.-VOIDG(IDX) )/3.14159)**0.66566667

D-3
1 *(9.81*RIIOF(IDX)*RHOG(IDX)*ANAX(SATIIG(IDX)-SATHF(IDX),0.01)

2 *TERM5*CONVAP/(AMXIA(TMPBDY-TE1IPF(IDX) ,0.O001)*VISCG(IDX)

3 *(3* 14159/6. )**O.3333333*DDROP) )**0.25

IF(VOIDG(IDX) .LE.O.6)THEN

HCFB=1ICBR

ELSE

IF(VOIDG(IDX).GE.0.8) THEN

HCFB=HCFO

ELSE

HCFB=(VOIDG(IDX)-0.6)/O.2*HCFO+(0.8-VOIDG(IDX))/0.2

1 *HCBR

ENDIF

ENDIF

*D QFHTRC.187,138

TERII=TERIIZ+HCFB

*D QFHTRC .209

1 *AMA1(0.023*(REYN2)**0.4/'DIILIV(IDX) ,TERII4)

*D QFHTRC.221,223

VELD=MlAX(VELG( IDX)-VELF( IDX) .0.001)

DDROP=3. *SIGjA( IDX)/( RH0G( IDX) *VELD**2)

IF(DDROP.LT.1.5E-4) DDROP = M.E-4

IF(DDROP.GT.3.OE-3) DDR0P = 3.OE-3

TERII5=1./(1.+0.35*CSIJBPG(IDX)*AMAX1(TIIPBDY-SATT(IDX) .0.0001)

1 /(SATHG(IDX)-SATHF(IDX) ))**3.

HCFO=0.4*3. 14159/4.*(6.*(1.-VOIDG(IDX) )/3.14159)**O.6666667

1 *(9.81*RHOF(IDX)*RHOG0(IDX)*(SATHG(IDX)-SATHF(IDX))

2 *TERN5*C0NVAP/(ANAX1(ThIPBDY-TEM1PF( IDX) ,0.0001)*VISCG( IDX)

3 *(3.1415916. )**0.3333333*DDROP))**0.Z5

HCFB=HCFO

*I VEXPLT.9

CONN0N/IFLG2/IFLAG2( 1000)

*1 VEXPLT.322

c0=1.0

IIFL2=( I-IJ+IJSKP)/IJSKP

IF(IFLAG2(IIFLZ).EQ.1) THEN

CO=1.2

IF(C1.LT.0.7) C1=0.7

ENDIF

*D VEXPLT.323

FJFG=(FIJ(I)*DX*(ABS(C1*VELGJO(I)-CO*VELFJO(I))+0.01) *D VEXPLT.507

DIFF=SCRACH+( FRICFJ+CO*FJFG+VPGNX+HLOSSF) *Ir

*D VEXPLT.508

DIFG=-SCRACH-( FRICGJ+C1*FJFG+VPGNX+HLOSSG)*DT

*I VIIPLT.8

CONMON/IFLG2IFLAGZ( 000)

*I VIMPLT.435

C021.0

C 1=1. 0

IIFL2=( I-IJ+IJSKP)/IJSKP

IF(IFLAGZ(IIFL2).EQ.1) THEN

C0=1.2

C1=(1.0-CO*VOIDGA)/AIIAX1( (1.-VOIDGA) ,1.OE-5)

IF(C1.LT.0.7) C1=0.7

ENDIF

*D VfIPVLT.436

FJFG=(FIJ( I)*DX*(ABS(C1*VELGJO(I)-CO*VELFJO(I))+0.01)

D -4
*D VIMPLT.591

COEFV( IDG-1) = (FRICFJ+CO*FJFG+VPGNX+HLOSSF)*DT + SCRACH

*D VIMPLT.592

COEFV(IDG) =-(FRICGJ+C1*FJFG+VPGNX+HLOSSG)*DT - SCRACH

*C DEFINE ,PHAINT,QFHTRC ,VEXPLT ,VIMPLT

*/END OF PSI UPDATE

*COMPILE ACCUN,PHAINT,DTSTEP

*/PROTECTS SIGMA (SURFACE TENSION) BY 1.OE-7 IN SUBROUTINE PHAINT

*DELETEPHAINT. 200

DSTAR(I =DIAMV(I)*SQRT(9.8*RHOFG/ANAX1(SIGMA(I) ,1.OE-7))

*DELETE.PHAINT.326

55 VCRIT=2.5*SQRT(SQRT(RflAX1(SI nA(I) ,1.OE-7)*RHOFG)/RHOG(I))

*/CORRECT ERROR IN SUBROUTINE DTSTEP INTRODUCED IN CYCLE 30 SO THAT

*/STATE PROPERTIES ARE NOT RESET WHEN AT A MIINIMUM TINESTEP DUE TO

*/MASS ERROR

*DELETE,DTSTEP.161

IF (NANY .EQ. 0) WRITE (OUTPT,2003)

*/REWET CRITERIA REDUCTION (89/5/23 AXSAN & ICAP)

*IDENT !IARTIN2

*1 HTRC1.60

GGT = RHOF(IV)*VOIDF(IV)*VELF(IV)+

1 RIIOG(IV)*VOIDG(IV)*VELF(IV)

*I HTRC1.1U1

IF(GGT.GT.-100.) GO TO 12

*D HTRC1.112

IF(XE.GT.XEC.OR.TW.GT.(1250.-TSAT)) GO TO 2000

GO TO 13

12 IF(E.GE.XEC) GO TO 2000

13 CONTINUE

*I HTRC1.82

IF(GGT.GT.-100.) GO TO 11

*D HTRC1.83

IF(TW.ff.1250.-TSAT) GO TO 2000

11 CONTINUE

*I PSTDNB.28

GGT = RHOF(IV)*VOIDF(IV)*VELF(IV)+

1 RHOG(IV)*VOIDG(I'J)*VELG(IV)

*I PSTDNB.29

IF(GGT.GT.-100.) GO TO 231

*D PSTDNB.30

IF(XE.GT.XEC.OR.TW.Gr.(1250.-TSAT)) GO TO 235

*1 FSrDNB.31

GO TO 232

231 IF(XE.GT.XEC) GO TO 235

232 CONTINUE

*I PSTDNB.124

IF(GGT.GT.-100.) GO TO 401

*D PSTDNB.126

1 (1250.-TSAT)) TRANS = .FALSE.

*I PSTDNB.141

GO TO 499

D-5
401 IF(XE.GE.XEC)THRNS=.FALSE.

IF(TRANS) THEN

GO TO 402

ELSE

GO TO 403

ENDIF

402 HTCF=AIAX1(HTBF ,HFB)

HTCG=AIAX1( HTBG ,HV)

QFFO=AflAX1( QTFBF ,QFBF)

QFGO=AflAX1(QTFBG,QFBG)

GO TO 450

403 HTCF=HFB

HTCG=HV

QFFO=QFBF

QFGO=-QFBG

499 CONTINUE

*D PSTDNB.42

IF(GGT.LT.-100) THEN

FL=EXP(-5.O*THETA*RIIIN1(ABS(TW-TWRTO) ,SQRT(DTSAT)))

ELSE

IF(GGT.GE.-100..AND.GGT.LE.O) THEN

FL=( (EXP(-2.O*THETA*AIIIN1(ABS(TW-TWRTO) ,SQRT(DTSAT)))

1 -EX[P(-5.O*THETA*AMIN1(ABS(TW-TWRTO),SQRT(DTSAT))))/100. )*GGT+

2 EXP( -2.O*THETA*AMIN1(ABS(TW-TWRTO) ,SQRT(DTSAT)))

ELSE

FL= EX[P(-2.O*THETA*AIIIN1(ABS(TW-TWRTO) ,SQRT(DTSAT)))

ENDIF

ENDIF

FL = FL*AIIIN1(1.,(((l.-ALPH)/O.05)**4))

*D PSTDNB.67

HFB = O.92163*(SQRT(HFB/SIGNA(IV))

*1 PSTDNB.69

HCBR = HFB

VAIIA = RIIAX1(VELG(IV)-VELF(IV),O.OO1)

VFG2 = VAMA**2.

RDIAM =RHOG( IV)*VFG2/XA

DDROP = 1./RDIAII

IF(DDROP.LT. 1.OE-4) DDROP=1.OE-4

IF(DDROP.LT. 3.OE-3) DDROP=3.OE-3

TERM5=1./(l.+O.35*CSUBPG(IV)*ANAX1(TW-TSAT,O.OO1)

1 /AMAX1(SATHG(IV)-SATHF(IV),O.O01))**3.

HCFO=O.2*3.14159/4.*(6.*(1.-VOIDG(IV))/3.14159)**O.6666667

1 *(9.81*RHOF(IV)*RHOG(IV)*AIIAX1(SATHG(IV)-SATHF(IV),O.01)

2 *TERfl5*THCONS**3/(AMAX1(TW-TEMPF( IV) ,0. O1)*VISCS

3 *(3.14159/6. )**O.3333333*DDROP) )**O.25

HCFO = O.OO1*HCFO

IF(VOIDG(IV).LE.O.60) THEN

HFB=HCBR

ELSE

IF(VOIDG(IV).GE.0.8O) THEN

HFB=HCFO

ELSE

HFB=(VOIDG(IV)-O.60)/O.2*HCFO+(O.8O-VOIDG(IV) )/O.2

1 *HCBR

ENDIF

ENDIF

IF(GGT.LT.O.) THEN

HHHH=AIIAX1(1.E-7,RIIOF(IV)-RHOG( IV))

D-6
HFB=1.09680*VOIDF(IV)*SQT( (1./i.)

1 *THCONS**3*RHjOG(IV)*uHflIH*(HFG-O. 5*DTSAT*CSIJDPG(IV))

2 /(VISCS*DTSAT) )**.25

ENDIF

*C IITRC1,PSTDNB,PREDNE

*/END OF AKSAI4 UPDATE

/EOR

*COMPILE SEUDIR

D-7

NRC FORM 33 U.S. NUCLEAR REGULATORY COMMISSION I.REPORT NUMBER

(2-89) IAu~rWd bj, NRC. Add Vol.. Svep.. Rev., 320M11302, and Addwndsm Numboms Itany.)

3201,3202 BIBLIOGRAPHIC DATA SHEET NUREG/IA-0070

(See instrujct ions on the reverse)

2. TITLE AND SUBTITLE

Assessment of RELAP5/!1OD2 Cycle 36.04 with LOFT____________

Large Break LOGE L2-3 3. DATE REPORT PUBLISHED

MONTH "EAR

April. 1992 4. FIN OR GRANT NUMBER

___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ ___ A4682 6. AUTHOR(S) 6. TYPE OF REPOR7T

Y. S. Bang, H. J. Kim, Korea Institute of Nuclear SafetyTehca

S. H. Kim, Korea Atomic Energy Research Institute Technical _______

7. PERIOD COVERED Vinciusine Dates

B. PERFORMING ORGANIZATION - NAME AND ADDRESS 1UfNRC.0mrvide Division. Ofice or Regon. U.1 Nuclear Regulatory Corn ,. afdiJngades if contra rto, pro sid

ew,,. and mailing addres&I

Korea Institute of Nuclear Safety

P.O. Box 16, Daeduk-Danji

Daejoni 300-31

Republic of Korea

and mailing address)

Office US ula of Nuclear euaoyCmiso Regulatory Research 

Washington, DC 20555

10. SUPPLEMENTARY NOTES

11. ABSTRACT (200 wardk or kis

The LOFT LOCE L2-3 was simulated using the RELAP5/MOD2 Cycle 36.04 code to assess its

capability to predict the thermal-hydraulic phenomena in LBLOCA of the PWR. The reactor

vessel was simulated with two core channels and split downcomer modelling for a base

case calculation using the frozen code. From the results of the base case calculation,

deficiencies of the critical flow model and the CHF correlation at high flow rate were

identified, and the severeness of the rewetting criteria were also found. Additional

calculation using an updated version of RELAP5/MOD2 Cycle 36.04 including modifications

of the rewet criteria shows a substantial improvement in the core thermal response.

12. KEY WORDSIDESCR.PTORS (List words or ph rese that wiltsinsst researchers in locating the port.I1 13. AVAILABILITY STATEMENT

Unl imi ted

RELAP5/MOD2, Assessment, RELAP5/MOD2 Cycle 36.04, LOFT Large Break 14. SECURITY CLASSIFICATION

LOCE L2-3 1This Page)

Unclassified

(This Report)

Unclassified

15. NUMBER OF PAGES

16. PRICE

NRC FORM 3.35 17.AQI


THIS DOCUMENT WAS PRINTED USING RECYCLED PAPER

UNITED STATES

NUCLEAR REGULATORY COMMISSION

WASHINGTON, D.C. 20555

SPECIAL FOURTH-CLASS RATE

POSTAGE AND FEES PAID

USNRC

PERMIT NO. G-07

OFFICIAL BUSINESS

PENALTY FOR PRIVATE USE, $300