NUREG/IA-0032

Intemadonal

Agreement Report

Assessment of RELAP5/MOD2,

Cycle 36.04 Using LOFT

Large Break Experiment L2-5

Prepared by

Young Seok Bang, Sang

Nuclear Safety Center

Korea Advanced Energy

Yong Lee, Hho-Jung Kim

Research Institute

Office of Nuclear Regulatory Research

U.S. Nuclear Regulatory Commission

Washington, DC 20555

April 1990

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

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

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

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by such third party Would not infringe privately owned rights.

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U.S. Government Printing Office

P.O. Box 37082

Washington, D.C. 20013-7082

and

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Springfield, VA 22161
NUREG/IA-0032

Agreement InternationalReport

Assessment of RELAP5/MOD2,

Cycle 36.04 Using LOFT

Large Break Experiment L2-5

Prepared by

Young Seok Bang, Sang Yong Lee, Hho-Jung Kim

Nuclear Safety Center

Korea Advanced Energy Research Institute

Office of Nuclear Regulatory Research

U.S. Nuclear Regulatory Commission

Washington, DC 20555

April 1990

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 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 States and Korea (Agreement on Thermal-Hydraulic Research

between the United States Nuclear Regulatory Commission 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/IIOD2 Cycle 36.04

USING LOFT LARGE BREAK EXPERIMENT LZ-5

Abstract

The LOFT L2-5 LBLOCA Experiment was simulated using the RELAP5/MOD2

Cycle 36.04 code to assess its capability to predict the phenomena

in LBLOCA. One base case calculation and three cases of different

nodalizations were carried out. The effect of different nodalization was studied in the area of the downcomer and core. For a

sensitivity study, another calculation was executed using an

updated version of RELAP5/MOD2 Cycle 36.04.

A Split downcomer with one crossflow junction and two core channels

were found to be effective in describing the ECC bypass and hot

channel behavior. And the updated version was found to be effective

in overcoming the code deficiency in the interfacial friction and

reflood quenching.

iii
Executive Summary

This report documents the assessment calculations using RELAP5/

MOD2 Cycle 36.04, a frozen version of the code, to predict the

thermal-hydraulic responses of the Loss of Fluid Test (LOFT) L2-5

Large Break- Loss of Coolant Accident (LBLOCA). Experiment L2-5

simulated a 200 % guillotine break at the discharge of a primary

coolant pump of a four loop commercial pressurized water reactor

(PWR).

The version of the code used in the present calculations was

the RELAP5/MODZ Cycle 36.04 with some corrections on indexing

errors. For the base calculation, the reactor vessel of the LOFT

system was modelled by a split downcomer with crossflow junctions

and the single core channel. Results of the base case calculation

indicated (1). the unrealistic ECC bypass flow through crossflow

junctions between the intact side downcomer and the broken side

downcomer, (2). the flow oscillations due to the overpredicted interfacial friction in the rod bundle geometry, and (3). underpredicted core heat up due to poor modelling the hot channel behavior.

To determine the effectiveness of the nodalization changes and

to quantify their effects on the thermal-hydraulic responses,

nodalization studies was performed for three different cases of

reactor vessel modelling. They are, split downcomer modelling

without crossflow junction (CASE A), finer axial modelling of core

(CASE B) and two core channel modelling (CASE C). A calculation was

also carried out using an updated version of RELAP5/MOD2 Cycle 36.04

iv
ACKNOWLEDGEMENTS

This report was completed under the sponsorship of the Korean Ministry

of Science and Technology. Dr. Sang Hoon Lee, President of the Korea Nuclear

Safety Center, contributed significantly to the administration of the project.

Authors expressed a great appreciation for their in-depth technical review of

the report to Professors E.C.Lee, C.S.Kang in Seoul National University and

Professors N.H. Chun, S.H. Chang in Korea Advanced Institue of Science and

Technology. Special Thanks should be addressed to Dr. Sih Hwan Kim, General

Manager of LWR Fuel Division in Korea Advanced Energy Research Institute,

for his general support to this project.

Another appreciation should be expressed to Mr. Dick Schultz, Rich Riemke

and Bob Hanson in EG&G, Idaho for their kind advices of RELAP5 assessment

work. Mr. Schultz's technical response for the experimental data tape questioned by authors was greatly important in preparing the data comparison in

this report. Authors should appreciate Dr. Aksan in Paul Scherrer Institute

in Switzland for his code update work and technical comments during his

visit in Korea and to Mr. D.Bessette in USNRC for his coordination of this

technical support.

Authors should express their sincere gratitudes to members of Department

of Safety Analysis in ENSC, Mr. Bub Dong Chung and Dr. Euy Joon Lee for

techincal discussions and to Mr. Jong Han Park for preparing data plots.

v
with PSI (Paul Scherrer Institute) modifications to investigate the

sensitivity of code model changes.

According to the results of calculations for nodalization and

sensitivity studies, it is shown that an unrealistic ECC bypass flow

can be reduced by deleting unnecessary crossflow junctions in the

downcomer. Results also show that the axial refinement of core

nodalization has little effect on the thermal response of the core

and that two core channels are effective in describing a hot channel

behavior in LBLOCA. It is also found that the improvement of interfacial friction in the rod bundle and the correction of heat transfer

correlation in reflood phase can reduce the unphysical flow

oscillation and predict the quenching temperature accurately.

vi
List of Contents

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

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

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

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

2.3 Uncertainty .......................................... 4

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

3.1 Code Description ..................................... 5

3.2 Modelling Description ................................ 5

3.3 Boundary Conditions .................................. 6

3.4 Steady State Calculation ............................. 7

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

4.1 Results of Base Case Calculation ..................... 8

4.2 Discussions on Base Case Calculation ................. 8

4.2.1 Hydraulic Behavior .............................. 8

4.2.1 Thermal Behavior ................................ 11

5. Nodalization and Sensitivity Study ......................... 13

5.1 Scope of Nodalization and Sensitivity Study .......... 13

5.2 Discussion on Nodalization Study ..................... 14

5.2.1 Crossflow Junctions in Downcomer ................ 14

5.2.2 Refinement of Axial Nodalization of Core ........ 15

5.2.3 Two Flow Channels in Core ....................... 15

5.3 Discussion on Sensitivity Study ...................... 16

6. Run Statistics ............................................. 18

7. Conclusions ............................................... 19

References .................................................... 21

Tables ........................................................ 22

Figures ...................................................... 32

Appendix

vii
List of tables

Table I Summary of comparison of the initial conditions

between the measured and the calculated in base case

Table 2 Summary of comparison of the sequence of events

between the measured and the calculated in base case

Table 3 Uncertainties of measurements

Table 4 Summary of the corrected items in RELAP5/MOD2 Cycle 36.04

Table 5 Summary of the important items in nodalization

Table 6 Summary of the boundary conditions for base case calculation

Table 7 List of the important assessment parameters

Table 8 Updated items in PSI EIR-83

Table 9 Summary of the calculation conditions for nodalization and

sensitivity study

Table 10 Run statistics data in base case calculation

List of figures

Fig.1 Axonometric configuration of LOFT L2-5 test

Fig.2 Nodalization diagram for base case calculation of LOFT L2-5 test

Fig.3 Axial power distribution in base case calculation of LZ-5 test

Fig.4 Power history in base case calculation of L2-5 test

Fig.5 Comparison of primary system pressure

between the base case calculation and the experiment

Fig.6 Comparison of secondary system pressure

between the base case calculation and the experiment

Fig.7 Comparison of mass flow rate at broken loop cold leg

between the base case calculation and the experiment

Fig.8 Comparison of mass flow rate at broken loop hot leg

between the base case calculation and the experiment

Fig.9 Comparison of mass flow rate at intact loop cold leg

between the base case calculation and the experiment

Fig.1O Comparison of mass flow rate at intact loop hot leg

between the base case calculation and the experiment

viii
Fig.11 Comparison of primary system density at intact loop hot leg

between the base case calculation and the experiment

Fig.12 Comparison of primary coolant pump speed

between the base case calculation and the experiment

Fig.13 Comparison of liquid level in accumulator

between the base case calculation and the experiment

Fig.14 Comparison of coolant temperature in upper plenum

between the base case calculation and the experiment

Fig.15 Comparison of coolant temperature in lower plenum

between the base case calculation and the experiment

Fig.16 Comparison of coolant temperature at downcomer inlet

between the base case calculation and the experiment

Fig.17 Comparison of coolant temperature at downcomer outlet

between the base case calculation and the experiment

Fig.18 Comparison of fuel centerline temperature at 27 inches

between the base case calculation and the experiment

Fig.19 Comparison of cladding temperature at 5 inches of hot fuel

between the base case calculation and the experiment

Fig.20 Comparison of cladding temperature at

between the base case calculation and

Fig.21 Comparison of cladding temperature at

between the base case calculation and

Fig.22 Comparison of cladding temperature at

between the base case calculation and

Fig.23 Comparison of cladding temperature at

between the base case calculation and

Fig.24 Mass flow rate at the inlet of intact

Fig.25 Mass flow rate at the inlet of intact

Fig.26 Mass flow rate at the bypass junction

Fig.27 Mass flow rate at the bypass junction

Fig.28 Mass flow rate at the bypass junction

Fig.29 Mass flow rate at the bypass junction

21 inches of hot fuel

the experiment

27 inches of hot fuel

the experiment

39 inches of hot fuel

the experiment

54 inches of hot fuel

the experiment

side downcomer in base case

side upper annulus in base case

J722 in base case

J724 in base case

J726 in base case

J728 in base case

Fig.30

Fig.31

Fig.32

Fig.33

Mass flow rate to the core from the lower plenum in base case

Collapsed liquid level in the core in base case

Comparison of nodalization in CASE A, CASE B and CASE C

Discretization scheme of hot channel of the core

ix
Fig.34 Comparison of mass flow rate at broken loop cold leg

between base case and CASE A

Fig.35 Collapsed liquid level of the downcomer in CASE A

Fig.36 Comparison of liquid level in the intact side downcomer

between base case and CASE A

Fig.37 Comparison of primary system pressure

between base case and CASE A

Fig.38 Comparison of liquid level in the core

between base case and CASE A

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

between base case and CASE A

Fig.40 Comparison of

in base case,

Fig.41 Comparison of

in base case,

Fig.42 Comparison of

in base case,

Fig.43 Comparison of

in base case,

Fig.44 Comparison of

in base case,

Fig.45 Comparison of

in base case,

primary system pressure

CASE A and CASE B

cladding temperature at

CASE A and CASE B

cladding temperature at

CASE A and CASE B

cladding temperature at

CASE B and CASE C

cladding temperature at

CASE B and CASE C

cladding temperature at

CASE B and CASE C

21 inches of hot fuel

27 inches of hot fuel

21 inches of hot fuel

27 inches of hot fuel

5 inches of hot fuel

Fig.46 Collapsed liquid level in the hot channel of core in CASE C

Fig.47 Comparison of cladding temperature at 43.8 inches of hot fuel

between CASE B and CASE C

Fig.48 Comparison of primary system pressure

between CASE B and CASE C

Fig.49 Comparison of mass flow rate at intact loop hot leg

between CASE C and CASE D

Fig.50 Comparison of liquid level in the hot channel of core

between CASE C and CASE D

Fig.51 Comparison of primary coolant pump velocity

between CASE C and CASE D

Fig.52 Comparison of cladding temperature at 21 inches of hot fuel

between CASE C and CASE D

Fig.53 Comparison of cladding temperature at 27 inches of hot fuel

between CASE C and CASE D

x
Fig.54 The required CPU time versus the advanced time

in base case calculation of L2-5 test

Fig.55 Time step size of base case calculation of L2-5 test

List of Appendix

Appendix A. Update List for RELAP5/MOD2 Cycle 36.04

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

Appendix C. A Base Case Input Deck for a Transient Calculation

Appendix D. Update List for PSI-EIR 83 based on RELAP5/1OD2 C.36.04

xi

1. Introduction

RELAP5/IOD2[1], which was developed by the Idaho National Engineering

Laboratory (INEL) under the sponsorship of the United States Nuclear

Regulatory Commission (USNRC), has been frequently used in safety

analysis of the Pressurized Water Reactor(PWR). The RELAP5/MOD2 code

is applicable to the simulation of the postulated Loss of Coolant

Accident (LOCA). However it has some deficiencies especially in

analyzing the Large Break Loss of Coolant Accident (LBLOCA) (2]. Most

of these deficiencies are being removed in the next version of the code,

RELAP5/MOD3 [3].

Under the International Code Assessment and Application Program(ICAP)

organized by the USNRC, the code is being assessed and the code

deficiencies are being identified based on code assessment activities

of the ICAP member countries [4].

This report is part of the Korean contribution of 15 code assessments to ICAP. The RELAP5/MODZ Cycle 36.04 code was used in the

present calculation simulating the Experiment LZ-5 of the Loss of Fluid

Test (LOFT) [5). The Experiment L2-5, as one of the Integral Effect

Test (IET), simulated a 200 % guillotine break at the primary coolant

pump (PCP) discharge with a rapid coastdown of PCP in a Westinghouse

4 loop commercial PWR.

One base case calculation and three sensitivity calculations for

different nodalizations of the reactor vessel using the frozen version

of the code are presented in this report. Another calculation using

an updated version of RELAP5/MODZ Cycle 36.04 is also presented to

address the code deficiencies and sensitivity of the models in the code.

The descriptions of the LOFT system and the Experiment L2-5 are provided in Chapter 2. The code and modelling for a base case calculation

-1-
are described in Chapter 3. The results of the base case calculation

are discussed in Chapter 4 in terms of thermal and hydraulic behaviors.

In Chapter 5, the scope and results of the calculations for nodalization and sensitivity studies are presented. Run statistics are discussed in Chapter 6, !and general conclusions are drawn: in Chapter 7.

Appendices of this report contain the detailed information discussed

in theappropriate chapters.

-2-
2. Facility and Test Description

2.1 Facility Description

The LOFT facility is an experimental 50 MWt PWR designed to simulate

LOCA's and anticipated transients and to provide data on the thermal

hydraulic phenomena occurring throughout the system [6]. It is a scaled

representation of a commercial PWR of Westinghouse type having 4 loops

with a volume ratio of 1/60. The LOFT syatem consists of five major

systems : reactor 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 10 m, respectively. The overall configuration is

shown in Fig.l.

2.2 Test Description

Loss of Coolant Experiment (LOGE) L2-5 was the third experiment in the

nuclear power ascension test L2 series as an IET. L2-5 Test simulated a

guillotine break simultaneous with a loss of site power, at the discharge of the primary coolant pump of commercial PWR.

The specific objectives of L2-5 [5] were to determine if early core

rewet occurs with immediate PCP coastdown, to provide data on the core

thermal response for evaluation of computer code, and to evaluate the

external thermocouple effects on core thermal response.

Prior to the experiment, the intact loop was set to flow rate of 192.4

kg/s, temperature of 589.4 K and pressure in hot leg of 14.94 KPa.

Table 1 shows a summary of the measured initial conditions with the cal-

-3--
culated values by RELAP5/MODZ for the base case.

The experiment was initiated by opening the Quick-Opening BlowdownValves (QOBV) both in hot and cold leg, the reactor was scrammed on low

pressure (14.19 NPa) at 0.24 sec and PCP was tripped by operator at 0.94

sec. Accumulator was started to inject the coolant at 16.8 sec and

the delayed ECC injection from HPIS and LPIS was started at 23.9

and 37.3 sec, respectively. The experiment was completed at the time

of the end of LPIS injection, 107 sec. The detailed sequence of events

for L2-5 test are listed in Table 2 compared with the results of the

base case calculation.

2.3 Uncertainty

Uncertainties of the experimental data and computed variables from

measured data were fully discussed in reference[7] for L2-5 test. Uncertaineies 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

3.1 Code Description

RELAP5/MOD2 Cycle 36.04, frozen version of RELAP5/MOD2 used in this

assessment was received at October 1986.

For a specific objective of LBLOCA simulation in this report, the

indexing errors in subroutine RACCUM, IHTCMP and IRFLHT are corrected

from ýthe frozen code. In the correction, there are no model change and

hence the corrected version can also be regarded as RELAP5/MOD2 Cycle

36.04. These corrections were based on the update work of KWU, and

STUDSVIK, [8]. The corrected items and their rationale are listed in

Table 4, and the whole update list is presented in Appendix A. The code

features and input descriptions for a frozen code are presented in the

code manual[l].

3.2 Modelling Description

For a simulation of LOFT L2-5 Test, the original input as developed

by INEL[9] for RELAP5/MOD1 had a sufficiently discretized nodalization

including a pressurizer and its surge line, a steam generator secondary

side, a complex ECCS line, and a letdown and charging line, etc. A nodalization selected for a base case calculation in this assessment is

basically the same as used in reference [2]. It was also the fullydiscretized representation of the LOFT system, which was almost similar

to that in reference [9] except for the discretization in reactor vessel.

The selection of this nodalization scheme allows the results of base

calculation to be compared with the results in the reference [2]. The

5
important items of the nodalization scheme are shown in Table 5.

Differences of nodalization in the reactor vessel from the original one

[9] came from the trials to make a simple core modelling, i.e., single

core channel modelling, and to compare the cladding temperatures obtained

from calculations with those measured in experiment at the same locations, i.e., 12 volumes for a channel. Table 5 also shows a summary

of reactor vessel modelling for a base case. The overall nodalization

diagram in simulating L2-5 experiment is shown in Fig.2. It consists of

128 hydrodynamic volumes, 138 junctions and 33 heat structures. The

volume and junction options are selected almost the same as reference [21,

i.e., nonequilibrium and nonhomogeneous. The input deck used for a base

case is presented in Appendix B and C for steady state and transient

cases, respectively.

3.3 Boundary Conditions

Boundary conditions required for a simulation of L2-5 experiment are

listed in Table 6 . As shown in Table 6, the specified boundary conditions are almost the same as those in reference[2]. In the test calculations prior to the base calculation, the unrealistic results were

obtained when the containment back pressure, 0.1 TPa is used, which

was specified in reference [2]. This led to changes of some boundary

conditions, such as containment back pressure, reactor power history,

etc, in base case calculation. In the axial power level, the total

power integrated by the linear heat generation rate measured at the

locations of 5H8, IC7 for the central fuel assembly and the peripheral

fuel assembly repectively, is not equal to 36.0 Rt. Thus, the power

levels were corrected as shown in Fig.3. The power history used in

-6-
reference [2] was originally obtained only from the fission power

measured at the neutron detector of RE-T-77-1A2 [7] while the uncertainty for this measurement has the order of magnitude, 2 MR~t.

It exceeds the range of powers measured at the times 1.0 sec after

the experiment. To avoid this uncertain power, and to consider the

decay heat, a new power history was implemented as shown in Fig.4. and

Table 6.

3.4 Steady State Calculation

The steady state run was carried out with some modification of input

deck to reproduce fundamental, measured initial conditions and to provide all initial quantities of the whole system proir to the transient

calculation. Major changes are additions of 7 steady state controllers

2 PCP speed controllers, 1 pressurizer heater power controller,

1 pressurizer spray valve area controller, 1 letdown/charging valve

area controller, 1 Main Steam Control Valve (MSCV) area controller

and 1 feedwater flow rate controller. Some options are changed for

the related components. The changed input is provided in Appendix B.

The computing time required to obtain the final steady state was

about 980 s. The results of steady state calculation are summarized in

Table 1. From this Table, the calculated steady state values are found

to be similar to the measured values. A little difference in steam

generator secondary pressure can be ignored in that MSCV are closed

in a short time after initiation of experiment. The secondary side

pressure has little effect on the transient calculation in LBLOCA.

-7-
4. Base Case Calculation

4.1 Results of Base Case Calculation

The base case transient calculation was carried out on the basis of

the restart-plot file obtained from the steady state calculation. Some

additional components and steady state controllers were deleted and

options changed. The restart transient inputs are listed in Appendix C.

In this assessment the LBLOCA transient up to 120 sec was simulated,

during which the core quenching was completed at about 65 sec. The

sequence of events predicted in base case calculation is presented in

Table 2 as compared with the experimental chronology. In this chapter,

the comparison of results between the base case calculation and the

experiment is discussed in terms of the primary system hydraulic behavior and thermal response of the core.

Table 7 shows a list of the important assessment parameters to be

discussed below, which were almost the same as the ones discussed in

the reference [2].

4.2 Discussions on the Base Case Calculation

4.2.1 Hydraulic Behavior

The calculated primary system pressure is well-behaved as shown in

Fig.5. During 15 sec to 30 sec, a little more depressurization was

shown in the calculation than the experiment, which caused earlier

initiation and completion of accumulator injection as shown in Fig.13.

-8-
The secondary side pressure also agrees well with the experimental behavior up to 50 sec, after which there is significant underprediction

as shown in Fig.6.

The break flow at the cold leg shows overall agreement with the experiment except for the duration of 15 to 40 sec as shown in Fig.7. The

difference during this period, which corresponds to the accumulator injection phase, can be considered as noticeable ECC bypasses through the

crossflow junctions between the intact side and broken side of the downcomer and upper annulus, which were not observed in experiment [7].

Figures from 24 to 30 present the calculated mass flow rates at the inlet of downcomer, at the inlet of upper annulus, at the downcomer crossflow junction 3722, J724, J726 and 3728, and at the inlet to the core

from lower plenum, repectively. According to these figures, flow

oscillations with high frequencies and large amplitudes can be observed

after about 15 sec. From these observations, the sudden oscillation of

the cold leg mass flow rate during 15 to 40 sec in the Fig.7, seems

to be caused by the sum of these oscillatory EGC bypass flows. The

oscillation of the ECC bypass flow may be due to the numerical oscillation associated with the current nodalization.

For the hot leg flow in both broken and intact loops, Fig.8 and Fig.l0

show comparisons with experiment. In Fig.l0, two kinds of deviations

from the experimental behavior are found; the first one is a negative

flow until 25 sec, and the second one is a oscillation after about

40 sec. The positive flows of the experiment during 0 to 20 sec can

be explained as 'mirror image' of negative flow in the sense that the

negative flow can not be measured in the experiment [7], and that the

magnitude was almost same as the experiment [7]. The second deviation,

namely, oscillation can be considered as a propagation of flow oscillation at the core inlet in Fig.27, which has a larger amplitude than

-9-
that at the downcomer inlet in Fig.24. The reason for these flow

oscillations can be regarded as an over-prediction of the interfacial

friction in the rod bundle geometry [10]. As shown in Fig.31, the

collapsed core liquid level has a similar oscillation especially in

the period after quenching (at about 60 sec).

The effect of the over-predicted interfacial friction on the flow at

broken loop hot leg was found to be smaller than that at the intact

loop because larger values of the foward and reverse form loss factors

were used for the broken side junction than those for the intact side

junction ( 0.738 and 1.23 for broken side junction versus 0.1 and 0.1,

for intact side one ).

The mass flow rate at PCP discharge in the intact loop cold leg is

provided in Fig.9, showing a partly good agreement with the experiment.

A poor prediction of experimental behavior was found during 30 to 60

sec, which corresponds to a period for which the PCP speed was underpredicted as shown in Fig.12. A lower estimate of mass flow can be

considered to be caused by the poor prediction of pump speed from these

two figures. In Fig.11, several jumps in the calculated coolant density

were found after about 40 sec., which also can be regarded as the results from the over-prediction of interfacial drag in the rod bundle in

the sense that the oscillation mode was similar to that of the mass

flow rate in Fig.l0. Similar jumping behavior was found in the calculated pump speed as shown in the Fig.12, which also might be related

to the problem of interfacial friction. From the sensitivity study

to be discussed in the later chapter, it will be demonstrated that the

correction of the interfacial friction in the rod bundle can reduce the

magnitudse of oscillation in mass flow and pump spped, etc.

- 10 -
4.2.2 Thermal Behavior

Fig.14 and 15 present the comparisons of the calculated coolant temperatures in the upper and lower plenums with experiment. The code underpredicted both temperatures from about 25 seconds. The reason for

under-prediction can be considered as the earlier depressurization in

the upper plenum, yielding lower saturation temperature.

Two downcomer coolant temperatures are also showing the same

behaviors as indicated in Fig.16 and 17.

Fig.18 compares the calculated temperature with the experiment at the

fuel centerline at 27 inches from the bottom of the core. The comparis shows a good overall agreement.

The cladding temperatures in hot assembly predicted in the base case

calculation are compared with those in the experiment for the axial

locations of 5, 21, 27, 39 and 54 inches from the bottom of core in

Fig.19 to Fig.23, respectively. From these comparisons, the following

behaviors are found :

1. A later departure of nucleate boiling(DNB) for all axial locations

than experiment in Fig.19 to Fig.21

2. A lower heat up during the blowdown phase and a lower peak clad

temperature (PCT) than the experiment (926.4 K vs. 1077 K) shown

in Fig.20 and Fig.21

3. No heat up and no top-down quenching in the higher part of the

core (Fig.23 and 24, see also Table 2)

4. Larger amplitude oscillations than those in the experiment at the

locations with high LHGR during reflood phase (Fig.21 and 22)

5. Lower quenching temperatures than experiment for all locations

One of the reasons for these behaviors seems to be a single core

flow channel modelling used in this base case calculation. Acccording

- 11 -
to an experiment L2-5 data report[7], the thermal behaviors of cladding

in the central fuel assembly(Assembly 5) are quite different from those

in other parts (peripheral assemblies). To describe these two different

behaviors accurately, the core needs to be modelled as two separated

flow channels, hot and average channel.

The oscillations in the cladding temperature at 21 and 27 inches

during the reflood phase must be closely linked with the oscillation

of the collapsed liquid level of the core in Fig.31.

The absence of the top-down quenching and the lower estimation of reflood quenching temperature can be looked upon as the defiencies of the

current code, as reported in the reference(IlJ.

To match the experimental values more closely, finer nodalizations

in the axial direction are needed so that the volume centers are

located exactly at the measuring point with the same LHGR as used

in the experiment for each corresponding heat structure.

- 12 -
5. Nodalization and Sensitivity Study

5.1 Scope of Nodalization and Sensitivity Study

From the discussions in the previous chapters, it is shown that some

nodalization changes and code model changes are needed to predict the

phenomena accurately. Four cases of calculations were thus performed

to determine and to quantify the effects of the nodalization and model

changes on the thermal and hydrodynamic behaviors.

For nodalization study, three cases of different nodalization of the

downcomer and core were tested. In the first case (Case A) the core

was modelled with twelve volumes of equal length and the split downcomer model with only one crossflow junction was used to reduce the

unrealistic ECC bypass and oscillations,

In second case (Case B), the core was modelled with fourteen volumes

in a single channel with unequal volume lengths to match the measuring

point exactly. The other conditions are the same as for Case A .

Two core channel model was implemented in Case C in which there

was no crossflow junction between the hot channel and the average one.

The hot and average channels are divided by 14 and 6 volumes with

unequal lengths, respectively. The flow in the hot channel was 17 %

of the total core flow. Fig.32 shows the reactor vessel nodalizations

for each case while Fig.33 shows the discretization of core channel

into 14 volumes.

For a sensitivity study (Case D), an updated version from RELAP5/MODZ

Cycle 36.04 was used to recalculate a Case C. This update was made

with the PSI-UPDATE EIR-83 [111 and designated as Special MOD2. Table 8

summarizes the major items in EIR-83. This updates also includes change

- 13 -
of the limit used in the criteria of early blowdown rewet. Since

the early return to the nucleate boiling (REWET) was not observed in

the Experiment L2-5 during which pumps were coasted down, this update

is expected to have little effect on calculation. The effectiveness of

EIR-83 was reported for assessment against NEPTUN and FLECHT-SEASET in

reference[ll]. The full update list is presented in Appendix D.

Table 9 summarizes the calculation conditions for nodalization and

sensitivity studies.

5.2 Discussions on Nodalization and Sensitivity Study

5.2.1 Crossflow Junction in Downcomer

As mentioned previously, the modelling with one crossflow junction between broken side and intact side downcomer was tested in Case A.

Fig.34 shows a comparison of the mass flow rate at the broken loop

cold leg between the base case and Case A. The figure shows that there

is a noticeable reduction in the ECC bypass flow caused by deleting the

crossflow junctions.

This effect can be described in terms of downcomer liquid level in

Fig.35, which shows that there is a difference in liquid level between

the intact side and the broken side downcomer during 20 to 30 sec.

Fig.36 shows that the minimum water level in Case A is higher than that

in the base case.

A less break flow yielded a less depressurization, and the primary

system pressure was closer to the experiment than the base case, as

shown in Fig.37.

In Fig.38, the comparison of the collapsed liquid level in the core

- 14 -
is presented. From this comparison, it is shown that the core was fully

covered, even though momentarily, with water at about 45 sec in Case A,

while the core was re-emptied at that time in the base case. Because

of this difference, the quenching time was sooner in Case A than that

of the base case as shown in Fig.39 for cladding temperatures at the

27 inch elevation.

The mass flow rate in the intact loop hot leg, however, still shows a

oscillatory behavior after 40 sec.

5.2.2 Refinement of Core Nodalization

Core nodalization was revised in Case B, i.e, 14 volumes with unequal

length with no other changes from Case A.

The predicted primary system pressure was almost the same as that of

Case B, as shown in figure 40.

In the area of thermal behavior, little difference was found, as

shown in Fig.41 and 42, which present comparisons of cladding temperatures at 21 inches and 27 inches, repectively, with those of CASE A.

These comparisons show that the predicitions in Case B are somewhat

closer to the experiment. However, the fundamental behaviors are poorly

predicted in both cases.

5.2.3 Two Channels in Core Nodalization

In Case C, the core was modelled by two independent channels. Nodalization in hot channel was basically the same as in Case B.

Fig.43 and 44 show comparisons of cladding temperatures calculated

in the base case, Case B and Case C at 21, 27 inches, respectively.

As shown in these comparisons, the behaviors of cladding temperature in

- 15 -
Case C are considerably closer to the experiment with earlier DNB and

higher heat up than those in single channel cases. From these figures

the effect of two core channel on the core response can be clearly

seen.

Hot channel effects, however, are not cleary demonstrated in the

lower part of the core as shown in Fig.45 which shows cladding

temperatures at 5 inches. The reason for this ineffectiveness can be explained in terms of core collapsed liquid level in Fig.46. The level in

the hot channel did not fully drop in the blowdown phase but again

moved up to 0.4 m in 10 sec; i.e., a partial rewet which was not

observed in the experiment.

At the higher location of 43 inches, the early heat up vanished and

a later DNB was found even in Case C than experiment as shown in

Fig.47.

The hydraulic behavior of primary system are found to be almost the

same as those in Case B as shown in Fig.48.

5.3 Discussions on Sensitivity Study

As mentioned previously, the Special MOD2 code was tested to recalculate Case C (Case D).

Fig.49 shows a comparison of mass flow rate at the intact loop hot

leg, which shows a considerable reduction in flow oscillations after 40

sec, as compared with Case C. This stabilization occurs in the

collapsed liquid level in the hot channel of the core as shown in

Fig.50. This improvement is probably due to the correction of the

interfacial friction in the rod bunble in PSI update.

Fig.51 shows the comparison of primary pump velocity between the Case

C and the Case D. It is shown that pump speed also was stablized by the

- 16 -
update code.

Fig.52 and 53 show comparisons of cladding temperatures at 21 and 27

inch elevations with CASE C. Quenching temperatures at 21 and 27 inch

location in Case D were predicted to be closer to the experiment, and

thermal responses in Case D to be more stablized than the Case C though

cladding temperatures in the Case D were higher and more deviated from

the experiment than those in the Case C.

- 17 -
6. Run Statistics

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

875 Series at KAERI, with NOS Version 2.6.1.

Fig.54 presents a plot of the required CPU time for the transient time

in the base case calculation. The time step size in the base calculation

is also plotted in Fig.55. The user-specified maximum time step was 0.01

sec in the base case calculation as recommended in reference[1]. The

computational efficiency is summarized in Table 10 from the major edit

for a base case calculation and can be calculated as follows.

Computer time,

Number of time step,

Number of volume

Transient real time

CPU 2528.43 - 3.2 = 2525.23 , sec

DT = 13407 - 252 = 13157

C= 128'

RT=120 , sec

Grind time = CPU / ( C * DT ) = 0.01498 CPU sec/vol.step

- 18 -
7. Conclusions

RELAP5/MOD2 Cycle 36.04 code was assessed using LOFT L2-5 LBLOCA test.

A base case calculation including the single core and split downcomer

modelling with crossflow junctions was carried out. To determine the

effect of nodalization change and code model change and to quantify

the effects on the hydraulic and thermal behavior, three cases of nodalization of downcomer and core were tested. In addition, a sensitivity

calculation was performed using a corrected code updated from RELAP5/

MOD2 Cycle 36.04 with PSI. As a result of the present calculations,

the following conclusions are obtained.

1) Using LOFT L2-5 Experiment, a base case calculation and a nodalization and sensitivity study were successfully executed from the

viewpoint of the specific objectives and the requirements of ICAP

assessment activity.

2) In the base case calculation using a nodalization of single core

and split downcomer with crossflow junctions, an unrealistic ECC

bypass flow was found and a hot channel behavior was not predicted.

The code deficiencies of over-prediction of interfacial friction

and core quenching temperature were also found in the current

frozen code.

3) A split downcomer model without crossflow junctions except for a

connection with upper annulus was demonstrated to be effective in

reducing the unrealistic ECC bypass flow. The refinement of the

axial nodalization in the core has little effect on the core

- 19 -
thermal response. Two core channel modelling was recommended to

describe the hot channel behavior accurately.

4) The PSI-updated version which includes the correction of the

interfacial friction and the reflood heat transfer correlations

was found to be effective in predicting the thermal-hydraulic behaviors during LBLOCA.

- 20 -
References

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

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

2. Ransom, V.H. et al, RELAP5/MOD2 Code Manual,

Vol. 3 : Developmental Assessment Problems, EGG-TFM-7952, 1987.

3. Weaver, W.L, RELAP5/MOD3 Status,

the 5th ICAP Specialist Meeting March 14, 1989, JAERI, Japan

4. USNRC, International Code Assessment and Application Progran,

Annual Report, NUREG-1270, vol 1, March 1987.

5. Adams J.P., Quick Look Report on LOFT Nuclear Experiment L2-5

EGG-LOFT-5921, June 1982

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

7. Bayless, P.D and Divine, J.M., Experiment Data Report for LOFT Large Break

Loss of Coolant Experiment L2-5, NUREG/CR-2826, EGG-2210, August 1982

8. Seeberger, RELAP5/MOD2-RP2 Modification of Cycle 36.04,

.U811-87-3065a, Dec. 22, 1987, Kraftwerk Union, Erlangen

9. Demmie, P.N., Chen, T.H and Behling, S.R., Best Estimate Prediction

for LOFT Nuclear Experiment L2-5, EGG-LOFT-5869, May 1982

10. 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

11. Richner M., Analytis, G.Th., Aksan, S.N.,

Assessment of RELAP5/MOD2 Cycle 36.02 using NEPTUN Reflooding

Experimental Data, Draft of ICAP report, PSI, Switzerland, Apr. 1989

- 21 -
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* , kg/s 192.4 192.4

Hot leg pressure* , MPa 14.94 14.918

Core delta T , K 33.1 33.03

Cold leg temperature* ,K 556.6 556.49

-Reactor Vessel

Power level , MW 36.0 35.69

Max.Linear HGR , kW/m 40.1 39.8

-Pressurizer

Liquid temperature , K 615 614.7

Pressure , MPa 14.94 14.94

Liquid level* , m 1.14 .1.1389

-Steam Generator sec.side

Saturation temperature , K 547.1 546.22

Pressure ; MPa 5.85 5.78

Mass flow rate , kg/s 19.1 18.7

Level* , m 3.1293 3.12

Note * : Setpoint in steady state controllers

- 22 -
Table 2 Summary of comparison of the sequence of events

between the measured and the calculated in base case

Event Measured,sec Calculated,sec

/Uncertainty

Experiment initiated 0. 0.

End of Subcooled Blowdown 0.043/0.01 0.01

Reactor Scrammed 0.28/0.2 0.015

Clad Temperatur deviated

from saturation 0.91/0.2 3.4

Primary Pump Coastdown initiated* 0.94/0.5 0.94

End of Subcooled Break flow(cold leg) 3.4/0.5 2.55

Top-down Quench initiated 12.1/1.0 **

Pressurizer Empty 16.3/2.0 13.6

Accumulator Injection 17.3/0.7 15.0

End of Top-down Quench 22.7/1.0 **

HPIS initiated* 24.0 24.0

Peak Clad Temperature-reached 28.5/0.5 47.0

Lower Plenum Refill 31.2/1.0 30.9

LPIS initiated* 37.0/0.5 37.0

Accumulator Empty 49.4/1.5 33.0

Core Reflood completed 55.3/1.5 63.0

Core Cladding Quenched 65.0/2.0 67.0

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

- 23 -
Table 3. Uncertainties of Measurements

item type range uncertainty

Primary system pressure

Secondary system pressure

Coolant Temperature

Mass Flow Rate

Broken loop cold leg

Broken loop hot leg

Intact loop cold leg

intact loop hot leg

Density

Cladding Temperature

Accumulator Liquid Level

Primary Coolant Pump Speed

Reactor Power

MM

M

C

C

M

M

C

M

0.1 -

0.1 -

310 -

420 -

0-

0-

0-

21 MPa

7.0 MPa

970 K

1530 K

3.5 m

4500 RPM

62.5 MWt

0.12 MPa

0.087 MPa

4.3 K

62.0 kg/s

23.0 kg/s

32.0 kg/s

30.0 kg/s

0.10 Mg/m

6 - 13 K [1]

0.007 m

8.2 RPM

2.0 MWt

Note. M : Measured data,

C : Computed varibles derived from the measured data

[1] For cladding temperatures, uncertainties vary within

this range depending on the measurement locations
Table 4. Summary of corrected items in RELAP5/MOD2 Cycle 36.04

No. Subroutine Reasons Reference

1 RACCUM To correct indexing error Update KWU-01

2 IHTCMP To correct indexing error in Update SKI01

gap pressure calculation in CDC

version

3 IRFLHT To correct a geometric pointer to Update SKIO1

allow reflood to work with/out

change of heat slab associated

with reflood in RESTART case

- 25 -
Table 5. Summary of the important items in nodalization

items description Reference [9]

-Primary Coolant System (Intact Loop)

Number of volumes in

hot leg from RV outlet to S/G inlet

Steam Generator U tube

cold leg from S/0 outlet to RV inlet

Primary Coolant Pump

-Primary Coolant System (Broken Loop)

Number of volumes in

hot leg from RV outlet to S/G simulator

Steam Generator simulator

cold leg from RV outlet to BST inlet

Reflood Assist Bypass line

-Blowdown Suppretion Tank

Number of volume in connection to cold leg

Number of volume in connection to hot leg

-Emergence Core Cooling System

Accumulator

High Pressure Injection System

Low Pressure Injection System

Number of volume in ECC line

-Pressurizer System

Number of volume in dome

Number of volume in surgeline to hot leg

Number of volume in spray line from cold leg

-Steam Generator Secondary System

Number of volume in boiler

Separator

Number of volume in Steam line

Number of volume in Liquid Fall Back line

Number of volume in S/G downcomer

Feedwater Tank

Line from MSIV to Air-cooled Condenser

-Reactor Vessel

Core

Number of flow channel

Number of volume per channel

Number of heat structure component

Number of volume per H.S. component

Gap conductance model

Reflood option P

Number of mesh point in heat structure

Number of maximum fine mesh

Number of volume in core bypass compnt

Core Bypass flow ratio

Downcomer

Number of flow channel

Number of volume per flow channel

Number of crossflow junctions for

downcomer bypass

7

8

18

2

3

8

4

6

1 TMDPVOL

1 TMDPVOL

1 ACCUN

1 TMDPVOL

1 TMDPVOL

2

8

3

1

5

1 SEPARATOR

3

2

4

1 TMDPVOL

1

1

12

2

12

used

1

ressure *

10

8

3

5%

2

5

4

same

same

same

1 TMDPVOL

same

same

same

2

6

3

6

none

none

10

none

3

5%

2

5

5

Note * : Reflood option was not used even in reference [2),

Option used in base calculation : Pressure at core top less than 0.1 MPa

- 26 -
Table 6. Summary of the boundary conditions for a base case

item description

* Primary coolant system -Primary coolant system Primary Coolant Pump *

Containment *

-Secondary Coolant System Feedwater

Air-cooled Condenser

•ECC System

Accumulator *

HPIS

LPIS

-Reactor

Axial

Power

Trip time of 0.94 sec

changed from 1.74 for accurate description

Pressure chaged from 0.1 IPa to simulate

the measurement PE-SV-060 accurately

Tablet form of mass flow rate vs. pressure

2.0 MPa

Empty level changed to 0.94 m from 1.04 m

for accurate description

Tablet form of mass flow rate vs. pressure

Tablet form of mass flow rate vs. pressure

From experiment data, see Fig.3

Changed to aviod the measurement uncertainty

:measurement RE-T-77-1A2 plus L2-5 posttest decay heat curve, see Fig.4

Power table changed to zero in transient

calculation witout any change of H.S.

Extended the lower limit to 300 K from

380 K

Vessel Core

power shape history *

-Others *

Pressurizer heater

Thermal conductivy

table

Note * : Changed items 4

from reference[2J

- 27 -
Table 7. List of the important assessment parameters

description experiment ID[7] calculation No.of Fig.

Primary system pressure

S/6 secondary system pressure

Mass flow rate at broken loop

cold leg

Mass flow rate at broken loop

hot leg

Mass flow rate at intact loop

cold leg

Mass flow rate at intact loop

hot leg

Primary system density at

intact loop hot leg

Primary coolant pump speed

Accumulator liquid level

Coolant temperature at

upper plenum

Coolant temperature at

lower plenum

Coolant temperature at

broken side downcomer, 4.8 m

Coolant temperature at

broken side downcomer, 0.85 m

Fuel Centerline temperature

at hot fuel, 27 inches

Cladding Temperature at hot

fuel, 5 inches

Cladding temperature at hot

fuel, 21 inches

Cladding temperature at hot

fuel, 27 inches

Cladding temperature at hot

fuel, 39 inches

Cladding temperature at hot

fuel, 54 inches

PE-1-UP-OOA1

PE-SGS-O01

FR-BL-001

FR-BR-002

FR-PC-101

FR-PC-201

DE-PC-205

RPE-PC-002

LE-ECC-OIA

TE-4UP-001

TE-4LP-001

TE-IST-001

TE-1ST-007

TC-5D09-27

TE-5106-005

TE-5106-021

TE-5104-027

TE-5106-039

TE-5106-054

P 250-01

P 530-01

MFLOWJ 340-01

MFLOWJ 305-01

MFLOWJ 180-01

MFLOWJ 100-01

RHO 100-01

PMPVEL 165

CNTRLVAR 4

TEMPF 250-01

TEMPF 215-01

TEMPF 712-01

TEMPF 718-01

HTTEMP 21-0501

HTTEMP 21-0110

TfTEMP 21-0410

HTTEMP 21-0510

HTTEMP 21-0810

II•TTEMP 21-1010

5

6

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

- 28 -
Table 8. Updated items in PSI-EIR 83 [11I

item description effect

heat transfer Correction of Modified-Bromley correlation Decrease heat

coefficient in film boiling to original form with co- transfer coefficient in medium/high flooding rate efficient

interfacial New correlation from CATHARE code for Decrease interfriction interfacial friction in bubbly and slug facial drag flow regime

heat transfer Implementation of Forslund/Rosenhow formula Stabilize numcoefficient for the reflood dispersed film boiling erical vibration

heat transfer

interfacial Reduction of interfacial friction in rod Reduce too high drag bundle in inverted slug flow regime by void fraction

factor of 0.4, in dispersed flow and

annular mist flow regime by factor 0.5

criteria Changing the criterion for predry-out Reduce unphysical interfacial friction correlation near oscillation

quench front

quenching Changing an exponent in the Weisman Increase quenching

temperature reflood transition film boiling correla- temperature tion multiply a factor to Modified-Bromley heat transfer correlation

- 29 -
Table 9. Summary of the calculation conditions for

nodalization and sensitivity study

item Base-case CASE A CASE B CASE C CASE D

No.of core channel 1 1 1 2 2

No.of volume

average channel 12 12 14 6 6

hot channel none none none 14 14

No.of crossflow

junction in DC 4 0 0 .0 0

Used code C.36.04 C.36.04 C.36.04 C.36.04 Special*

Note * : Special MOD2 : RELJP5/MOD2 Cycle 36.04 plus PSI Update

- 30 -
Table 10. Run statistics data in base case

Transient time CPU time Attempted Repeated Mass error

(sec) (sec) ADV ADV (kg)

0 3.2

10 187.855 1040 13 -1.28

20 365.525 2040 13 -0.9371

30 566.903 3142 15 -0.929

40 866.809 4703 88 0.269

50 1081.10 5813 104 0.277

60 1281.74 6877 131 0.672

70 1484.11 7924 141 1.043

80 1685.57 9004 159 0.931

90 1895.16 10109 170 0.886

100 2109.97 11239 202 0.8155

110 2314.75 12300 222 0.934

120 2528.43 13407 252 2.12

- 31 -
Intact loop Broken loop

BL-1

experimental

measurement

valve

(2)

I

I

PC-1 - experimental

measurement

station plenum

Reactor vessel INEL 3 0591

Fig. 1 Axonometric configuration of LOFT L2-5 test
-9E-- sflow Jmtion

kmrctaoon

STCAM GENERATrPPWF ST)@ATO

PESSLURIER

GENERATOR

Bad-up Cyding Hequ~r

2

REACT1R VESSL

ILDVMMV SLWPRESMM~ TAWC

I

TAWK

CHARGING

INTACT LMP BRKEN LOP

Fig.2 Nodalization diagram for base case calculation of LOFT L2-5 test
50

0

a

0

C

0

4j

a

0

L

C

40

30

I 20

!

10

0

0 0.2 0.4 0.6 0.8 1 1.2 1.4

Height From The Bottom Of Core (M)

Axial power distribution in base case calculation

1.6

Fig. 3 of L2-5 test
1

0.9 - 132-5 Posttest

- L2-5 Posttest + Decay Heat

0.8 -

0.7 -

0

o 0.6 - 0.

U

.10

"C 0.5 - 0

o 0.4 - E

CJ1

0.3 -

0.2 -

0.1 -

0 0 -I I I Ii Ii

0 2 4 6 8 10

Time After Rupture (Sec)

Fig.4 Power history ii base case calculation of LZ-5 test
'5

15 - n Exp. PE-1-UP-OOA1

- Col. RELAP5

13

12

11 "

10

9

LO 8

0-' 9-7

0. 6

n 5 5

4

3

2

1

0 - T I I I I

0 20 40 60 80 100 120

Time After Rupture (See)

Fig.5 Conparison of primary system pressure

between the"base case calculation and the experdmnt
6

5.9 L- IAF. 4 J 1~..J 

-Col. RELAP5

5.8

5.7

o 5.6

5.5

In 5.4-

5.3

5.2

5.1

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.6 Comparison of secondary system pressure

between the base case calculation and the experiment
600 I

o Exp. FR-BL-001

-Col. RELAP5

500 -

I]

400

U

N

0b

U

.4.,

a

0

U

U

00 a

300 -

200 -

100 -

0

-100

I

i L &ý j I ý I kWIUWIkAhV%'VW%6 AA.,A .- A -~ A

iI, . I'J , rI LJI 1"

I

2 I

20 40 0

S I I I I I

60 80 100

I

120

Time After Rupture (Sec)

Comparison of mass flow rate at broken loop cold leg between the base case calculation and the experimentFig.7
300 -

0 Exp. FR-BL-002

250 - Col. RELAP5

200

150

C

-4,

100

0

50-

:0

0-

-50

-100 I I I I I I I I

0 20 40 60 80 100 120

rime After Rupture (Sec)

Fig.8 Comparison of mass flow rate at broken loop hot leg between the base case calculation and the experiment
400

300

200

0

010

0~ - 100 -

-100 1 I 1 I 1

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.9 Comparison of mass flow rate at intact loop cold leg between the base case calculation and the experiment
400

300 - Col. RELAP5

200

-Y 100

%op e0

| :-. 0

, -100 I:A I0

-200

-300

-400 - I i i -

0 20 40 60.. 80 100 120

Time After Rupture (Sec)

Fig. 10 Comparison of mass flow rate at intact loop hot leg

between the base case calculation and the experiment
1

0.9 0 Exp. DE-PC-205

- Cal. RELAP5

0.8 -

0.7 4

E 0.6

0.5

00.4

0.43

0.2

o.1

-0.2 1u

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig. 11 Comparison of primary system density at intact loop hot leg

between the base case calculation and the experiment
200 -

190 -

180 - 03 Exp. RPE-PC-002

170 - Cal. RELAP5

160 -

150 -

140 -

U), 130

'0 120 0

110

v00 00 100

0. 90

• 80 -

E 70

(L n.60 -

50 -

40 -

30-

20 -

10 -

0

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.12 Comparison of primary coolant pump speed

between the base case calculation and the experiment
2.5 -

2.4 -

2.3 - calculation -

2.2 - experiment ...... 2.1 -

2

1.9

1.8

E• 1.7 -

1.6 -

1.5 -

o1.4

1.3 -

I:3 1.2 -

1.1

0.9

0.8

0.7

0.6

0.5

-20 0 20 40 60 80 100 120

TIME AFTER RUPTURE (See)

Fig.13 Comparison of liquid level in accumulator

between the base case calculation and the experiment
600 i

580 13 Exp. TE-1UP-O01

560 -- Col. RELAP5

540

520

500

480

a

n 460 -

E

E 440 -

CJ 420 - 0

0 400 -

380 -

360

340 -

320 -

300

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.14 Comparison of coolant temperature in upper plenum

between the base case calculation and the experiment
600

580 -3 Exp. TE-1LP-O01

5Cal. RELAP5 560 "

540

520

500

480

*e 460

E* 440 - 420 -

42

0 400

380 -

360 -

340 -

320 -

300 -

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.15 Comparison of coolant temperature in lower plenum

between the base case calculation and the experiment
600 -

580 -3 Exp. TE-1ST-O01

560 - Cal. RELAP5

540

520

500

480 -

o 460 - 0.

E 440 -

C 420 -

0

- 400 - 0

380 -

360 -

340

- 320

300 -

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.16 Comparison of coolant temperature at downcomer inlet

between the base case calculation and the experiment
600 -

580 - 0 Exp. TE-1ST-007

50 --- Cal. RELAP5 560-

540-

520 -

. .500

480 -

* 460 -

o 440 I.-

C c 420 -

0 400 - 0

380 -

360 -

340

320

300-

0 20 40 60 80 100 120

Time After Rupture (See)

Fig.17 Comparison of coolant temperature at downcomer outlet

between the base case calculation and the experiment
1.8

1.7 -3 Exp. TC-5D09-27

1.6 - Cal. RELAP5

1.5

1.4

1.3

1.2

'5 1.1

E 0

0.9 -

0.8 -

0.7 -

0.6

0.5

0.4 - I 

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.18 Comparison of fuel centerline temperature at 27 inches

between the base case calculation and the experiment
1

0.9 E3 Exp.TE-5104-00

CaI.RELAP5

0.8-

0.7

0-

0.6

C=)

0 0.5

0.4 .

0.3 - 1 i 1 1 I i i

0 20 40 60 80 100

Time after Rupture (Sec)

Fig.19 Comparison of cladding temperature at 5 inches of hot fuel

between the base case calculation and the experiment
1.4

1.3 - 0 Exp. TE-5106-021 - Cal. RELAP5

1.2

v 1.1

L0 ScC

E• 0.9 .

0

, 0o, .8 "l

U • 0.7 -

0.6

0.5

0.4- - i i i

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.20 Comparison of cladding temperature at 21 inches of hot fuel

between the base case calculation and the experiment
1.5

1.4 - M Exp. TE-5104-027

-- Cal. RELAP5

1.3 -

1.2 -

1.1 - 0

Ole 0. - 0.9

uC,. 0.8-

"o0 0.7-

0.6-

0.5-

0.4

0.3

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.21 Comparison of cladding temperature at 27 inches of hot fuel

between the base case calculation and the experiment
1.2

lol -- • 1 . .. . . . - Cal. RELAP5

0.9

0.8 -

00.7 -

oo "u 0.6-

00

0.5

0.4

0.3 i

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.22 Comparison of cladding temperature at 39 inches of hot fuel

between the base case calculation and the experiment
900

800 -

700 - 0

L

:3

E 600

'0

C.n "0500-

0.

400

300

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.23 Comparison of cladding temperature at 54 inches of hot fuel

between the base case calculation and the experiment
400

300 -

200 -

(I,

100

0 -

-,00

-200

-300 -

-40 0 - I I

0 20 40 60 80 100 120

TIME AFTER RUPTURE (Sac)

Fig.24 Mass flow rate at the inlet of intact side downcomer in base case
U,

400

300

200

100

0

-100

-200

-300

-400 I I I I I I I I I I

0i,

¢j'0

!m

0 20 40 60 80

TIME AFTER RUPTURE (Sec)

100 120

Fig. 25 Mass flow rate at the inlet of intact side upper annulus in base case
400

300

200

100

00

C- 100

-200

-300 -

--400 ,

0 20 40 60 so 100 120

TIME AFTER RUPTURE (Sec)

Fig.26 Mass flow rate at the bypass junction J722 in base case
U,

0

COD 0.0'

400

300

200

100

0

-100

-200

-300

-400

0 20 40 60 80 100 120

TIME AFTER RUPTURE (See)

Fig.27 Mass flow rate at the bypass junction J724 in base case
U,

0'

0

400

300

200

100

0

-100

-200

-300

-400

I

¢j'l

0 20 40 60 80 100

TIME AFTER RUPTURE (Sec)

120

Fig.28 Mass flow rate at the bypass junction J726 in base case
400 -

300 -

200 -

100

0-

-100

-200

-300

-400-

0 20 40 60. 80 100 120

TIME AFTER RUPTURE (Sec)

Fig.29 Mass flow rate at the bypass junction J728 in base case
0

400

300

200

100

0

-100

-200

-300

-400

0C) I

0 20 40 60 80 100

TIME AFTER RUPTURE (Sac)

120

Fig.30 Mass flow rate to the core from the lower plenum in base case
4

3.5

3

2.5

E

2J core top

1.5

I

0.5

0-

0 20 40 60 80 100 120

TIME AFTER RUPTURE (Sec)

Fig.31 Collapsed liquid level in the core in base case
I j. I8, I

Q) CASE A B) CASE B c) CASE C

Flg.32 Compoarison of nodalizotlon In the core for Coase A, B ond C
HOT CHANNEL AVERAGE CHANNEL

U

i.

L

0

U

(4-

0

E

0

0

_Q

0; L

Ci UC-

-d

14

13

12

11

10

9

7

5

4

3

1

- 061

- 054

- 049

- 043

- 037

- 031

- 027

- 024

- 021

- 018

- 015

- 009

- 005

- 002

6

5

- 061

-045

- 031

- 021

- 010

-003

4

3

2

1

FIg.33 DlscretIzatlon scheme of hot and average channet of the core
&

U,

!~

0)

4-

400

350

300

250

200

150

100

50

0

-50

4 8 12 16 20 24 28 32 36

Time after rupture (sec)

Fig.34 Comparison of mass flow, rate at broken

between base case and CASE A

loop cold leg
6

5

4

3

0

0

CrI _2

o - r"-'-1-'

-20 0 20 40 60,

TIME AFTER RUPTURE (Sac)

s0 100 120

Fig.35 Collapsed liquid level of the downcomer in CASE A
6

center of cold leg nozzle

5

4.

c' 2 -

1 -

Base case calculation

CASE A calculation

0 -- I I--- I | i-

-20 0 20 40 80 80 100 120

TIME AFTER RUPTURE (Sac)

Fig.36 Comparison of liquid level in the intact side downcomer

between base case and CASE A
16

15 - 0 Exp. PE-1-UP-OOA1

14 A BASE CASE ( 1 Core 12 Vol. Cross)

13- 13 CASE A (1 Core 12 Vol. No-Cross)

12

11

,• 10 0

9

U'.- 7-

E.2

0. 6

00 5

4

3

2

1 -

0 - ---- -I - I T

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.37 Comparison of primary system pressure

between base case and CASE A
4

1.5 CASE A calculation

E 2.5 -

,3

• 

core top

l. 5 1.5

0.5 .1

0 "

-20 0 20 40 60 80 100 120

TIME AFTER RUPTURE (See)

Fig.38 Comparison of liquid level in the core

between base case and CASE A
1.4

1.3 A BASE CASE 1 Core12 Vol. Cross

.2- CASE A (1 Core 12 Vol. No-Cross)

~1.1

e 1

C.c 0.9

0.

•o 0.7

0.6

0.5

0.4 -

0 20 40 60 80 100 120

Time After Rupture (Sec)

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

between base case and CASE A
16

15 " 13 Exp. PE-1-UP-OOA1

14 A BASE CASE ( 1 Core 12 Vol. Cross)

13 V CASE A (1 Core 12 Vol. No-Cross) CASE B (1 Core 14 Vol. No-Cross)

12

11 j

J_% 10

0

0) 9

w 5

4.

3

2

1

00

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.40 Comparison of primary system pressure

in base case, CASE A and CASE B
1.4

1 - E r.A.PA. I E.--JIUU--u I

BASE CASE ( 1 Core 12 Vol. Cross )

A CASE A (1 Core 12 Vol. No-Cross)

1.2 V CASE B (1 Core 14 Vol. No-Cross)

X 1.1

0.0

m0.9

I 0.5

"0C 0.7

i • 0.7

0.6

0.5

0.4

0 20 40 60 80 100 120

Time After Rupture (See)

Fig.41 Comparison of cladding temperature at 21 inches of hot fuel

in base case, CASE A and CASE B
e%

0

M

1.4

1.3

1.2

1.1

I

0.9

0.8

0.7

0.6

0.5

0.4

0.3

13 Exp. TE-5104-027

A BASE CASE ( 1 Core 12 Vol. Cross)

V CASE A (1 Core 12 Vol. No-Cross)

- CASE B (1 Core 14 Vol. No-Cross)

CA)

0 20 40 60 80 100 120

Time After Rupture (See)

Fig.42 Comparison of cladding temperature at 27 inches of hot fuel

in base case, CASE A and CASE B
Y..

0.

0

.C,

1.4

1.3

1.2

1.1

0.9

0.8

0.7

0.6

0.5

0.4

A

V

Exp. TE-5106-021

BASE CASE ( 1 Core 12 Vol. Cross)

CASE B (1 Core 14 Vol. No-Cross )

CASE C (2 Core 14 Vol. No-Cross)

I

0 20 40 60 80 100

Tme After Rupture (Sec)

Fig.43 Comparison of cladding temperature at 21 inches of ho'tfuel

in base'vcase, CASE 7Bt-and CASEIC"

120
1.4 -

0 Exp. TE-5104-027

1.3 A BASE CASE ( 1 Core 12 Vol. Cross) - CASE B (1 Core 14 Vol. No-Cross )

1.2 X CASE C (2 Core 14 Vol. No-Cross)

S1.1 -

E03

000.

Sc 0.9 -

0.8 -

CL

0.7 -

e o 0.6

0.4 - -.... . .

0.3

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.44 Comparison of cladding temperature at V7 inches of hot fuel

in base case, CASE B and CASE C
1

C

(L

0

0.9

0.8

0.7

0.6

0.5

0.4

0.3

I

I

0 20 40 60 80 100

Time after Rupture (Sec)

Fig.45 Comparison of

in base case,

cladding temperature at 5 inches

CASE B and CASE C

of hot fuel
2.6

2.4 -

2.2

2

1.8 Core Top

1.6

E 1.4

1.2

1 - I 

0.6

0.4 -11 , V

0,2

0-

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fiv.46 Collapsed liquid level in the hot channel of core in CASE C
1.1

1 - CASE B (1 Core 14 Vol. No-Cross)

A CASE C (2 Core 14 Vol. No-Cross)

0.9

0.8

E 30 0.7

, 0.6

0.5

0.4

0.3

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.47 Comparison of cladding temperature at 43.8 inches of hot fuel

between CASE B and CASE C
16

15

14

13

12

11

10

CL,-%

E.2

3

(L

9

8

7

6

5

4

3

2

1

0

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.48 Comparison of primary system pressure

between CASE B and CASE C
200

100

0

4J

0

0

0

0 CASE C calculation

-- CASE D calculation

a Experiment

I I I I

-1

I -100

-200

-300

0 20 40 .60 80 100 120

Time After Rupture (sec)

Fig.49 Compaiison of mass flow rate at intact loop hot leg between CASE C and CASE.D
2.6

2.4 CASE C (2 Core 14 Vol. No-Cross)

2.2 - CASE D (2 Core 14 Vol. No-Cross , Update)

2

1.8

1.6 Core Top

"E 1.4

> 1.2

1

00

0.8

0.6

0.4

0.2

0 20 40 60 80 100 120

lrime After Rupture (Sec)

Fig. 50 Comparison of liquid level in the hot channel of core

between CASE C and CASE D
150

0 Exp.RPE-PC-002

140 -

1 CaI.CASE C 130-

CaI.CASE D

120 -

110 -

o 100 -

90 -

80 -

60

*E

E 50 - f CL

40 -

30

20 -

0 . I1 1 1

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.51 Comparison of primary coolant pump velocity between CASE C and CASE D
1.4

M rý Tr-ring-noill

1.3 V CASE C ( 2 Core 14 Vol. No-Cross)

- CASE D ( 2 Core 14 Vol. No-Cross , Update )

1.2

~1.1 "

4a c .

200

E = 0.9 -

*0

C= 0.8 -

00 WA 0 0.7

0.6

0.5

0 .4 .

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.552 Comparison of cladding temperature at 21 inches of hot fuel between CASE C and CASE D
1.4

1.3 - X CASE C (2 Core 14 Vol. No-Cross)

- CASE D ( 2 Core 14 Vol. No-Cross , Update )

1.2 -

1. 1 -

0.9 -

0 0.8 -

•0..

C

0.0

C.) 0.6

0.5 -

0.4 -

0.3

0 20 40 60 80 100 120

Time After Rupture (Sec)

Fig.53 Comparison of cladding temperature at 27 inches of hot fuel

between CASE C and CASE D
2.6 -

2.4 -

2.2 -

2

1.8

o, 1.8

S'-1.4

Pa 1.2

co1

00

c-n 0.8

0.6

0.4 -

0.2

0 -- I I I I I I I i I

-20 0 20 40 60 80 100 120

TIME AFTER RUPTURE (Sec)

Fig.54 The required CPU time versus the advanced time

in base case calculation of L2-5 test
C,?

Iji

0.02 -

0.019 

-

0.018 

-

0.017 

-

0.016 

-

0.015 

-

0.014 

-

0.013 

-

0.012 

-

0.011 

-

0.01 

-

0.009 

-

0.008 

-

0.007 

-

0.006 

-

0.005 

- 0.004 -

0.003 

-

0.002 

-

0.001 

-

0 

-

00I

r FF

m 1W! I

-20 I 2 I 

I 20 40 I I I I I 

I 60 80 100 120

0

TIME AFTER RUPTURE (Sec)

Fig.55 Time step size of base case calculation of L2-5 test
Appendix

1

-191 -
APPENDIX A Update list for RELAP5/MODZ Cycle 36.04

/JOB

RM364B,T200.

/USER

ATTACH, OLDPL=REL364S.

PURGE,RE364BS/NA.

PURGE,RE364BX/NA.

PURGE,RE364BL/NA.

* IMPORTANT !! *

* THE UPDATE DIRECTIVE *

* SHOULD HAVE *COMPILE DEFINE

* AS THE FIRST DIERECTIVE

**** *** ** *** *** ** ***** *** ** *

UPDATE,N=RE364BS.

UPDATE,P=RE364BSOQ, C=R5SEG.

REPLACE,R5SEG.

RETURN,OLDPL.

*DEFINE,RE364BS.

RETURN,RE364BS.

ATTACH, ENVRLX=ENVR41X.

LIBRARY,ENVRLX.

SELECTA,COMPILE,COMP.

LIBRARY.

RETURN,ENVRLX.

REWIND,COMP.

FTN5, I=COMP,DO,ET,STATIC,OPT=Z,ROUND,LO=M/A/R/S,L=O.

RETURN,COMP.

REWIND,LGO.

ATTACH, RELAP51=REL364L.

GTR,RELAP51,ADD.REL/*

*DEFINE, RELAP50=RE364BL.

LIBEDIT,P=RELAP50, I=0,B=ADD,LO=F,U,C.

LIBEDIT,P=RELAP50,B=LGO,I=O,LO=F,U,C.

RETURN,NULL,LGO,RELAP5I.

RETURN,RLP5Fl, RLP5F2.

ATTACH,ENVRL=ENVR41L.

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

RFL,EC=200.

DEFINE,RE364BX.

SEGLOAD,-I=R5SEG,B-=RE364BX.

LDSET, LIB=RELAP50/ENVRL.

LDSET,PRESETA=NGINDEF,ERR=NONE,MAP=SB.

LDSET,STAT=RSTIN.

LIBLOAD,ENVRL, $HDR=$.

LIBLOAD,FTN5LIB, $FERCAP.$,$RPVCAP.$,$FTNRP2. $,$Q2NTRY.$.

NOGO.

PERMIT, RE364BX, KA41202.

RETURN,RELAP50,ENVRL,COMPILE.

SKIPKKX.

EXIT.

ENDIF,KKK.

DAYFILE,MIRRDAY.

REPLACE,IMRRDAY.

/EOR

*COMPILE DEFINE

*ID CBD3604

*D DMK3601.484

*D PLOTMD.24

- 88 -
901 FORMAT ('OPLOTFL SCRACH FILE GENERATED.') *COMPILE DEFINE,SEGDIR

*COMPILE RELAP5

*D RJW3603.23

DATA PTITLE/"RELAP5/2/3","6.04-NSC","REACTOR LO","SS OF COOL",

*/ ENDIF

*ID KWUOl ALREADY IMPLEMENTED IN RELAP50LDPL3604C,

WHICH IS USED AS BASIS

**/ CORRECTIONS OF INDEX IN SUBROUTINE RACCUM

*I RACCUM.618

IELV=I

*B DMK360O.581

,/ I=IELV

*COMPILE DEFINE,SEGDIR,RACCUM

*ID KWUO1

*1 RACCUM.618

IELV=I

*B DMK360Z.581

I=IELV

/ */ END OF KWU-UPDATES TO CYCLE 3604

*COMPILE DEFINE,SEGDIR

*IDENT SKI01

THESE UPDATES ARE RECOMMENDED BY SKI TO BE

IMPLEMENTED IN RELAP5/MOD2-36.04

*/ SOURCE: LETTER FROM STUDSVIK (MR.SANDERVAG)

*/ TO KWU (MR.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.MASK(43).AND.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..HEAT STRS ASSOCIATED WITH REFLOOD CANNOT BE ALTERED

ON RESTART AS IRFLHT IS NOW PROGRAMMED

*COMPILE IRFLHT

*1 IRFLHT.330

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

C HEAT STRUCTURE FILE CHANGED ON RESTART.

J=(.NOT.MASK(43).AND.IH) + IHT

J=(.NOT.MASK(43).AND.IHTPTR(J)) + IHT

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

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

*/ END OF UPDATES SKIO0

/EOR

*COMPILE SEGDIR

- 89 -
APPENDIX B A Base case input deck for a steady state calculation

/JOB

L25BSR1,T4000.

/USER

ATTACH,STH2XT, RE364BX.

DEFINE,RSTPLT=L25SR.

FILE, RSTPLTSBF=NO.

RFL,CM=350000,EC=200.

REDUCE(-)

RE364BX, ,*PL=5OOOO.

/EOR

= LOFT L2-5 POST TEST ANALYSIS

* LZ-5 INITIAL CONDITIONS

POWER = 36.0 MW

* PCS FLOW = 192.4 KG/S

* TCOLD = 556.6 K

* PCS PRESSURE = 14.94 MPA

* PZR LEVEL = 1.14 M (45 IN)

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

0000100 NEW STDY-ST

0000101 RUN

0000105 5.0 10.0

* TIME STEP CONTROL CARDS * REQUIRED

* END TIME MIN DT MAX DT OPTN MNR MJR RST

0000201 900.0 1.0-6 1.0 14003 1 100 450

* 'IMINOR EDIT VARIABLES

* STEADY STATE PLOT REQUESTS

0000301 P 250010000

0000302 P 530010000

0000303 TEMPF 250010000

0000304 TEMPF 185010000

0000305 TEMPF 515010000

0000306 iFLOWJ 540000000

0000307 MFLOWJ 985000000

0000308 MFLOWJ 995000000

0000309 CNTRLVAR 1

0000310 CNTRLVAR 2

0000311 MFLOWJ 566000000

0000312 CNTRLVAR 910

0000313 MFLOWJ 100010000

0000314 P 420010000

0000315 VOIDG 500010000

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

* CLADDING TEMPERATURES

0000321 HTfTEMP 001100210 *

0000322 HTTEMP 001100310 •

0000323 HITEMP 002100210 *

0000324 HI'TEMP 002100310 *

0000325 HTTEMP 0O2100410 *

- 90 -
* ,1 . .... 1 - ,1 -.-- 1I ---- ---- -1 I 

* FUEL CENTERLINE TEMPERATURES

• -.... 1 - 01 00201"1 -1 -. .

0000326 HTTEMP 002100201 * 0000327 HITiEM~P 002100301 *

0000328 HTTEMP 002100401 ,

* TRIPS

• 501-509 GENERAL TRIPS

* ALWAYS TRUE

0000501 TIME 0 GE NULL 0 -1.0 L

• ALWAYS FALSE ,

0000502 TIME 0 LT NULL 0 -1.0 N

• PRESSURIZER LOW LEVEL ALARM

0000503 CNTRLVAR 002 LE NULL 0 0.3810 L

* BUDGET SAVER CONTROLS

• FOR EVERY 100 CPU SECONDS THE TRANSIENT MUST ADVANCE

• AT LEAST 1.00 SECONDS OR THE PROBLEM WILL TERMINATE

* THIS PROVIDES A RATIO OF 100:1 CPU:TRANSIENT -

0000507 TIME 0 GE CNTRLVAR 705 1.0 N

0000508 CPUTIME 0 GE CNTRLVAR 703 100. N

0000509 CPUTIME 0 GE NULL 0 100. L

0000600 602

0000601 -507 AND 508 N

0000602 601 AND 509 N

20570100 TU-VT508 TRIPUNIT 1.0 0.0 0

20570101 508

20570200 NXT-CPU MULT 1.0 0.0 0

20570201 CPUTIME 0

20570202 CNTRLVAR 701

20570300 OLD-CPU STDFNCTN 1.0 0.0 0

20570301 MAX CNTRLVAR 702 CNTRLVAR 703

20570400 NXT-TRAN MULT 1.0 0.0 0

20570401 TIME 0

20570402 CNTRLVAR 701

20570500 OLD-TRAN STDFNCTN 1.0 0.0 0

20570501 MAX CNTRLVAR 704 CNTRLVAR 705

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

* 510-519 TEST SPECIFIC TRIPS

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

0000510 P 100010000 LT NULL 0 14.19+6 L

* BREAK OPENS

0000511 TIME 0 GE NULL 0 0.00 L

* PCP TRIP

0000512 TIME 0 GE NULL 0 0.94 L

* HPIS ON

0000513 TIME 0 GE NULL 0 23.90 L

* LPIS ON

0000514 TIME 0 GE NULL 0 37.32 L

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

- 91 -
* LT 555 REFLOOD TRIP

0000555 P 230120000 LE NULL 0 1.0+6 L

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

* LT 677 COLD LEG BREAK VALVE CARD 3470301

0000677 511 OR 511 L

* ----.---- I----1 ---- 1--- --- 1 ---- * LT 679 HOT LEG BREAK VALVE CARD 3170301

0000679 511 OR 511 L

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

* LT 681 ECC CHECK VALVE CARD 6000301

0000577 NFLOWJ 600000000 GE NULL 0 0.0 N

0000578 P 605010000 GT P 185010000 0. N

0000681 577 AND 578 N

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

* LT 682 ACCUMULATOR VALVE CARD 6100301

0000579 TIME

0000682 579

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

* LT 683 HPIS J

0000683 513

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

* LT 684 LPIS J

0000684 514

* LT 685-686 ST]

* OPEN TRIP

0000589 P

0000590 p

0000670 685

0000671 -590

0000685 671

* CLOSE TRIP

0000591 P

0000592 P

0000672 686

0000673 -591

0000674 -685

0000686 673

* JOB TERMINATION

* OPEN

0000687 685

* CLOSE

0000688 686

0 GE

AND 579 --- 1----1--

UNCTION

OR 513 --- ------ 1 ---- UNCTION

OR 514 --- 1 ------ 1 ----

NULL 0 1.0+9 L

L

CARD 6400200

L

;ARD 6350200

L

BAN VALVE (

CARD 5400301

530010000

530010000

OR

AND

AND

530010000

530010000

OR

AND

AND

AND

VALVE TRIPS

OR

GT

LT

589

-686

670

GT

LT

592

672

699

674

NULL

NULL

N

N

N

NULL

NULL

N

N

N

N

0

0

7.1125+6 N

6.9747+6 N

0

0

6.5613+6 N

6.4924+6 N

602

OR 602

* ----.---- 1 .----- 1 ---- ---- * LT 689 FEED TRIP

0000689 510 OR 510

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

N

N

CARD 5660200

L

* LT 695 PCP I TRIP

0000695 512 OR

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

* LT 696 PCP 1 VELOCITY

0000696 502 AND

* ----.---- -------- 1 ---- * LT 697 PCP 2 TRIP

0000697 512 OR

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

* LT 698 PCP 2 VELOCITY

0000698 502 AND

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

CARD 1350301

512 N

TABLE CARD 1356100

502 N

CARD 1650301

512 N

TABLE CARD 1656100

502 N ---- 1 ----

- 92 -
* LT 699 SCRAM CARD 20269900 OR 20290000

0000699 510 OR 510 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 .---.--- 1 ---- * PRESSURIZER CONNECTION TEE REACTOR VESSEL SIDE

1050000 "PZR T RVS " BRANCH

1050001 1 0

1050101 0.0634444 1.0531192 0.0 70.0 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 ----- --- --- 1 ----.... 1 --- 7

* 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

* -----------1 ----- I ----1 ------ 1 ------ 1 ---------- * PRESSURIZER CONNECTION TEE STEAM GENERATOR SIDE

1100000 "PZR T SGS " BRANCH

1100001 1 0

1100101 0.0606063 0.9207292 0.0 0.0 0.0 0.0

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----

* HOT LEG PIPING

1120000 "HOT LEG PP" PIPE

1120001 2

1120101 0.0 2

1120201 0.0 1

1120301 1.38893 1

1120302 0.707687 2

1120401 0.0796973 1

1120402 0.0579614 2

- 93 -
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 15002900. 1410030. 2459870. .00000000 0.0

1121202 0 15005500. 1410030. 2459770. .00000000 0.0

1121300 0

1121301 5.1146000 5.1146000 0.0 01

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

* SG INLET PLENUM

1140000 "SG IN PLNM" BRANCH

01

02

1140001

1140101

1140102

1140200

1141101

1142101

1141201

1142201

2

0.0

4.E-5

0

112010000

114010000

3.5832000

1.9414000

0

0.629795

0.0102

14987200.

114000000

115000000

3.5832000

1.9414000

0.33532

00

1410020.

0.0512

0.0

0.0

0.0

0.0

2460000.

0.0

0.0

90.0

.00000000

0.0

0.0

0.512756

0100

0100

* ----.---- -------- 1 ---- * SG U-TUBES

1150000 "SG TUBES " 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

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 0.0102

1150901 0.0 0.0

1151001 00 8

1151101 0000 7

1151201 0 14979(

1151202 0 14972E

1151203 0 149673

1151204 0 149620

PIPE

2 8

7

00.

300.

300.

)00.

1367230.

1333400.

1306120.

1288520.

2460010.0

2460020.0

2460030.0

2460040.0

.00000000

.00000000

.00000000

.00000000

0.0

0.0

0.0

0.0

01

02

03

04

- 94 -
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

1151302 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

* SG OUTLET PLENUM

1160000 "SG OUT PLN" BRANCH

50.0 .00000000 0.0

'40.0 .00000000 0.0

30.0 .00000000 0.0

)20.0 .00000000 0.0

-90.0 -0.512756

05

06

07

08

1160001 2 0

1160101 0.0 0.629795 0.335:

1160102 4.E-5 0.0102 00

1160200 0 14976400. 12338:

1161101 115010000 116000000 0.0

1162101 116010000 118000000 0.051

1161201 1.7656000 1.7656000 0.0

1162201 3.2740000 3.2740000 0.0

* ---- ------------ 1 ------ 1 ---- * PUMP SUCTION PIPING

1180000 "PMP SUC PP' t 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

1180703 -0.355604 3

32 0.0

10.

2

2460100.

0.0

0.0

.00000000

0.0

0.0

0100

0100

----1------

1180801

1180901

1180902

1181001

1181101

1181201

1181202

1181203

4. E-5

0.083

0.104

00

0000

0

0

0

0.0

0.083

0.104

3

2

14965800.

14967700.

14970500.

3

1

2

1233810.

1233810.

1233810.

2460030.0

2460033.0

2460035.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

01

02

03

1181300 0

1181301 4.1288000 4.1288000 0.0 01

1181302 4.2081000 4.2081000 0.0 02

* -------- 1 ------ 1 ------ 1------ 1 -------- ---- 1 ---- * PUMP SUCTION TEE

1200000 "PMP SCT T " BRANCH

1200001 3 0

1200101 0.0 0.759614 0.0487901 0.0 0.0 0.0

- 95 -
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 ---- * PUMPI SUCTION TEE OUTLET

1250000 "PMPl SCT T" 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 ---- * PUMP 1 INLET

1300000 "PMP1 INLET" SNGLVOL

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 ---- * PRIMARY COOLANT PUMP 1

1350000 "PCPUMP " PUMP

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. 1233820. 2459500. .00000000

1350201 0 3.2631000 3.2631000 0.0

1350202 0 3.4591000 3.4591000 0.0

1350301 0 0 0 -1 -1 695 0

1350302 369.00000 .36043360 .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----

* PUMP 1 OUTLET PUMP SIDE

1400000 "PMP1 OUT P" SNGLVOL

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

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

* PUMPI OUTLET PIPE TEE SIDE

1450000 "PMP1 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

- 96 -
* ----. -.-- 1 ----. .... 1 ----. .... 1 ----. .... 1 . .... --- I .... ....- 1 ---- * PUMP OUTLET TEE

1500000 "PMP 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----

* PUMP 2 SUCTION TEE OUTLET

1550000 "PMP2 SCT 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

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

* PUMP 2 INLET PIPE

1600000 "PNP2 INLET" SNGLVOL

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----

* 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 -1 697 0

1650302 369.00000 .37883469 .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----

* PUMP 2 OUTLET

1700000 "PIP2 OUT T" BRANCH

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 ------ ---- * INTACT LOOP COLD LEG PIPE

1750000 "ILCL PIPE " PIPE

1750001 2

1750101 0.0 2

1750201 0.0 1

- 97 -
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

1751202 0 15042800. 1233820. 2459500.0 .00000000 0.0

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---- , 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. 1233830. 2459550. .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

* REACTOR VESSEL

* INLET ANNULUS UPPER VOLUME INTACT SIDE

7000000 "INANUPRINT" ANNULUS

7000001 1

7000101 0.1308530 1

7000301 0.1876129 1

7000401 0.0 1

7000501 0.0 1

7000601 90.0 1

7000801 3.81-6 0.172 1

7001001 00 1

7001201 0 15028400. 1233830. 2459250. .00000000 0.0

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

* JUNCTION - UPPER TO LOWER INLET ANNULUS INTACT SIDE

7010000 "INANNUINT" SNGLJUN

7010101 730000000 700000000 0.129467 0.0000 0.0000 0100

01

02

01

- 98 -
7010201 0 .34062000 .34062000 0.0 * ----. -.-- 1 ---- --- .. I .... ....- 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. 1233830. 2459250. 0.0 0.0 01

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

* JUNCTION - MIDDLE TO LOWER INLET ANNULUS INTACT SIDE

7310000 "INANMLINT " SNGLJUN

7310101 730010000 702000000 0.0709408 0.0 0.0 0100

7310201 0 1.5959 1.5959 0.0

* 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 15030600. 1233830. 2459300. .00000000 0.0 01

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

* 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----

* DOWNCOIER UPPER VOLUME INTACT SIDE

7040000 "DNCRUPRINT" ANNULUS

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

7041001 00 1

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

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

* JUNCTION - UPPER TO MIDDLE DOWNCOMER INTACT SIDE

7050000 "UPR2MIDINT" 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----

- 99 -
* DOWNCOMER MIDDLE VOLUME INTACT SIDE

7060000 "DNCRMIDINT" ANNULUS

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 ---- * JUNCTION - MIDDLE TO LOWER DOWNCOMER INTACT SIDE

7070000 "MID2LWRINT" SNGLJUN

7070101 706010000 708000000 0.0709408 0.0000 0.0000 0100

7070201 0 1.4821000 1.4821000 0.0

* -------- 1 ------ 1 -------- ---- ------ 1 ---------- * DOWNCOMER LOWER VOLUME INTACT SIDE

7080000 "DNCRLWRINT" ANNULUS

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----

* JUNCTION - LOWER DOWNCOMER 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---- 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 ---- * JUNCTION - MIDDLE TO UPPER INLET ANNULUS BROKEN SIDE

7110000 "INANUBEN " SNGLJUN

7110101 740000000 710000000 0.129467 0.0000 0.0000 0100

7110201 0 -. 2873200 -. 2873200 0.0

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

* INLET ANNULUS MIDDLE VOLUME BROKEN SIDE

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

- 100 -
7400000 "INANMIDBKN" ANNULUS

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

* JUNCTION - MIDDLE TO LOWER INLET ANNULUS BROKEN SIDE

7410000 "INANMLBKN " SNGLJUN

7410101 740010000 712000000 0.0709408 0.0 0.0 0100

7410201 0 .86411 .86411 0.0

* ----.------- 1 ---- 1 ---- ---- ----- ------ 1 ---- * INLET ANNULUS LOWER VOLUME BROKEN SIDE

7120000 "INANLWRBKN' ANNULUS

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 ---------- * JUNCTION - INLET ANNULUS TO DOWNCOMER BROKEN SIDE

7130000 "INAN2DCBKN" SNGLJUN

7130101 712010000 714000000 0.0709408 0.0000 0.0000 0100

7130201 0 .86411000 .86411000 0.0

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

* DOWNCOMER UPPER VOLUME BROKEN SIDE

7140000 "DNCRUPRBKN" 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 - .---- I-1--- ---- 1 ------ 1 ------ 1 ------ 1----

* JUNCTION - UPPER TO MIDDLE DOWNCOMER BROKEN SIDE

7150000 "UPR2MIDBKN" SNGLJUN

7150101 714010000 716000000 0.0709408 0.0000 0.0000 0100

7150201 0 1.1432000 1.1432000 0.0

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

* DOWNCOMER MIDDLE VOLUME BROKEN SIDE

7160000 "DNCRMIDBKN" ANNULUS

7160001 1

- 101 -
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----

* JUNCTION - MIDDLE TO LOWER DOWNCOIER BROKEN SIDE

7170000 "MID2LWRBKN" SNGLJUN

7170101 716010000 718000000 0.0709408 0.0000 0.0000 0100

7170201 0 1.3175000 1.3175000 0.0

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

* DOWNCOMER LOWER VOLUME BROKEN SIDE

7180000 "DNCRLWRBN' t ANNULUS

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----

* JUNCTION - LOWER DOWNCOMER 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----

* CROSSFLOW JUNCTION - UPPER INLET ANNULUS

7200000 "UPRINANNXF" SNGLJUN

7200101 700000000 710000000 0.0296780 1.8341 1.8341 0003

7200201 0 .28732000 .28732000 0.0

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

* CROSSFLOW JUNCTION - LOWER INLET ANNULUS

7220000 "LWRINANNXF" SNGLJUN

7220101 702000000 712000000 0.0428706 1.8079 1.8079 0003

7220201 0 .38395000 .38395000 0.0

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

* CROSSFLOW JUNCTION - UPPER DOWNCOMER

7240000 "UPRDNCMRXF" SNGLJUN

7240101 704000000 714000000 0.03 1.33165-2 1.33165-2 0003

7240201 0 .19557000 .19557000 0.0

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

* CROSSFLOW JUNCTION - MIDDLE DOWNCOMER

7260000 "MIDDNCMRXF" SNGLJUN

7260101 706000000 716000000 0.03 2.10929-2 2.10929-2 0003

7260201 0 .10572000 .10572000 0.0

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

* CROSSFLOW JUNCTION - LOWER DOWNCOMER

- 102 -
* . --.--.. 1 ----.... 1 - -1 - 1- 1 .---- 1---

7280000 "LWRDNCMRXF" SNGLJUN

7280101 708000000 718000000 0.03 3.05234-2 3.05234-2 0003

7280201 0 .07171910 .07171910 0.0

* -------- 1 ------ 1 ----1------ 1 ------ 1 ------ 1 ---- * LOWER PLENUM TOP VOLUME

2150000 "LWR PL TOP" BRANCH

2150001 2 0

2150101 0.0 0.3533183 0.2592277 0.0 -90.0 -0.3533183

2150102 3.81-6 0.0 00

2150200 0 15059400. 1233780. 2458550. .00000000

2151101 215010000 220000000 0.0 0.005 0.005 0000

2152101 215000000 225000000 0.1499 1.5 1.5 0000

2151201 .571898-5 .571894-5 0.0

2152201 1.7076000 1.7076000 0.0

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

* LOWER PLENUM BOTTOM VOLUME

2200000 "LWR PL BOT" SNGLVOL

2200101 0.0 0.3741720 0.29656 0.0 -90.0 -0.3741720

2200102 4.OE-5 0.0 00

2200200 0 15062100. 1233780. 2458500. .00000000

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

* LOWER CORE SUPPORT STRUCTURE

2250000 "% CORE SUP" BRANCH

2250001 2 0

2250101 0.2832456 0.5709989 0.0 0.0 90.0 0.5709989

2250102 3.81-6 0.095 00

2250200 0 15054400. 1233780. 2458550. .00000000

2251101 225010000 230000000 0.1134 1.5 1.5 0000

2252101 225010000 235000000 0.0 12. 12. 0000

2251201 2.1758000 2.1758000 0.0

2252201 .65905000 .65905000 0.0

* ---- ------------------- 1 ---- -- 1 ---- ------ 1 ---- * ACTIVE CORE

2300000 "CORE " PIPE

2300001 12

2300101 0.183262 2

2300102 0.171287 4

2300103 0.172986 6

2300104 0.171486 8

2300105 0.171455 10

2300106 0.177236 12

2300201 0.1705 3

2300202 0.144 4

2300203 0.1705 7

2300204 0.144 8

2300205 0.1705 11

2300301 0.1397017 12

2300401 0.0 12

2300501 0.0 12

2300601 90.0 12

2300801 1.27-7 0.012 12

2300901 0.0 0.0 3

2300902 0.66 0.66 4

2300903 0.0 0.0 7

- 103 -
2300904 0.66 0.66 8

2300905 0.0 0.0 11

2301001 00 12

2301101 0000 11

2301201 0 15048500. 1263450. 24595

2301202 0 15045400. 1309480. 24595

2301203 0 15042500. 1357660. 24595

2301204 0 15040100. 1394080. 24595

2301205 0 15037200. 1417170. 24595

2301206 0 15034300. 1424460. 24595

2301300 0

2301301 1.4679000 1.4679000 0.0 02

2301302 1.7789000 1.7789000 0.0 04

2301303 1.5425000 1.5425000 0.0 06

2301304 1.8668000 1.8668000 0.0 08

2301305 1.5994000 1.5994000 0.0 11

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

* 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

2350801 3.81-6 0.003 3

2350901 0.0 0.0 2

2351001 00 3

2351101 0000 2

2351201 0 15048000. 1233790. 24595

2351202 0 15042400. 1233790. 24595

2351203 0 15036500. 1233790. 24595

2351300 0

2351301 .71258000 .71258000 0.0 01

2351302 .73579000 .73579000 0.0 02

* ---------------- 1 ------ 1------ 1 ---- * UPPER END BOXES AND SUPPORT STRUCTURE

2400000 "UPR END BX" BRANCH

2400001 2 0

2400101 0.2423341 0.5867979 0.0 0.0

2400102 3.81-6 0.145 00

2400200 0 15028800. 1417550. 24596

2401101 230010000 240000000 0.1118 1.5

2402101 235010000 240000000 0.0 12.

2401201 2.4488000 2.4488000 0.0

2402201 .73579000 .73579000 0.0

p50.

50.

i50.

50.

50.

50.

.00000000

.00000000

.00000000

.00000000

.00000000

.00000000

0.0

0.0

0.0

0.0

0.0

0.0

02

04

05

06

10

12

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

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

50.0

'50.0

50.0

.00000000 0.0

.00000000 0.0

.00000000 0.0

01

02

03

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

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

00.

90.0

.00000

1.5

12.

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

* UPPER CORE SUPPORT STRUCTURE - CROSS FLOW REGION

2450000 "UPR CR SUP" BRANCH

2450001 2 0

2450101 0.0 0.4933248 0.1280806 0.0 90.0

2450102 3.81-6 0.145 00

2450200 0 15025400. 1417510. 2459600. .0000

2451101 240010000 245000000 0.0 0.0 0.0

2452101 245010000 251000000 0.0 0.0 0.0

0.5867979

1000

0000

0000

'1

0.4933248

)000

0000

0000

0

- 104 -
2451201 1.1669000 1.1669000 0.0

2452201 .439867-4 .439867-4 0.0

* ----.---- -------- 1 --.---- I--1--- ---- 1 ---- -- 1-- I----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 245010000 250000000 0.0 0.0 0.0 0000

2501201 1.8273000 1.8273000 0.0

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

* DEAD END OF FUEL MODULES

2510000 "DE FL MODS" SNGLVOL

2510101 0.0 0.7844123 0.1154214 0.0 90.0 0.7844123

2510102 3.81-6 0.214 00

2510200 0 15021500. 1424270. 2459600. .00000000

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

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 0003

2521201 -. 1334300 .1334300 0.0

2522201 .05329530 .05329530 0.0

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

* UPPER PLENUM BOITOM 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 ---- * UPPER PLENUM TOP VOLUME

2600000 "UPR PL TOP" SNGLVOL

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

- 105 -
3000101 0.0 0.876303 0.0575410 0.0 0.0 0.0

3000102 4.0E-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 ---- * 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 ------ 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------ 1 ---- ------ 1 ------ * STEAM GENERATOR AND PUMP SIMULATIOR

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

3150000 "SG+PMP 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

3150307 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

- 106 -
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

3151202 0 15005700. 1237630. 2459924

3151203 0 14996600. 1237670. 2459924

3151204 0 14996600. 1237680. 2459924

3151205 0 15005600. 1237680. 2459924

3151206 0 15018100. 1237680. 2459924

3151207 0 15025100. 1237680. 2459924

3151208 0 15022500. 1237680. 2459924

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

* HOT LEG BREAK VALVE

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

3170000 "UL BREAK " VALVE

3170101 315010000 800000000 8.3647-3 0.94883

3170102 0.93 0.84

3170201 0 .00000000 .00000000 0.0

3170300 TRPVLV

3170301 679

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

* REACTOR VESSEL NOZZLE - BROKEN LOOP COLD LEG

3350000 "RVN BLCL " BRANCH

3350001 2 0

3350101 0.0 0.749305 0.047979 0.0

3350102 4.OE-5 0.0 00

3350200 0 15028400. 1233660. 2459250.

3351101 740000000 335000000 0.064130 1.45559•

3352101 335010000 340000000 0.063426 0.1005

3351201 .06071680 .06071680 0.0

3352201 .06138070 .06138070 0.0

.00000000

.00000000

.00000000

.00000000

.00000000

.00000000

.00000000

.00000000

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

01

02

03

04

05

06

07

08

---10.9-----1-0

---1------

0•94883 0100

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

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

0.0 0.0

4 .00000000

0.812933

0.1005

0002

0000

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

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

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

0.0 0.0

- 107 -
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----

* BROKEN LOOP COLD LEG RABS TO DTr

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

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

* COLD LEG BREAK VALVE

3470000 "CL BREAK " VALVE

3470101 344010000 805000000 8.3647-3 0.415 0.415 0100

3470102 0.93 0.84

3470201 0 .00000000 .00000000 0.0

3470300 TRPVLV

3470301 677

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

* REFLOOD ASSIST BYPASS PIPING - COLD LEG SIDE

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

- 108 -
3701302 .10027000 .10027000 0.0 02 * ----. -.-- 1 ---- --- 1 ---- --- 1 ----. .... 1 ----. .... 1 ---- -- -I - -

* REFLOOD ASSIST BYPASS VALVES

3750000 "RABS VALVS" SNGLJUN

3750101 370010000 380000000 0.0 0.90+4 0.90+4 0000

3750201 0 .05011390 .05011390 0.0

* -------- ---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

3800902 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

* 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

* ----.---- 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

- 109 -
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. 24595(

4051202 0 15010100. 1444040. 24595(

4051300 0

4051301 -. 0608633 -. 0608633 0.0 01

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

* PRESSURIZER SURGE LINE

4100000 "SRG LINE " SNGLJUN

4100101 405010000 415000000 1.44561-3 0.42

4100201 0 -. 0608789 -. 0608789 0.0

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

* 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

4150801 4.OE-5 0.0 6

4151001 00 6

4151101 0000 5

4151201 0 15009100. 1586220. 24596(

4151202 0 15008000. 1586220. 24596(

4151203 0 15006300. 1586220. 24596(

4151204 0 15003800. 1586220. 24600(

4151205 0 15002300. 1586220. 24665(

4151206 0 15002000. 1586220. 24681(

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 -. 23263-4 0.0 05

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

* PRESSURIZER VESSEL TO TOP HAT

4170000 "VSSL-TPHAT" SNGLJUN

4170101 415010000 420000000 0.0 0.0

D0. .00000000 0.0

D0. .00000000 0.0

--1-----1.-

---- 1----1-.

01

02

1.00 1000

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

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

)0.

)0.

)0.

)0.

0.

0.

.00000000

.00000000

.00000000

.03846070

1.0000000

1.0000000

0.0

0.0

0.0

0.0

0.0

0.0

01

02

03

04

05

06

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

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

0.0 0000

- 110 -
4170201 0 -. 21090-4 -. 21090-4 0.0

* . --.--.. 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 4.E-5 0.346066 2

4201001 00 2

4201101 0000 1

4201201 0 15001900. 1509900. 2482590. 1.0000000 0.0

4201202 0 15001800. 1509900. 2484800. 1.0000000 0.0

4201300 0

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

* STEAM 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 4.E-5 0.2840 00

5000200 0 5828810.0 1145280. 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

01

02

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

* SEPARATOR BYPASS

5030000 "SEPBYPASS " BRANCH

5030001 2 0

5030101 0.0 0.4445 0.4384 0.0

5030102 4.E-5 0.3678 00

5030200 0 5827350.0 1150000. 25912

5031101 505000000 503000000 0.98627 0.0

5032101 503010000 520000000 0.98627 0.8

5031201 -1.265400 .17607000 0.0

5032201 -. 3871600 .07560020 0.0

* SEPARATOR OUTLET REGION

5050000 "LWR SEPAR " BRANCH

5050001 1 0

5050101 0.0 1.2131 1.4850 0.0

5050102 4.E-5 1.9048 00

5050200 0 5830080.0 1236530. 258001

5051101 505010000 508000000 0.0 0.0

5051201 .64364000 -2.022800 0.0

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

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

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

70.

90.0

.99988000

0.0

0.0

0.4445

0100

0100

-90.0 -1.2131

00. .02870570

0.0 0100

....- 1------1--

- 11i -
* FEED INLET VOLUME

5080000 "UPR DWNCMR" BRANCH

5080001 1 0

5080101 0.0 0.6096 0.22107 0.0 -90.0 -0.6096

5080102 4.E-5 0.163697 00

5080200 0 5835210.0 1145280. 2580000. .00000000

5081101 508010000 510000000 0.0 0.0 0.0 0100

5081201 .66587000 .66587000 0.0

* ----.---- 1 ----- ------ 1 ----.--- 1 ---- --- --- 1 ---- * STEAM GENERATOR DOWNCOMER

5100000 "DWNCMR " ANNULUS

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

* JUNCTION - DOWNCOMER TO BOILER

5130000 "DNCMR-BLR " SNGLJUN

5130101 510010000 515000000 0.0 17.5 17.5 0100

5130201 0 .66609000 .88146000 0.0

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

* STEAM GENERATOR BOILER

5150000 "BOILER " PIPE

5150001 5

5150101 0.2776 4

5150102 0.306294 5

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 1321180. 2580000. .08907110 0.0 03

- 112 -
5151204 0 5834160.0 1360130. 2580000. .11715000 0.0 04

5151205 0 5829740.0 1414230. 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

* --- ---- ----- ----.---- ---- ---- ----.------- * LOWER PORTION OF STEAM DOME

5200000 "LWR STM DM" 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. 2591540. .99979000

5201101 520010000 525000000 0.0 0.0 0.0 0000

5201201 -. 0806823 .41903000 0.0

* ---- ----.----.----- 1.----- I .---- ----- .1 ----.-- 1--- --- 1 ---- * UPPER PORTION OF STEAM DOME

5250000 "UPR STM 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 ---- * STEAM PIPE FROM GENERATOR TO CONTROL VALVE

5300000 "STEAM PIPE" SNGLVOL

5300101 0.04635 25.074 0.0 0.0 0.0 0.0

5300102 4.E-5 0.0 00

5300200 0 5819190.0 1148038. 2591620. 1.0000000

* -------- 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 0 13.593000 13.593000 0.0

5400300 IITRVLV

5400301 687 688 0.05 0.44405 540

20254000 NORMAREA

20254001 0.0 0.0

20254002 9.25-4 9.25-4

20254003 1.0 1.0

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

* 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 ---- * AIR COOLED CONDENSER

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

- 113 -
5420000 "CONDENSER " TMDPVOL

5420101 0.21677 17.67 0.0 0.0

5420102 4.E-5 0.02 00

5420200 2

5420207 0.0 2.069E6 1.0

*- 1------1------1---------- .... .... * SIMPLIFIED FEED SYSTEM

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

* FEED STORAGE TANK

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

5650000 "FEED TANK " TMDPVOL

5650101 29.81 3.048 0.0 0.0

5650102 4.E-5 0.0 00

5650200 3 502

5650201 0.0 2.15323E6 477.6

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

* FEED WATER

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

0.0 0.0

*ICO1

*ICO1

---- 1----1.-

---- 1--....-1.-

..-.-1--....-1.-

0.0 0.0

--1-- ...-1-....

--..-1------..1....

5660000 "FEED " TMDPJUN

5660101 565000000 508000000 0.05

5660200 1 689

5660201 -100.0 18.788 0.0 0.0 *L2-5

5660202 0.0 18.788 0.0 0.0 *L2-5

5660203 0.5 10.0 0.0 0.0 *L2-5

5660204 1.0 2.50 0.0 0.0 *L2-5

5660205 1.5 1.00 0.0 0.0 *L2-5

5660206 2.0 0.25 0.0 0.0 *L2-5

5660207 2.5 0.00 0.0 0.0 *LZ-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----

*ECCS HEADER TO PCS

6050000 "ECCS HEADR" SNGLVOL

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

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

* ACCUMULATOR VALVE

6100000 "ACCUM VLV " VALVE

6100101 615010000 605000000 5.9896-3 6.278 6.278 1000

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

6100300 TRPVLV

6100301 682

* -------- 1 ------ 1 ------ 1 -- 1 ---- 1-- ---- ---- * ACCUMULATOR PIPE

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

6150000 "ACC PIPE " SNGLVOL

- 114 -
6150101 0.0 25.997165 0.4074774 0.0 0.0 0.0

6150102 4.0-5 0.0 00

6150200 0 4.5E+6 11Z409. 2459920. .00000000

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

* ACCUMULATOR VESSEL

*6200000 "ACCUMULATR" ACCUM

*6200101 0.0 1.8103 2.3422 0.0 90.0 1.811

*6200102 4.0-5 0.0 01

*6200200 4.223+6 305.38

*6201101 615000000 8.2132-3 13.3 13.3 0

*6202200 0.0 1.0662 2.4509 1.6927 0.04445 0 0

03

O00

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

* BWST LPIS

6250000 "BWST LPIS " TMDPVOL

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

* - ---- --------- 1 ---- 1 ------ 1 ---- * LOW PRESSURE INJECTION SYSTEM

6300000 "LPIS TMDPJUN

6300101 625000000 605000000 5.9896-3

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

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

90.0 5.0

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

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

6300200 1 684 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----- 1 .--- 1 -------. 1 ---- * BWST HPIS

6350000 "BWST HPIS " TMDPVOL

6350101 20.44 5.0 0.0 0.0 90.0 5.0

6350102 4.OE-5 0.0 00

6350200 3

6350201 0.0 1.0+5 300.0

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

* HIGH PRESSURE INJECTION SYSTEM

6400000 "HPIS TMDPJUN

6400101 635000000 185000000 5.9896-3

6400200 1 683 P 185010000

6400201 -1.0 0.0 0.0 0.0

6400202 0.0 .75687272 0.0 0.0

6400203 7.72514+6 .75687272 0.0 0.0

6400204 8.3597+6 .31536281 0.0 0.0

6400205 17.2436+6 .31536281 0.0 0.0

- 115 -
* CONTAINMENT ,

* CONTAINMENT BROKEN LOOP HOT LEG

8000000 "CONT BLHL " TMDPVOL

8000101 0.0 1.0 0.1 0.0 0.0 0.0

8000102 0.0 0.0 00

8000200 2

8000201 0.0 1.0+5 1.0

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

* CONTAINMENT BROKEN LOOP COLD LEG

8050000 "CONT BLCL " TMDPVOL

8050101 0.0 1.0 0.1 0.0 0.0 0.0

8050102 0.0 0.0 00

8050200 2

8050201 0.0 1.0+5 1.0

* REACTOR VESSEL HEAT STRUCTURES

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

* ACTIVE CORE

* STATION 116.91 TO 182.94

* PERIPHERAL FUEL MODULES

10011000 12 10 2

10011001 7.869E+6

10011011 I.OE-6 2.OE-6 0.0

10011100 0 1

10011101 5 4.65564-3

10011102 1 4.75106-3

10011103 3 5.36806-3

10011201 1 5

10011202 -2 6

10011203 -3 9

10011301 1.0 5

10011302 0.0 9

10011401 560.0 10

10011501 0 0 0

10011601 230010000 10000 1

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

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

1

10011701 900

10011702 900

10011703 900

10011704 900

10011705 900

10011706 900

10011707 900

10011708 900

10011709 900

10011710 900

10011711 900

10011712 900

10011901 0

* -------- --------

* CENTER FUEL MODULE

0.0416629

0.0778047

0.0912202

0.0948738

0.0980981

0.0977318

0.0861681

0.0662856

0.0565472

0.0386339

0.0146376

0.0099343

0.013633

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.01504

0.0

1

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0 0.0

1.6764

0.0 555 1 8

12

153.113 12

153.113 12

1 * SGTR 36MW

2 * SGTR 36MW

3 * SGTR 36MW

4 * SGTR 36MW

5 * SGTR 36MW

6 * SGTR 36MW

7 * SGTR 36MW

8 * SGTR 36MW

9 * SGTR 36MW

10 * SGTR 36MW

11 * SGTR 36MW

12 * SGTR 36MW

12

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

- 116 -
* . --.--.. 1 ---- 1- ....---- 1 1"

10021000 12 10 2 1 0.0 555 1 8

10021001 7.869E+6

10021011 1.OE-6 2.0E-6 0.0 0.0 12

10021100 0 1

10021101 5 4.65564-3

10021102 1 4.75106-3

10021103 3 5.36806-3

10021201 1 5

10021202 -2 6

10021203 -3 9

10021301 1.0 5

10021302 0.0 9

10021401 560.0 10

10021501 0 0 0 1 28.4988 12

10021601 230010000 10000 1 1 28.4988 12

10021701 900 1.25-2 0.0 0.0 1 * SGTR 36MW

10021702 900 1.33435-2 0.0 0.0 2 * SGTR 36MW

10021703 900 2.7-2 0.0 0.0 3 * SGTR 36MW

10021704 900 2.80814-2 0.0 0.0 4 * SGTR 36MW

10021705 900 2.85-2 0.0 0.0 5 * SGTR 36MW

10021706 900 2.83936-2 0.0 0.0 6 * SGTR 36MW

10021707 900 2.44008-2 0.0 0.0 7 * SGTR 36MW

10021708 900 1.87704-2 0.0 0.0 8 * SGTR 36MW

10021709 900 1.58694-2 0.0 0.0 9 * SGTR 36MW

10021710 900 1.08422-2 0.0 0.0 10 * SGTR 36MW

10021711 900 0.51629-2 0.0 0.0 11 * SGTR 36MW

10021712 900 0.3504-2 0.0 0.0 12 * SGTR 36MW

10021901 0 0.013633 0.01504 1.6764 12

* STEAM GENERATOR HEAT STRUCTURES

* TUBING

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 ,

20100100 TBL/FCTN 1 1 * U02

20100200 TBL/FCTN 3 1 * GAP

- 117 -
20100300 TBL/FCTN 1 1 * ZR

20100400 TBL/FCTN 1 1 * S-S]

20100500 C-STEEL

20100600 TBL/FCTN 1 1 * INC(

* -- ------------- ---- --- --- 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

20100106 1.03315E3 3.357625

20100107 1.08871E3 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 2.289762

20100115 2.25537E3 2.307069

20100116 2.53315E3 2.433413

20100117 2.81093E3 2.661870

20100118 3.08871E3 2.994171

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

* U02 - VOLUMETRIC 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 1.77315E3 3.531030E6

20100157 1.97315E3 3.792588E6

20100158 2.17315E3 4.228518E6

20100159 2.37315E3 4.882412E6

20100160 2.67315E3 6.015829E6

20100161 2.77315E3 6.320980E6

20100162 2.87315E3 6.582538E6

20100163 2.97315E3 6.713317E6

20100164 3.11315E3 6.800503E6

20100165 4.69982E3 6.800503E6

* HELIUM(GAP) - THERMAL CONDUCTIVITY

20100201 HELIUM 1.00

• HELIUM(GAP) - VOLUMETRIC HEAT CAPACITY

20100251 273.15 5.4

20100252 5000.0 5.4

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

* ZIRCALOY-4 - THERMAL CONDUCTIVITY F

20100301 300.0 12.68

*20100301 380.4 13.6

20100302 469.3 14.6

20100303 577.6 15.8

IEEL

)NEL 600

ROM 1------1----

---- 1-- ....-1.-

---- 1------1--.

FROM IMATPRO

•--I-1-----1--

- 118 -
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

, 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

* S-STEEL - THERIMAL 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 4.773E6

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

- 119 -
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

* 001-006 LEVEL CALCULATORS

* 001 STEAM GENERATOR LEVEL

20500100 SGLVL SUM 1.0 0.0

20500101 0.0 0.4445 VOIDF 503010001

20500102 1.2131 VOIDF 50501000(

20500103 0.6096 VOIDF 50801000(

20500104 0.6096 VOIDF 510010001

20500105 0.6096 VOIDF 51002000(

20500106 0.6096 VOIDF 51003000(

* 002 PRESSURIZER LEVEL

20500200 PZRLVL SUM 1.0 0.0

20500201 0.0 0.1815 VOIDF 41501000(

20500202 0.1524 VOIDF 41502000(

20500203 0.3967 VOIDF 415030001

20500204 0.5289 VOIDF 415040001

20500205 0.3967 VOIDF 41505000(

20500206 0.1943 VOIDF 41506000(

20500207 0.1029 VOIDF 42001000(

20500208 0.1029 VOIDF 42002000(

* 003 REACTOR VESSEL LEVEL

20500300 RVLVL SUM 1.0 0.0

20500301 0.0 0.84888 VOIDF 26001000(

20500302 0.24333 VOIDF 25501000(

20500303 0.9285337 VOIDF 25001000(

20500304 0.4933248 VOIDF 24501000(

20500305 0.4933248 VOIDF 24001000(

20500306 0.4234231 VOIDF 23006000(

20500307 0.2794034 VOIDF 23005000(

20500308 0.2794034 VOIDF 23004000(

20500309 0.2794034 VOIDF 23003000(

20500310 0.2794034 VOIDF 23002000(

20500311 0.3728765 VOIDF 23001000(

20500312 0.4269792 VOIDF 22501000(

20500313 0.3533183 VOIDF 21501000(

20500314 0.3741720 VOIDF 22001000(

* 004 ACCUMULATOR LEVEL

*20500400 ACCMLVL INTEGRAL -6.3480-3 2.0447

*20500401 VELFJ 620010000

, 007 REACTOR VESSEL DOWNCOMER LEVEL INTACT SIDE

20500700 RVDCLVLIN SUM 1.0 0.0

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

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

0

0

0

0

0

0

0

0

0

0

0

0

0

0

0

0

0

)

0

)

)

)

)

)

1

1

1

0

1

- 120 -
20500701 0.0 0.3302040 VOIDF 700010000

20500702 0.3951272 VOIDF 702010000

20500703 1.5200561 VOIDF 704010000

20500704 1.2616333 VOIDF 706010000

20500705 1.0792591 VOIDF 708010000

20500706 0.3533183 VOIDF 215010000

20500707 0.3741720 VOIDF 220010000

* 008 REACTOR VESSEL DOWNCOMER LEVEL BROKEN SIDE

20500800 RVDCLVLBK SUM 1.0 0.0

20500801 0.0 0.3302040 VOIDF 710010000

20500802 0.3951272 VOIDF 712010000

20500803 1.5200561 VOIDF 714010000

20500804 1.2616333 VOIDF 716010000

20500805 1.0792591 VOIDF 718010000

20500806 0.3533183 VOIDF 215010000

20500807 0.3741720 VOIDF 220010000

* 061-072 PRIMARY SYSTEM MASS CALCULATOR

* 061 INTACT LOOP HOT LEG MASS

20506100 ILHLMASS SUM 1.0 0.0 1

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 SGPRIMASS SUM 1.0 0.0 1

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 PMPSUMASS SUM 1.0 0.0 1

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 1

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 175020000

20506409 7.30598-2 RHO 180010000

- 121 -
20506410 6.44920-2 RHO 185010000

* 065 DOWNCOMER/LOWER PLENUM MASS

20506500 DCLPMASS 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

20506505 0.0986806 RHO 708010000

20506506 0.0432082 RHO 710010000

20506507 0.0578606 RHO 712010000

20506508 0.1581866 RHO 714010000

20506509 0.1217000 RHO 716010000

20506510 0.0986806 RHO 718010000

20506511 0.24520 RHO 215010000

20506512 0.29656 RHO 220010000

* 067 CORE/UPPER PLENUM MASS

20506700 CRUPMASS SUM 1.0 0.0

20506701 0.0 0.12094 RHO 225010000

20506702 0.0683340 RHO 230010000

20506703 0.0478582 RHO 230020000

20506704 0.0483329 RHO 230030000

20506705 0.0479138 RHO 230040000

20506706 0.0479052 RHO 230050000

20506707 0.0750459 RHO 230060000

20506708 0.0091280 RHO 235010000

20506709 0.0072325 RHO 235020000

20506710 0.0088095 RHO 235030000

20506711 0.1195494 RHO 240010000

20506712 0.1280806 RHO 245010000

20506713 0.1436936 RHO 250010000

20506714 0.1154214 RHO 251010000

20506715 0.083595 RHO 255010000

20506716 0.310967 RHO 260010000

* 068 BROKEN LOOP HOT LEG MASS

20506800 BLHLMASS SUM 1.0 0.0

20506801 0.0 5.75410-2 RHO 300010000

20506802 4.42927-2 RHO 305010000

20506803 6.78467-2 RHO 310010000

20506804 7.75291-3 RHO 315010000

20506805 1.72111-1 RHO 315020000

20506806 8.97552-2 RHO 315030000

20506807 8.97552-2 RHO 315040000

20506808 1.72111-1 RHO 315050000

20506809 1.82303-2 RHO 315060000

20506810 5.46687-2 RHO 315070000

20506811 1.82489-2 RHO 315080000

20506812 9.15000-2 RHO 380010000

20506813 4.80000-2 RHO 380020000

20506814 4.89000-2 RHO 380030000

* 069 BROKEN LOOP COLD LEG MASS

20506900 BLCLMASS SUM 1.0 0.0

20506901 .0.0 4.79790-2 RHO 335010000

20506902 4.43927-2 RHO 340010000

20506903 3.62484-2 RHO 342010000

20506904 3.10679-2 RHO 344010000

20506907 2.79000-2 RHO 370010000

20506908 7.00000-2 RHO 370020000

20506909 1.16500-1 RHO 370030000

* 070 PRESSURIZER MASS

- 122 -
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

20507012 2.12609-3 RHO 430010000

* 071 REACTOR VESSEL TOTAL MASS

20507100 RVMASS SUM 1.0 0.0 1

20507101 0.0 1.0 CNTRLVAR 65

20507103 1.0 CNTRIVAR 67

* 072 PCS 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 CNTRIVAR 64

20507205 1.0 CNTRLVAR 68

20507206 1.0 CNTRLVAR 69

20507207 1.0 CNTRLVAR 70

20507208 1.0 CNTRLVAR 71

* GENERAL TABLE DATA

*

*

*

TABLE

NUMBER DESCRIPTION *

*

* 900 REACTOR POWER VS TIME AFTER SCRAM

20290000 POWER

20290001 0.0

20290002 0.1

20290003 0.2

20290004 0.3

20290005 0.4

20290006 0.5

20290007 0.6

20290008 0.8

20290009 1.0

20290010 1.5

20290011 2.0

20290012 3.0

20290013 4.0

20290014 6.0

20290015 8.0

20290016 10.0

20290017 15.0

20290018 20.0

699 1.0 36.0+6

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

0.047947

0.044575

0.042176

- 123 -
20290019 30.0 0.038783

20290020 40.0 0.036348

20290021 60.0 0.031546

20290022 1.+5 0.001460 * FROM LTR LO-08-81-173

* PUMP DATA

* SINGLE PHASE HEAD CURVES ....-1--..... -. --

* ------------ ---- I----

* HEAD CURVE NO. 1

1351100 1

1351101 0.000000E+00

1351102 1.906100E-01

1351103 3.896300E-01

1351104 5.939600E-01

1351105 7.902000E-01

1351106 1.OOOOOOE+00

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

* HEAD CURVE NO. 2

1351200 1

1351201 0.OOOOOOE+00

1351202 2.000000E-01

1351203 4.OOOOOOE-01

1351204 5.755400E-01

1351205 7.443200E-01

1351206 7.734800E-01

1351207 8.631300E-01

1351208 1.000000E+00

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

* HEAD CURVE NO. 3

1351300 1

1351301 -1.000000E+00

1351302 -8.057400E-01

1351303 -6.069000E-01

1351304 -4.068300E-01

1351305 -2.001710E-01

1351306 O.OOOOOOE+O0

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

* HEAD CURVE NO. 4

1351400 1

1351401 -1.000000E+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 0.000000E+00

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

* HEAD CURVE NO. 5

1351500 1

1351501 0.OOOOOOE+00

.... 1------..1----1------1-,-

1.403600E+00

1.363600E+00

1.318600E+00

1.232800E+00

1.133600E+00

1.000000E+00

2

-6.700000E-01

-5.OOOOOOE-01

-2.500000E-01

O.OOOOOOE+00

2.583000E-01

3.778000E-01

6.326000E-01

1.000000E+00

3

2.472200E+00

2.047400E+00

1.831000E+00

1.624000E+00

1.470500E+00

1.403600E+00

4

2.472200E+00

1.996800E+00

1.589700E+00

1.327900E+00

1.194900E+00

1.060500E+00

1.015600E+00

9.342790E-01 -..-- 1----1.-

5

2.500000E-01

... 1. -- 1--

----1-----1--,

....- 1------1-.--

....-1-- ....-1.-

•--1-- ....-1--

....- 1----1--.

....-1-----1"-

--1------1-....

--1----1--
1351502 2.000000E-01

1351503 4.OOOOOOE-01

1351504 4.118000E-01

1351505 5.976300E-01

1351506 7.934670E-01

1351507 1.000000E+00

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

* HEAD CURVE NO. 6

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

1351600 1

1351601 O.O00000E+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.OOOOOOE+00

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

* HEAD CURVE NO. 7

1351700 1

1351701 -1.OOOOOOE+O0

1351702 -8.OOOOOOE-01

1351703 -6.OOOOOOE-01

1351704 -4.OOOOOOE-O1

1351705 -2.OOOOOOE-01

1351706 O.OOOOOOE+O0

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

* HEAD CURVE NO. 8

1351800 1

1351801 -1.000000E+00

1351802 -8.OOOOOOE-01

1351803 -6.OOOOOOE-01

1351804 -4.OOOOOOE-01

1351805 -2.OOOOOOE-01

1351806 0.OOOOOOE+00

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

2.800000E-01

3.400000E-01

2.768000E-01

4.584000E-01

6.992000E-01

1.OOOOOE+O0

6

9.342790E-01

9.229000E-01

8.963000E-01

8.750000E-01

8.433000E-01

8.355000E-01

8.466000E-01

8.469000E-01

8.838000E-01

1.OOOOOOE+00

7

-1.OOOOOOE+O0

-6.300000E-01

-3.OOOOOOE-01

-5.OOOOOOE-02

1.5000OOE-01

2.5000OOE-01

8

-1.OOOOOOE+0O

-9.700000E-01

-9.5000OOE-01

-8.800000E-01

-8.OOOOOOE-01

-6.700000E-01

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

....-1------..1--

...--1------1-.--

-1----..-1-...-

....- 1------1.---

--1--- ...-1---

•1 1....-1

....- 1-- ....- 1--

* SINGLE PHASE TORQUE DATA

* TORQUE CURVE NO. 1

1351900 2 1

1351901 O.OOOOOOE+O0 6.032000E-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-01 9.229000E-01

1351906 1.OOOOOOE+O0 l.OOOOOOE+00

* -------- 1 ------ 1 ------ 1 ---------- * TORQUE CURVE NO. 2

1352000 2 2

1352001 O.OOOOOOE+00 -6.700000E-01

1352002 4.OOOOOOE-01 -2.500000E-01

1352003 5.OOOOOOE-01 1.500000E-01

- 125 -
1352004 7.372550E-01

1352005 7.680490E-01

1352006 8.672300E-01

1352007 1.000000E+00

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

* TORQUE CURVE NO. 3

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

1352100 2

1352101 -1.OOOOOOOE+0

1352102 -8.009600E-01

1352103 -6.063800E-01

1352104 -4.068600E-01

1352105 -1.992800E-01

1352106 0.OOOOOOE+00

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

* TORQUE CURVE NO. 4

1352200 2

1352201 -1.000000E+00

1352202 -8.223400E-01

1352203 -6.337100E-01

1352204 -4.585300E-01

1352205 -2.670230E-01

1352206 -1.761070E-01

1352207 -8.931000E-02

1352208 O.OOOOOOE+00

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

1352300 2

1352301 O.O00000E+00

1352302 4.OOOOOOE-01

1352303 5.OOOOOOE-01

1352304 1.000000E+O0

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

* TORQUE CURVE NO. 6

1352400 2

1352401 O.OOOOOOE+00

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

1352410 1.OOOOOOE+00

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

* TORQUE CURVE NO. 7

1352500 2

1352501 -1.000000E+0O

1352502 -3.OOOOOOE-01

1352503 -1.O00000E-01

1352504 O.O0O000E+O0

* ----.---- 1 ----.-- 1--- * TORQUE CURVE NO. 8

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

5.265860E-01

6.065940E-01

7.436600E-01

1.OOOOOOE0O

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

1.436200E+00

1.387900E+00

1.348100E+O0

1.233610E+00

5

-4.500000E-01

-2.500000E-01

O.OOOOOOE+O0

3.569000E-01 ---- 1------1--

--1------1-....

6

1.233610E+00

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-01 ---- 1----1--

7

-1.000000E+O0

-9.OOOOOOE-01

-5.000000E-O1

-4.500000E-01

--------- 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....

- 126 -
1352600 2 8

1352601 -1.OOOOOOE+0O -1.000000E+00

1352602 -2.500000E-01 -9.000000E-01

1352603 -8.000000E-02 -8.000000E-01

1352604 O.O00000E+00 -6.700000E-01

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

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

* HEAD CURVE

1353000 0

1353001 O.OOOOOOE+00

1353002 1.OOOOOOE-01

1353003 2.OOOOOE-01

1353004 3.OOOOOOE-01

1353005 3.500000E-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 1.000000E+00

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

* TORQUE CURVE *-----------1------1---

1353100 0

1353101 O.OOOOOOE+00

1353102 1.OOOOOOE-01

1353103 2.OOOOOOE-01

1353104 3.OOOOOOE-01

1353105 3.500000E-01

1353106 4.OOOOOOE-01

1353107 5.OOOOOOE-01

1353108 6.OOOOOOE-01

1353109 7.0000O0E-01

1353110 8.OOOOOOE-01

1353111 9.OOOOOOE-01

1353112 1.000000E+00

* PUMP 2-PHASE DIFFERENCE

* HEAD CURVE NO. 1

1354100 1

1354101 O.OOOOOOE+00

1354102 1.000000E+00

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

* HEAD CURVE NO. 2

1354200 1

1354201 O.OOOOO0E+00

1354202 1.OOOOOOE+0O

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

* HEAD CURVE NO. 3

1354300 1

1354301 -1.OOOOOOE+O0

1354302 -9.OOOOOOE-01

.---1------1------1------1.-.-

----1-----1--- ...-1--....... -

O.OOOOOOE+00

0.OOOOOOE+00

1.O0000E-O1

2.OOOOOOE-01

3.OOOOOOE-01

6.OOOOOOE-01

6.OOOOOOE-01

6.OOOOOOE-01

6.OOOOOOE-01

5.OOOOOOE-01

3.OOOOOOE-01

O.OOOOOOE+00 ---- 1----1--

O.OOOOOOE+O0

0.OOOOOOE+00

1.00000E-OI

3.OOOOOOE-01

5.OOOOOOE-01

7.500000E-01

7.500000E-01

7.500000E-01

7.500000E-01

7.500000E-01

5.OOOOOOE-01

O.OOOOOOE+00

DATA ....-1------1--

---1-----..-

--1--- ...-1-.-

---1------1-....

.--.1----1I-----1----1---

1

1.OOOOOOE+O0

1.0OOOOOE+O0

2

1.OOOOOOE+00

1.OOOOOOE+00

3

-1.160000E+0O

-1.240000E+00

-- 1--- ...-1---

....-1------..1-.

---- 1------..1....

- 127 -
1354303 -8.000000E-01

1354304 -7.OOOOOOE-01

1354305 -6.000000E-01

1354306 -5.000000E-01

1354307 -4.000000E-01

1354308 -2.500000E-01

1354309 -1.000000E-01

1354310 O.O00000E+00

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

* HEAD CURVE NO. 4

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

1354400 1

1354401 -1.OOOOOOE+O0

1354402 -9.OOOOOOE-01

1354403 -8.000000E-01

1354404 -7.OOOOOOE-01

1354405 -6.OOOOOOE-01

1354406 -5.OOOOOOE-01

1354407 -3.500000E-01

1354408 -2.OOOOOOE-01

1354409 -1.OOOOOOE-01

1354410 O.OOOOOOE+00

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

1354500 1

1354501 O.OOOOOOE+00

1354502 2.OOOOOOE-01

1354503 4.OOOOOOE-01

1354504 6.OOOOOE-01

1354505 8.OOOOOOE-01

1354506 1.OOOOOOE+0O

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

* HEAD CURVE NO. 6

1354600 1

1354601 O.OOOOOOE+00

1354602 1.OOOOOOE-01

1354603 2.500000E-01

1354604 4.OOOOOOE-O1

1354605 5.OOOOOOE-01

1354606 6.OOOOOOE-01

1354607 7.OOOOOOE-01

1354608 8.OOOOOOE-01

1354609 9.OOOOOOE-01

1354610 1.OOOOOOE+O0

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

* HEAD CURVE NO. 7

1354700 1

1354701 -1.000000E+00

1354702 O.OOOOOOE+00

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

* HEAD CURVE NO. 8

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

1354800 1

1354801 -1.OOOOOOE+00

1354802 O.OOOOOOE+00

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

-1.770000E+00

-2.360000E+00

-2.790000E+00

-2.910000E+00

-2.670000E+00

-1.690000E+00

ý-5.000000E-O1

O.OOOOOOE+0

4

-1.160000E+O0

-7.800000E-01

-5.OOOOOOE-01

-3. I00000E-01

-1.700000E-01

-8.OOOOOOE-02

O.OOOOOOE+00

5.OOOOOOE-02

8.OOOOOOE-02

1.100000E-O1

5

O.OOOOOOE+00

-3.400000E-01

-6.500000E-01

-9.300000E-01

-1.190000E+00

-1.470000E+00

6

1.100000E-01

1.300000E-01

1.50OOOOE-01

1.300000E-01

7.000000E-02

-4.OOOOOOE-02

-2.300000E-01

-5.100000E-01

-9.100000E-01

-1.470000E+00

7

O.OOOOOOE+00

O.OOOOOOE+00

----1------.1----

8

O.OOOOOOE+00

O.OOOOOOE+00

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

...- ...---1-- -

•--1--------

....-1------1--.

....-1----1--

- 128 -
* TORQUE CURVE NO. 1

1354900 2

1354901 O.OOOOOOE+O0

1354906 1.OOOOOOE+O0

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

* TORQUE CURVE NO. 2

1355000 2

1355001 O.OOOO0E+O0

1355007 1.OOOOOOE+O0

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

* TORQUE CURVE NO. 3

1355100 2

1355101 -1.OOOOO0E+O0

1355102 -8.009600E-01

1355103 -6.063800E-01

1355104 -4.068600E-01

1355105 -1.992800E-01

1355106 O.OOOOOOE+O0

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

* TORQUE CURVE NO. 4

1355200 2

1355201 -1.OOOOOOE+OO

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

*-----------1------1--"

1355300 2

1355301 O.OOOOOOE+O0

1355302 4.OOOOOOE-01

1355303 5.OOOOOOE-01

1355304 1.OOOOOOE+00

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

* TORQUE CURVE NO. 6

1355400 2

1355401 O.OOOOOOE+00

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+00

* ---------------- 1 ---- * TORQUE CURVE NO. 7

1355500 2

1

1.OOOO0OE+O0

1.OOOOOOE+OO

2

1.OOOOOOE+O

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

1.436200E+00

1.387900E+00

1.348100E+00

1.233610E+00

5

-4.500000E-01

-2.500000E-01

O.OOOOOOE+O0

3.569000E-01

6

1.233610E+00

1.196500E+00

1.109600E+00

1.041600E+O0

8.958000E-01

7.807000E-01

6.134000E-01

5.849000E-01

4.877000E-01

3.569000E-01

....-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....

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

- 129 -
1355501

1355502

1355503

1355504

-1.000000E+00

-3.000000E-01

-1.000000E-01

O.O00000E+00

-1.O00000E+O0

-9.OOOOOOE-01

-5.OOOOOOE-01

-4.5000OOE-01

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

* TORQUE CURVE NO. 8 *----------1-----1-- ---1-------1-----

1355600 2 8

1355601 -1.OOOOOOE+O0 -1.OOOOOOE+O0

1355602 -2.500000E-01 -9.OOOOOOE-01

1355603 -8.OOOOOOE-02 -8.000000E-01

1355604 O.OOOOOOE+O0 -6.700000E-01 , $$$ REMOVE ALL REMAINING DATA CARDS AFTER ACHIEVING STEADY STATE

* PUMP DATA

* ----.---- 1 ---- 1 .--------- I.-1-- ---- 1 ---- * SINGLE PHASE HEAD CURVES

* HEAD CURVE NO. 1

1651100 1 1

1651101 O.OOOOOOE+O0 1.403600E+00

1651102 1.906100E-01 1.363600E+00

1651103 3.896300E-01 1.318600E+00

1651104 5.939600E-01 1.232800E+00

1651105 7.902000E-01 1.133600E+00

1651106 1.OOOOOOE+00 1.OOOOOOE+O0

* -------- ---1- ---- 1 ----- --- --- 1 ---- * HEAD CURVE NO. 2

1651200 1 2

1651201 0.000000E+00 -6.700000E-01

1651202 2.OOOOOOE-01 -5.OOOOOOE-01

1651203 4.OOOOOOE-O1 -2.5000OOE-01

1651204 5.755400E-01 O.OOOOOOE+O0

1651205 7.443200E-01 2.583000E-01

1651206 7.734800E-01 3.778000E-01

1651207 8.631300E-01 6.326000E-01

1651208 1.•00000E+00 I.OOOOOOE+00

* -------- ---1- ---- 1 ------ 1 -- -------- * HEAD CURVE NO. 3

1651300 1 3

1651301 -1 .000000E+00 2.472200E+00

1651302 -8.057400E-01 2.047400E+00

1651303 -6.069000E-01 1.831000E+00

1651304 -4.068300E-01 1.624000E+00

1651305 -2.001710E-01 1.470500E+00

1651306 0.000000E+00 1.403600E+00

* ---------------- 1 ------ 1 ------- I --- * HEAD CURVE NO. 4

1651400 1 4

1651401 -1.OOOOOOE+0O 2.472200E+00

1651402 -8.229700E-01 1.996800E+00

1651403 -6.333200E-01 1.589700E+00

1651404 -4.5534OOE-01 1.327900E+00

....-1------1--

---1----1--

....- 1----1-

-...- 1------1..--

....- 1------1.-

-...-1------1..--

--1----..-1--

....- 1----1-

--1----1--

- 130 -
1651405 -2.710900E-01

1651406 -1.771600E-01

1651407 -9.073000E-02

1651408 O.OOOOOOE+00

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

1651500 1

1651501 O.O00000E+00

1651502 2.OOOOOOE-01

1651503 4.OOOOOOE-01

1651504 4.118000E-01

1651505 5.976300E-01

1651506 7.934670E-01

1651507 1.O00000E+00

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

* HEAD CURVE NO. 6

1651600 1

1651601 O.OOOOOOE+00O

1651602 9.109900E-02

1651603 1.865090E-01

1651604 2.717620E-01

1651605 4.558720E-01

1651606 5.744060E-01

1651607 7.405760E-01

1651608 7.666190E-01

1651609 8.714710E-01

1651610 1.OOOOOOE+00

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

* HEAD CURVE NO. 7

1651700 1

1651701 -1.OOOOOOE+00

1651702 -8.OOOOOOE-O1

1651703 -6.OOOOOOE-01

1651704 -4.OOOOOOE-01

1651705 -2.OOOOOOE-01

1651706 O.OOOOOOE+00

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

* HEAD CURVE NO. 8

1651800 1

1651801 -1.OOOOOOE+00

1651802 -8.OOOOOOE-01

1651803 -6.OOOOOOE-01

1651804 -4.OOOOOOE-01

1651805 -2.OOOOOOE-01

1651806 0.OOOOOOE+00 *-----------1----1--

1.194900E+00

1.060500E+00

1.015600E+00

9.342790E-01

5

2.500000E-01

2.800000E-01

3.400000E-01

2.768000E-01

4.584000E-01

6.992000E-01

1.000000E+00

6

9.342790E-01

9.Z29000E-01

8.963000E-01

8.750000E-01

8.433000E-01

8.355000E-01

8.466000E-01

8.469000E-01

8.838000E-01

1.OOOOOOE+00

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

7

-1.OOOOOOE+00

-6.300000E-01

-3.OOOOOOE-01

-5.OOOOOOE-02

1.500000E-01

2.500000E-01

8

-1.OOOOOOE+00

-9.700000E-01

-9.500000E-01

-8.800000E-01

-8.OOOOOOE-01

-6.700000E-01

S--1-- ---- 1 ----

...-- 1----1--

....- 1------1--

.... 1-- ....-1.--

.... 1-- ....-1.--

....- 1----1--

-- 1------1-....

--1-----1--

---1----1--

* SINGLE PHASE TORQUE DATA

TORQUE CURVE NO. 1

1651900 2 1

1651901 0.OOOOOOE+00 6.032000E-01

1651902 1.930000E-01 6.325000E-01

1651903 3.930000E-01 7.369000E-01

1651904 5.955200E-01 8.331000E-01

- 131 -
1651905 7.978200E-01

1651906 1.OOOOOOE+O0

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

* TORQUE CURVE NO. 2

1652000 2

1652001 O.OOOOOOE+O0

1652002 4.OOOOOOE-01

1652003 5.OOOOOOE-01

1652004 7.372550E-01

1652005 7.680490E-01

1652006 8.672300E-01

1652007 1.OOOOOOE+0O

* ----.---- 1 ----.-- 1 ---- * TORQUE CURVE NO. 3

1652100 2

1652101 -1.OOOOOOE+00

1652102 -8.009600E-01

1652103 -6.063800E-01

1652104 -4.068600E-01

1652105 -1.992800E-01

1652106 0.OOOOOOE+00

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

* TORQUE CURVE NO. 4

1652200 2

1652201 -1.000000E+00

1652202 -8.223400E-01

1652203 -6.337100E-01

1652204 -4.585300E-01

1652205 -2.670230E-01

1652206 -1.761070E-01

1652207 -8.931000E-02

1652208 O.OOOOOOE+O0

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

1652300 2

1652301 0.000000E+00

1652302 4.OOOOOOE-01

1652303 5.000000E-01

1652304 1.OOOOOOOE+0

* ----.---- --- ---- 1 ---- * TORQUE CURVE NO. 6

1652400 2

1652401 0.OOOOOOE+00

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+00

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

* TORQUE CURVE NO. 7

9.229000E-01

1.000000E+00

2

-6.700000E-01

-2.500000E-01

1.5000OOE-01

5.265860E-01

6.065940E-01

7.436600E-01

1.OOOOOOE+00

3

1.984300E+00

1.394000E+00

1.097500E+00

8.220000E-01

6.648000E-01

6.032000E-01

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

---1--w---1I-

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

--1----1---

....-1------..1,-

.... 1-- ....-1--

....- 1------..1----1-. ....-1--

4

1.984300E+00

1.830800E+00

1.682400E+O0

1.557000E+00

1.436200E+00

1.387900E+00

1.348100E+00

1.233610E+00

5

-4.500000E-01

-2.500000E-01

0.000000E+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-01

5.849000E-01

4.877000E-01

3.569000E-01

S---- ----1 ----

....-1-- ....-1--

--1------1--,

....- 1------1,-

....-1-----1-,

....- 1-----1.

- 132 -
1652500 2 7

1652501 -1.OOOOOOE+O0 -1.OOOOOOE+O0

1652502 -3.000000E-01 -9.000000E-O1

1652503 -1.OOOOOOE-OI -5.000000E-01

1652504 O.O00000E+00 -4.500000E-01

* TORQUE CURVE NO. 8

1652600 2 8

1652601 -1.OOOOOOE+O0 -1.OOOOOOE+O0

1652602 -2.500000E-01 -9.OOOOOE-01

1652603 -8.OOOOOOE-02 -8.OOOOOOE-01

1652604 O.OOOOOOE+00 -6.700000E-01

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

----1----

----1----

----1----

.... 1--,

* -------- 1---1 ---- ---- * HEAD CURVE

1653000 0

1653001 O.OOOOOOE+00

1653002 1.000000E-01

1653003 2.OOOOOOE-01

1653004 3.OOOOOOE-01

1653005 3.500000E-01

1653006 4.OOOOOOE-01

1653007 5.OOOOOOE-01

1653008 6.000000E-01

1653009 7.OOOOOOE-01

1653010 8.OOOOOOE-01

1653011 9.OOOOOOE-01

1653012 1.OOOOOOE+00

* ----.---- -------- 1 ---- * TORQUE CURVE

1653100 0

1653101 O.O00000E+00

1653102 1.OOOOOOE-01

1653103 2.OOOOOOE-01

1653104 3.000000E-01

1653105 3.500000E-O1

1653106 4.OOOOOOE-01

1653107 5.OOOOOOE-01

1653108 6.OOOOOE-01

1653109 7.OOOOOOE-01

1653110 8.OOOOOOE-01

1653111 9.OOOOOOE-01

1653112 1.OOOOOOE+O0

* PUMP 2-PHASE DIFFERENCE

* HEAD CURVE NO. 1

1654100 1

1654101 O.OOOOOOE+00

1654102 1.OOOOOOE+00

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

* HEAD CURVE NO. 2

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

--..-1------1---- ----1---I' --- 1----

O.OOOOO0E+O0

O.OOOOOOE+00

1.OOOOOOE-01

2.OOOOOOE-01

3.OOOOOOE-O1

6.OOOOOOE-01

6.OOOOOOE-01

6.OOOOOE-O1

6.OOOOOOE-01

5.OOOOOOE-01

3.OOOOOOE-01

O.OOOOOOE+00

O.OOOOOOE+00

O.OOOOOOE+00

1.OOOOOOE-01

3.OOOOOOE-O1

5.OOOOOOE-01

7.5000OOE-01

7.500000E-01

7.500000E-01

7.500000E-01

7.500000E-01

5.OOOOOOE-01

O.OOOOOOE+00

DATA

...--1------..1-........1------1--

----1------..1-----1----1--

1

1.OOOOOOE+00

1.OOOOOOE+00 --1---- 1-- ---- 1-- ....-1"-

--1----1-. ...- . 1--- ----

- 133 -
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.OOOOOOE-01

1654305 -6.OOOOOOE-01

1654306 -5.OOOOOOE-01

1654307 -4.OOOOOOE-01

1654308 -Z.5OOOOOE-01

1654309 -1.OOOOOOE-01

1654310 O.OOOOOOE+00

* -------- 1 ------ 1 ---- * HEAD CURVE NO. 4

1654400 1

1654401 -1.OOOOOOE+O0

1654402 -9.OOOOOOE-01

1654403 -8.000000E-01

1654404 -7.OOOOOOE-01

1654405 -6.OOOOOOE-01

1654406 -5.000000E-O1

1654407 -3.5000OOE-01

1654408 -2.OOOOOOE-01

1654409 -1.OOOOOOE-01

1654410 O.OOOOOOE+00

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

* HEAD CURVE NO. 5

1654500 1

1654501 O.OOOOOOE+00

1654502 2.OOOOOOE-O1

1654503 4.OOOOOOE-01

1654504 6.OOOOOOE-01

1654505 8.OOOOOOE-01

1654506 1.OOOOOOE+00

* ----.---- 1 ----.-- 1 ---- * HEAD CURVE NO. 6

1654600 1

1654601 O.OOOOOOE+00

1654602 1.OOOOOOE-Ol

1654603 2.5000OOE-01

1654604 4.OOOOOOE-01

1654605 5.OOOOOOE-01

1654606 6.OOOOOOE-01

1654607 7.OOOOOOE-01

1654608 8.OOOOOOE-01

1654609 9.OOOOOOE-01

1654610 1.OOOOOOE+O0

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

* HEAD CURVE NO. 7

1654700 1

2

1.OOO0OOE+O0

l.OOOOOOE+O0

3

-1.160000E+00

-1.240000E+O0

-1.770000E+00

-2.360000E+00

-2.790000E+00

-2.910000E+00

-2.670000E+00

-1.690000E+00

-5.OOOOOOE-01

O.OOOOOOE+00

4

-1.160000E+0O

-7.800000E-01

-5.OOOOOOE-01

-3.100000E-01

-1.700000E-01

-8.OOOOOOE-02

O.OOOOOOE+00

5.OOOOOOE-02

8.OOOOOOE-02

1.100000E-01

5

O.OOOOOOE+00

-3.400000E-01

-6.500000E-01

-9.300000E-01

-1.190000E+O0

-1.470000E+00

6

1.100000E-01

1.300000E-01

1.5000OOE-O1

1.300000E-01

7.OOOOOOE-02

-4.OOOOOOE-02

-2.300000E-01

-5.100000E-01

-9.100000E-01

-1.470000E+00

7

--1----..-1---

--1---...-1---

--1----1--

.... 1-- ....-1-....

....-1----1--

--1---- ..-1....

-1----..-1-..-.

-1---- ..-1-....

--1------1-....

----.--.- 1-....

- 134 -
1654701 -1.OOOOOOE+00

1654702 0.OOOOOOE00

* HEAD CURVE NO. 8

1654800 1

1654801 -1.OOOOOOE+0O

1654802 O.OOOOOOE+00

* ----.---- --- ---- 1 ---- * TORQUE CURVE NO. 1

1654900 2

1654901 O.OOOOOOE+00

1654906 1.OOOOOOE+00

* ---------------- 1 ---- * TORQUE CURVE NO. 2

1655000 2

1655001 O.OOOOOOE+00

1655007 1.OOOOOOE+00

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

* TORQUE CURVE NO. 3

1655100 2

1655101 -1.OOOOOOE+OO

1655102 -8.009600E-01

1655103 -6.063800E-01

1655104 -4.068600E-01

1655105 -1.992800E-01

1655106 O.OOOOOOE+00

* ------------ ---- ---- * TORQUE CURVE NO. 4

1655200 2

1655201 -1.O00000E+00

1655202 -8.223400E-01

1655203 -6.337100E-01

1655204 -4.585300E-01

1655205 -2.670230E-01

1655206 -1.761070E-01

1655207 -8.931000E-02

1655208 O.OOOOOOE+00

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

* TORQUE CURVE NO. 5

*-----------1------1--'

1655300 2

1655301 O.OOOOOOE+00

1655302 4.OOOOOOE-01

1655303 5.OOOOOOE-01

1655304 1.OOOOOOE+00

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

* TORQUE CURVE NO. 6

1655400 2

1655401 O.OOOOOOE+00

1655402 9.064300E-02

1655403 1.885690E-01

1655404 2.734700E-01

1655405 4.586690E-01

O.OOOOOOE+00

O.OOOOOOE+00 --1------1--...

--1------1-....

8

O.OOOOOOE+00

O.OOOOOOE+00 ....- 1------1..-1

....- 1------1'-

.... 1-- ....- 1---

....-1-- ....- 1--

....- 1----1------1----1"-

1

1.OOOOOOE+00

1.OOOOOOE+00

2

1.OOOOOOE+00

1.OOOOOOE+00

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

1.436200E+00

1.387900E+00

1.348100E+00

1.233610E+00

5

-4.5000OOE-01

-2.5000OOE-01

O.OOOOOOE+00

3.569000E-01

6

1.233610E+00

1.196500E+00

1.109600E+00

1.041600E+00

8.958000E-01

....- 1-- ....- 1--

....- 1-----1--

.... 1----1---

---1------1..-

....- 1------..1....

....- 1----1-

--1------1-....

- 135 -
1655406 5.744800E-01 7.807000E-O1

1655407 7.381600E-01 6.1340OOE-01

1655408 7.685200E-01 5.849000E-01

1655409 8.700570E-01 4.877000E-01

1655410 1.OOOOOOE+O0 3.569000E-01

* TORQUE CURVE NO. 7 *-----------1-. ....- 1------..1-"-----1-. ....- 1-. ....-1'-

1655500 2 7

1655501 -1.000000E+O0 -1.000000E+00

1655502 -3.OOOOOOE-01 -9.OOOOOOE-01

1655503 -1.OOOOOOE-01 -5.OOOOOOE-01

1655504 O.O00000E+O0 -4.500000E-01

* TORQUE CURVE NO. 8

1655600 2 8

1655601 -1.OOOOOOE+O0 -1.OOOOOOE+O0

1655602 -2.500000E-01 -9.OOOOOOE-01

1655603 -8.000000E-02 -8.OOOOOOE-01

1655604 O.OOOOOOE+00 -6.700000E-01

* STEADY STATE CONTROL SYSTEM

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

* PRIMARY COOLANT PUMP SPEED CONTROLLERS

* CALCULATE MASS FLOW ERROR

20590100 MSSERR SUM 1.0 0.0 1

20590101 192.40 -1.0 MFLOWJ 100010000

* ----.---- 1 .----- 1 ---- ---- * PUMP 1 SPEED

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

20590200 PCPISPD INTEGRAL 0.34482 133.000 1

20590201 CNTRLVAR 901

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

* PCP1 PUMP VELOCITY TABLE

1356100 501 CNTRL VAR 902

1356101 0.0 0.0

1356102 369.0 369.0

* MODIFY PCPl PUMP DATA

1350301 0 0 0 -1 0 6

* PUMP 2 SPEED

20590300 PCP2SPD INTEGRAL 0.34482 139.790 1

20590301 CNTRLVAR 901

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

* PCP2 PUMP VELOCITY TABLE

1656100 501 CNTRLVAR 903

1656101 0.0 0.0

1656102 369.0 369.0

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

.... .. 1-....

.... 1....

95 0

- 136 -
* MODIFY PCP2 PUMP DATA

1650301 0 0 0 -1 0 697 0

* -------- -------- 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. 1238620. 2459550. .00000000

4301101 150000000 430000000 0.0 0.0 0.0 0000

4301201 .777018-4 .777018-4 0.0

* -------- 1 ---- ------ 1 --------I ---- 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 4350301 904 999

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

* SPRAY VALVE POSITION CALCULATOR

20590400 SPRAY SUM -1.0 0.0 1 * CONTIN

+ 3 0.0 1.0

20590401 14.94+6 -1.0 P 420010000

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

* POSITION VS AREA TABLE

20299900 NORMAREA

20299901 0.0 0.0

20299902 0.0001 0.0

20299903 1.0 1.0

* PRESSURIZER HEATERS IN INITIALIZATION

* PRESSURIZER HEATER TRIPS

* LT 693 CYLCING HEATERS CARD 20241700

0000585 P 420010000 UT NULL 0 14.90+6 N

0000586 P 420010000 LT NULL 0 14.8999+6 N

0000666 586 OR 693 N

0000667 -585 AND 666 N

0000693 -503 AND 667 N

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

* LT 694 BACKUP HEATERS CARD 20241800

0000587 P 420010000 6T NULL 0 14.85+6 N

0000588 P 420010000 LT NULL 0 14.8499+6 N

0000668 588 OR 694 N

0000669 -587 AND 668 N

0000694 -503 AND 669 N

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

* PRESSURIZER HEATERS

14172000 2 9 2 1 0.0

- 137 -
14172100 0 1

14172101 8 8.3820E-3

14172201 4 8

14172301 1.0 8

14172401 615.0 9

14172501 0 0 0 1 5.4864 1

14172502 0 0 0 1 1.8288 2

14172601 415040000 0 1 1 5.4864 1

14172602 415040000 0 1 1 1.8288 2

14172701 417 1.0 0.0 0.0 1 * CYCLING

14172702 418 1.0 0.0 0.0 2 * BACKUP

14172901 0 1.6764E-2 1.6764E-2 5.4864 1

14172902 0 1.6764E-2 1.6764E-2 1.8288 2

• PRESSURIZER CYCLING HEATERS

20241700 POWER 693

20241701 0.0 0.0

20241702 1.0 3.6+4

*-------- 1 ---- ------ 1 -- -------- 1 ------ 1 ---- * PRESSURIZER BACKUP HEATERS

20241800 POWER 694

20241801 0.0 0.0

20241802 1.0 1.2+4

* -------- 1 ---- ------ 1 ---- 1 ------ 1 -- ---- 1 ---- * PRESSURIZER LEVEL CONTROL USING CHARGING AND LETDOWN COMPONENTS

* MODIFY PZR LEVEL CONTROL VARIABLE

20500206 0.1249 VOIDF 415060000

20500207 0.02477 VOIDF 420010000

20500208 0.02477 VOIDF 420020000

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

* CHARGING RESERVIOR

9800000 "CHRG RESRV" TMDPVOL

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----

• 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----

* CHARGING VALVE POSITION CALCULATOR

20590500 CHARGE SUM 7.7 0.0 1 *CONTIN

+ 3 0.0 1.0

20590501 1.1370 -1.0 CNTRLVAR 2

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

* LETDOWN SINK

9900000 "LTDWN SINK" TIDPVOL

- 138 -
9900101 1.0 1.0 0.0 0.0 0

9900102 4.0-5 0.0 00

9900200 3

9900201 0.0 1.4+7 559.2

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

* LETDOWN VALVE

9950000 "LTDWN VLV " VALVE

9950101 185000000 990000000 2.5-5 0.0 0

9950201 0 .00000000 .00000000 0.0

9950300 SRVVLV

9950301 906 999

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

* LETDOWN VALVE POSITION CALCULATOR

20590600 LETDOWN SUM -7.7 0.0 1

+ 3 0.0 1.0

20590601 1.1430 -1.0 CNTRLVAR 2

* -------- ------- 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 NORI.AREA

20254001 0.0 0.0

20254002 0.0001 0.0

20254003 1.0 1.0

* -------- 1 ------ 1 ------ 1 ---- * COMPUTE DELTA T ERROR

20590700 "DELTA T" SUM 1.0 0.0

20590701 556.6 -1. TEMPF 185010000

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

* FILTER DELTA T THRU DEADBAND

20590800 DEADBAND FUNCTION 1.0 0.0 1

20590801 CNTRLVAR 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 ---- * INTEGRATE DELTA T ERROR

20590900 "INT D T" INTEGRAL 1.0 0.0 1

20590901 CNTRLVAR 908

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

* STEAM VALVE POSITION CALCULATOR

20591000 TCONTROL SUM 1.0 0.44405 0

+ 3 0.40 0.55

20591001 0.44405 -0.0564 CNTRLVAR 908

20591002 -0.0059 CNTRLVAR 909

.0

.0

0.0

0100

*CONTIN

*CONTI

- 139 -
* SIMPLIFIED FEED SYSTEM CONTROLLER

* SIMPLIFIED FEED LOGIC

20591100 SGLVLERR SUM 1.0 0.0

20591101 3.1293 -1.0 CNTRLVAR 001

20591200 FEEDFLOW SUM 1.0 0.0

20591201 0.0 1.0 MFLOWJ 540000000

20591202 48.4 CNTRLVAR 911

* --- ---- --------------- 1 ---- * REPLACE FEED JUNCTION TABLE

5660200 1 0 CNTRLVAR 912

5660201 -100.0 19.017 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

* REPLACE REACTOR POWER TABLE

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

20290000 POWER 699 1.0 36.0+6

20290001 0.0 1.0

20290002 0.1 1.0

20290003 0.2 1.0

20290004 0.3 1.0

20290005 0.4 1.0

20290006 0.5 1.0

20290007 0.6 1.0

20290008 0.8 1.0

20290009 1.0 1.0

20290010 1.5 1.0

20290011 2.0 1.0

20290012 3.0 1.0

20290013 4.0 1.0

20290014 6.0 1.0

20290015 8.0 1.0

20290016 10.0 1.0

20290017 15.0 1.0

20290018 20.0 1.0

20290019 30.0 1.0

20290020 40.0 1.0

20290021 60.0 1.0

20290022 1.+5 1.0

* REPLACE TRIPS FOR STEADY STATE

* SCRAM

0000510 TIME 0 GE NULL 0 1.+9 L

* BREAK OPENS

0000511 TIME 0 GE NULL 0 1.+9 L

* PCP TRIP

0000512 TIME 0 GE NULL 0 1.+9 L

* HPIS ON

0000513 TIME 0 GE NULL 0 1.+9 L

* LPIS ON

- 140 -
0 GE NULL 0 1.+9 L . . . . . RELAP5 END CARD

- 141 -
APPENDIX C A base case input deck for a transient calculation

/JOB

L25BTR4,T5OOO.

/USER

ATTACH,RSTIN=LZ5SR.

ATTACH,STH2XT,RE364BX.

FILE,RSTIN,SBF=NO.

FILE,RSTPLT,SBF=NO.

DEFINE,PLOTFL=L25P4BL.

RFL,CM=370000,EC=200.

REDUCE(-)

RE364BX,,*PL=50000.

/EOR

= LOFf 1,2-5 BASE TRANSIENT TO 120 SEC

0000100 RESTART TRANSNT

0000101 RUN

0000103 14453

0000105 5.0 10.0

0000201 120.0 1.0-6 0.01 14003 10 1000

* REMOVE PUMP SPEED CONTROLLERS

*2059 1- -----1------1- 0 .-. 0-.0 -- 1----

20590100 MSSERR DELETE 0.0 0.0 0.0 0.0 0.0

20590200 PCP1SPD DELETE 0.0 0.0 0.0 0.0 0.0 20590300 PCP2SPD DELETE 0.0 0.0 0.0 0.0 0.0

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

* RENODALIZE PUMPI

1350000 "PCPUMP1 " PUMP

1350101 0.0 0.4572 0.0991 0.0 90.0

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 -1 695

1350302 369.00000 .35018970 .31550000 96.000000 500.64

1350303 613.60000 .00000000 207.43300 .04440000 19.591

1350310 0.0 0.0 0.0

---- 1----

1000

---- 1----

0.0

0.0

0.0 -- 1--

--- 1-....

)0000

8700

0.317900

0

1.4310000

.00000000

* PUMP DATA

* SINGLE PHASE HEAD CURVES

* HEAD CURVE NO. 1

1351100 1 1

1351101 O.OOOOOOE+00 1.403600E+00

1351102 1.906100E-01 1.363600E+00

1351103 3.896300E-01 1.318600E+00

1351104 5.939600E-01 1.232800E+00

1351105 7.902000E-01 1.133600E+00

1351106 1.O00000E+00 1.000000E+00

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

* HEAD CURVE NO. 2

- 142 -
* . --.--.. 1 --- . 1----

1351200 1

1351201 O.O00000E+00

1351202 2.OOOOOOE-01

1351203 4.000000E-01

1351204 5.7554OOE-01

1351205 7.443200E-01

1351206 7.734800E-01

1351207 8.631300E-01

1351208 1.OOOOOOE+00

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

* HEAD CURVE NO. 3

1351300 1

1351301 -1.OOOOOOE+O0

1351302 -8.057400E-01

1351303 -6.069000E-01

1351304 -4.068300E-01

1351305 -2.001710E-01

1351306 O.OOOO0OE+O0

* ----.---- 1 ----.-- 1 ---- * HEAD CURVE NO. 4

1351400 1

1351401 -1.OOOOOOE+O0

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 O.OOOOOOE+00

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

* HEAD CURVE NO. 5

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

1351500 1

1351501 0.O00000E÷O0

1351502 2.OOOOOOE-01

1351503 4.OOOOOOE-01

1351504 4.118000E-01

1351505 5.976300E-01

1351506 7.934670E-01

1351507 1.OOOOOE+O0

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

* HEAD CURVE NO. 6

1351600 1

1351601 0.000000E+O0

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.OOOOOOE+00

* ---- "-----1---1----

* HEAD CURVE NO. 7

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

2

-6.700000E-01

-5.000000E-01

-2.500000E-01

O.OOOOOOE+O0

2.583000E-01

3.778000E-01

6.326000E-01

1.OOOOOOE+O0

3

2.472200E+00

2.047400E+00

1.831000E+00

1.624000E+00

1.470500E+00

1.403600E+00

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

....-1------..1..-.

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

....-1--- -1--

....-1-- ....-1-

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

4

2.472200E+00

1.996800E+00

1.589700E+00

1.327900E+00

1.194900E+00

1.060500E+00

1.015600E+00

9.342790E-01

5

2.500000E-01

2.800000E-01

3.400000E-01

2.768000E-01

4.584000E-01

6.992000E-01

1.OOOOOOE+00

6

9.342790E-01

9.229000E-01

8.963000E-01

8.750000E-01

8.433000E-01

8.355000E-01

8.466000E-01

8.469000E-01

8.838000E-01

1.OOOOOOE+00

.1 -------- 1----

--1------1----.

---.1----1--..-

...- 1----1--..-

....-1----1--

.... 1-- ....-1-.-

- 143 -
* . --.--.. 1 ---- . 1---

1351700 1

1351701 -1.OOOOOOE+00

1351702 -8.OOOOOOE-01

1351703 -6.OOOOOOE-01

1351704 -4.OOOOOE-01

1351705 -2.OOOOOOE-01

1351706 0.OOOOOOE+00

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

* HEAD CURVE NO. 8

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

1351800 1

1351801 -1.OOOOOOE+O0

1351802 -8.OOOOOOE-01

1351803 -6.OOOOOOE-O1

1351804 -4.OOOOOOE-01

1351805 -2.OOOOOOE-01

1351806 O.OOOOOOE+0O

* SINGLE PHASE TORQUE DATA

* TORQUE CURVE NO. 1

1351900 2

1351901 O.OOOOOOE+O0

1351902 1.9300E-01

1351903 3.93OOOOE-01

1351904 5.955200E-01

1351905 7.978200E-01

1351906 1.OOOOOOE+OO

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

* TORQUE CURVE NO. 2

1352000 2

1352001 O.OOOOOOE+00

1352002 4.OOOOOOE-01

1352003 5.OOOOOOE-01

1352004 7.372550E-01

1352005 7.680490E-01

1352006 8.672300E-01

1352007 1.OOOOOE+00

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

* TORQUE CURVE NO. 3

1352100 2

1352101 -1.OOOOOOE+OO

1352102 -8.009600E-01

1352103 -6.063800E-01

1352104 -4.068600E-01

1352105 -1.992800E-01

1352106 O.OOOOOOE+OO

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

* TORQUE CURVE NO. 4

1352200 2

1352201 -1.O00000E+00

1352202 -8.223400E-01

1352203 -6.337100E-01

1352204 -4.585300E-01

7

-1.OOOOOOE+OO

-6.300000E-01

-3.OOOOOOE-01

-5.OOOOOOE-02

1.5000OOE-01

2.500000E-01

8

-1.OOOOOOE+O0

-9.700000E-01

-9.500000E-01

-8.800000E-01

-8.OOOOOOE-O1

-6.700000E-O1 ---- ------ 1----

....--- 1--

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

---- 1------1..-1

.... 1--....-1------..1------1--

6.032000E-01

6.325000E-01

7.369000E-01

8.331000E-01

9.229000E-01

1.O00000E+O0

2

-6.7000OOE-01

-2.500000E-01

1.500000E-01

5.265860E-01

6.065940E-O1

7.436600E-01

1.000000E+00

3

1.984300E+00

1.394000E+00

1.097500E+00

8.220000E-01

6.648000E-01

6.0320005-01

4

1.984300E+00

1.830800E+00

1.682400E+00

1.557000E+00

---- 1----1-

--1----1--

--- 1----1--

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

----1-----1--'

---1-------"

...--1------1--,

- 144 -
1352205 -2.670230E-01 1.436200E+00

1352206 -1.761070E-01 1.387900E+00

1352207 -8.931000E-02 1.348100E+00

1352208 O.OOOOOOE+O0 1.233610E+00

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

1352300 2 5

1352301 O.O00000E+00 -4.500000E-01

1352302 4.OOOOOOE-01 -2.5000OOE-01

1352303 5.OOOOOOE-01 O.OOOOOOE+00

1352304 1.OOOOOOE+O0 3.569000E-01

* ---- ---- 1 .----- - ---- 1 ----- 1 ------- 1 ---- * TORQUE CURVE NO. 6

1352400 2 6

1352401 O.OOOOOOE+00 1.233610E00

1352402 9.064300E-02 1.196500E+00

1352403 1.885690E-01 1.109600E+00

1352404 2.734700E-01 1.041600E+00

1352405 4.586690E-01 8.958000E-O1

1352406 5.744800E-01 7.807000E-01

1352407 7.381600E-01 6.134000E-01

1352408 7.685200E-01 5.849000E-01

1352409 8.700570E-01 4.877000E-01

1352410 1.000000E+00 3.569000E-01

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

* TORQUE CURVE NO. 7

1352500 2 7

1352501 -1.000000E+O0 -1.OOOOOOE+O0

1352502 -3.OOOOOOE-01 -9.OOOOOOE-01

1352503 -1.OOOOOOE-OI -5.OOOOOOE-01

1352504 O.O0OOOOE+O0 -4.500000E-01

* ----.---- 1 ----.-- 1 ------ 1 ------ 1 ---- * TORQUE CURVE NO. 8

1352600 2 8

1352601 -1.OOOOOOE+O0 -1.OOOOOOE+00

1352602 -2.500000E-01 -9.OOOOOOE-O1

1352603 -8.OOOOOOE-02 -8.OOOOOOE-01

1352604 O.OOOOOOE+0O -6.700000E-01

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

....-1----1....

....-1------..1....

....-1------1..--

.... 1----1-

....-1-- ....- 1-

-- 1-----1--

.... 1-- ....- 1"--

-- 1---...-1"--

...--1------..1"-

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

* HEAD CURVE

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

---1-"

1353000

1353001

1353002

1353003

1353004

1353005

1353006

1353007

1353008

1353009

1353010

1353011

0

O.OOOOOOE+O0

1.OOOOOOE-O1

2.OOOOOOE-01

3.OOOOOOE-01

3.5000OOE-01

4.OOOOOOE-01

5.OOOOOOE-01

6.OOOOOOE-01

7.OOOOOOE-01

8.OOOOOOE-01

9.OOOOOOE-01

O.OOOOOOE+O0

O.OOOOOE+00

1.OOOOOOE-O1

2.OOOOOOE-O1

3.OOOOOOE-01

6.0000O0E-01

6.OOOOOOE-01

6.OOOOOOE-01

6.OOOOOOE-01

5.OOOOOOE-01

3.000000E-O1

- 145 -
1353012 1.OOOOOOE+O0

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

* TORQUE CURVE

1353100 0

1353101 O.OOOOOOE+0O

135310Z 1.000000E-O1

1353103 2.OOOOOOE-01

1353104 3.OOOOOOE-01

1353105 3.5000OOE-01

1353106 4.OOOOOOE-01

1353107 5.OOOOOOE-01

1353108 6.OOOOOOE-01

1353109 7.OOOOOOE-01

1353110 8.OOOOOOE-01

1353111 9.OOOOOOE-01

1353112 1.000000E+00

* PUMP 2-PHASE DIFFERENCE

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

* HEAD CURVE NO. 1

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

1354100 1

1354101 O.OOOOOOE+00

1354102 1.000000E+00

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

* HEAD CURVE NO. 2

1354200 1

1354201 O.O00000E+00

1354202 1.000000E+00

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

* HEAD CURVE NO. 3

1354300 1

1354301 -1.O0OOOOE+O0

1354302 -9.000000E-01

1354303 -8.O00000E-01

1354304 -7.000000E-01

1354305 -6.OOOOOOE-01

1354306 -5.OOOOOOE-01

1354307 -4.OOOOOOE-01

1354308 -2.500000E-01

1354309 -1.000000E-01

1354310 O.OOOOOOE+00

* ----.---- 1 ----.-- 1 ---- * HEAD CURVE NO. 4

1354400 1

1354401 -1.OOOOOOE+00

1354402 -9.OOOOOOE-01

1354403 -8.000000E-01

1354404 -7.OOOOOOE-01

1354405 -6.OOOOOOE-01

1354406 -5.OOOOOOE-01

1354407 -3.5000OOE-01

1354408 -2.OOOOOOE-O1

1354409 -1.000000E-01

1354410 O.O00000E+00

O.OOOOOOE+00 ---- 1 ------ 1---- ---- 1-----1--

.... 1--....-1------..1------1..--

O.OOOOOOE+00

O.OOOOO0E+00

1.OOOOOOE-01

3.OOOOOOE-01

5.OOOOOOE-01

7.500000E-01

7.500000E-01

7.5000OOE-01

7.5000OOE-01

7.500000E-01

5.OOOOOOE-01

O.OOOOOOE+00

DATA

---- 1.----1-

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

1

1.OOOOOOE+O0 1.O00000OE+O0

2

1. OOOOOOE+00

1. 000000E1-0

3

_1..160000E+00

-1. 240000E+00

-1.770000E+00

-2.360000E+00

-2. 790000E+00

-2.910000E+00

-2.670000E+00

-1.690000E+00

-5.000000E-01

O.OOOOOOE+00

.--1-- --- ----

----1------..1---..

---- 1------1.--1

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

..-.-1----1--

-- 1------1---..

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

---1---...-1--...

.... 1-----1--

4

-1.160000E+O0

-7.800000E-01

-5.OOOOOOE-01

-3.100000E-01

-1.700000E-01

-8.OOOOOOE-02

O.OOOOOOE+00

5.OOOOOOE-02

8.OOOOOOE-02

1.100000E-01

- 146 -
* ----. -.-- 1---- -I -- * HEAD CURVE NO. 5

1354500 1

1354501 0.000000E+00

1354502 2.OOOOOOE-O1

1354503 4.OOOOOOE-01

1354504 6.OOOOOOE-01

1354505 8.OOOOOOE-01

1354506 1.OOOOOOE+00

* ---------------- 1 ---- , HEAD CURVE NO. 6

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

1354600 1

1354601 O.OOOOOOE+00

1354602 1.OOOOOOE-O1

1354603 2.500000E-01

1354604 4.OOOOOOE-01

1354605 5.OOOOOOE-01

1354606 6.OO0OOOE-01

1354607 7.OOOOOOE-01

1354608 8.00000OE-01

1354609 9.OOOOOOE-01

1354610 1.OOOOOOE+00

* ---------------- I ---- • HEAD CURVE NO. 7

1354700 1

1354701 -1.OOOOOOE+00

1354702 O.OOOOOOE+00

* ---- ---- '--------1----

• HEAD CURVE NO. 8

1354800 1

1354801 -1.OOOOOOE+O0

1354802 O.OOOOOOE+00

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

* TORQUE CURVE NO. 1

1354900 2

1354901 0. OOOOOE+O0

1354906 1.OOOOOOE+00

* ----.---- 1 ----.-- 1 ---- * TORQUE CURVE NO. 2

1355000 2

1355001 0.000000E+00

1355007 1.OOOOOOE+00

* ----.---- 1 ----.-- 1 ---- • TORQUE CURVE NO. 3

1355100 2

1355101 -1.OOOOOOE+00

1355102 -8.009600E-01

1355103 -6.063800E-01

1355104 -4.068600E-01

1355105 -1.992800E-01

1355106 O.OOOOOOE+00

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

-...-1------1------..1------..1-....

5

O.OOOOOOE+0O

-3.400000E-01

-6.500000E-01

-9.300000E-01

-1.190000E+00

-1.470000E+00

6

1.100000E-01

1.300000E-01

1.500000E-01

1.300000E-01

7.OOOOOOE-02

-4.OOOOOOE-02

-2.300000E-01

-5.100000E-01

-9.100000E-01

-1.470000E+00 ....-1----1---

7

O.OOOOOOE+O0

O.OOOOOOE+00 -...- 1----1--

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

8

O.OOOOOOE+00

O.OOOOOOE+00 .. I---1---1I-

....-1----1--

1

1.OOOOOOE+O0

1.OOOOOOE+0O

2

1.000000E+00

1.000000E+00

--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.-

3

1.984300E+00

1.394000E+00

1.097500E+00

8.220000E-01

6.648000E-01

6.032000E-01 .... 1-- ....- 1------..1------..1-....

- 147 -
* TORQUE CURVE NO. 4

1355200 2

1355201 -1.OOOOOOE+O0

1355202 -8.223400E-01

1355203 -6.337100E-01

1355204 -4.585300E-01

1355205 -2.670230E-O1

1355206 -1.761070E-01

1355207 -8.931000E-02

1355208 O.OOOOOOE+O0

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

1355300 2

1355301 O.OOOOOOE+00

1355302 4.OOOOOOE-01

1355303 5.OOOOOOE-O1

1355304 1.OOOOOOE+00

*-------- ---- ----1 ---- * TORQUE CURVE NO. 6

1355400 2

1355401 O.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 1.000000E+O0

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

* TORQUE CURVE NO. 7

1355500 2

1355501 -1.OO0OOOE+O0

1355502 -3.OOOOOOE-01

1355503 -1.OOOOOOE-01

1355504 O.OOOOOOE+00

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

* TORQUE CURVE NO. 8

1355600 2

1355601 -1.OOOOOOE+0

1355602 -2.500000E-01

1355603 -8.OOOOOOE-02

1355604 O.OOOOOOE+0O

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

* RENODALIZE PUMP 2

1650000 "PCPUMP2 " 1650101 0.0 0.514

1650102 0

1650108 160010000 0.0

1650109 170000000 0.0

1650200 0 1.492M

1650201 0 3.4620

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

4

1.984300E+00

1.830800E+00

1.682400E+00

1.557000E+00

1.436200E+00

1.387900E+00

1.348100E+00

1.233610E+00

5

-4.500000E-01

-2.5000ooE-01

O.OOOOOOE+O0

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-01

4.877000E-01

3.569000E-01

7

-1.OOOOOE+0

-9.OOOOOOE-01

-5.OOOOOOE-01

-4. 500000E-01

8

-1.OOOOOOE+OO

-9.OOOOOOE-01

-8.OOOOOOE-01

-6.700000E-01

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

PUMP

0.0991 0.0

....-1-----1-.

....-1------1.---

---------

....-1------..1--

---- 1------..1"-

---- 1--....-1"-

---- 1-- ....-1....

---- 1-- ....-1..-.

---- 1-- ....-1-....

---1----1-

90.0 0.317900

0.017 0.017 0000

0.1 0.1 0000

37+7 1.23094+6 2.46151+6 0.

3.4623 0.0

- 148 -
1650202 0 3.5798 3.5798 0.0

1650301 135 135 135 -1 -1 697 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------ 1 ------ 1----

* REMOVE SPRAY LINE, SPRAY VALVE, AND CALCULATOR

*4301010 ..... DEL---1------1------1-E 1.. 

4300000 SPRAY DELETE 4350000 SPRVLV DELETE

20590400 SPRAY DELETE 0.0 0.0 0.0 0.0 0.0 0.0

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

* REPLACE PRESSURIZER BACKUP/CYCLING HEATERS POWER TABLE

* BY ZERO POWER IN ORDER TO DESCRIBE HEATER-OFF OF PRZ.

* INSTEAD OF REMOVING PRESSURIZER HEAT STRUCTURE COMPNENTS

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

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

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

20500200 PZRLVL SUM 1.0 0.0 1

20500201 0.0 0.1815 VOIDF 415010000

20500202 0. 1524 VOIDF 415020000

20500203 0.3967 VOIDF 415030000

20500204 0.5289 VOIDF 415040000

20500205 0.3967 VOIDF 415050000

20500206 0.1943 VOIDF 415060000

20500207 0.1029 VOIDF 420010000

20500208 0.1029 VOIDF 420020000

9800000 "CHRO R" DELETE

9850000 "CHRG V" 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------1----

* REMOVE STEAM VALVE CONTROLLER

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

- 149 -
5400000 "CV-P4-10 " VALVE

5400101 530010000 541000000 0.0047772 0.0 0.0 0100

5400201 0 35.132 13.536 0.0

5400300 MTRVLV

5400301 687 688 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 DEADBAND 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----

* REMOVE FEED SYSTEM CONTROLLER

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

20591100 SGLVLE

20591200 FEEDFL

5660000 "FEED

5660101 565000

5660200 1

5660201 -100.0

5660202 0.0

5660203 0.5

5660204 1.0

5660205 1.5

5660206 2.0

5660207 2.5

* 900

20290000 POWER

20290001 0.0

20290002 0.1

20290003 0.2

20290004 0.3

20290005 0.4

20290006 0.5

20290007 0.6

20290008 0.8

20290009 1.0

20290010 2.0

20290011 6.0

20290012 10.0

20290013 20.0

20290014 50.0

20290015 60.0

'OW

000

DELETE

DELETE

It

0.0 0.0

0.0 0.0

TMDPJUN

0.05

0.0 0.0 0.0 0.0

0.0 0.0 0.0 0.0

508000000

689

18.630 0.0 0.0

18.630 0.0 0.0

10.0 0.0 0.0

2.50 0.0 0.0

1.00 0.0 0.0

0.25 0.0 0.0

0.00 0.0 0.0 --- 1------1--

*L2-5

*L2-5

*L2-5

*L2-5

*L2-5

*L2-5

*L2-5

S-----

REACTOR POWER VS TIME AFTER SCRAM ----1----

----1----

699 1.0 36.0+6

1.0

0.963758 *NEWLY GENERATED FROM L2-

0.659722 *AND L2-5 DECAY CURVE BY

0.5625

0.409722

0.274004

0.22917

0.145832

0.117425

0.1085

0.077943

0.0701122

0.06049765

0.041384

0.040139

5 POSTTEST

EDR

20290016 100.0 0.035159

* REPLACE TRIPS 510-514

* SCRAM

0000510 P 100010000 LT NULL 0 14.19+6 L

* BREAK OPENS

0000511 TIME 0 GE NULL 0 0.00 L

* PCP TRIP*MODIFYRFROM1.75CSEC:ACCORDINGOTO1EXP.DAT.REP. L2-5

0000512 TIME 0 GE NULL 0 0.94 L

* IHPIS ON

- 150 -
0000513 TIME 0 GE NULL 0 23.90 L

* LPIS ON

0000514 TIME 0 GE NULL 0 37.32 L

* REFLOOD INITIATION TRIP MODIFY

0000555 P 230120000 LE NULL 0 1.0+6 L

* -------- 1 ------ 1 ---- 1 -- ---- -------- ---- 1 ---- * RENODALIZE DEAD END OF FUEL MODULES

2510000 "DE FL MODS" SNGLVOL

2510101 0.0 0.7844123 0.1154214 0.0 90.0 0.7844123

2510102 3.81-6 0.214 00

2510200 0 14942600. 1422680.0 2461200.0 2.43866E-4

* -------- 1 ------ 1 ------ 1------ 1 ---- ------ 1 ---- * MINOR EDIT VARIABLES

*----------1 P-----1 0001------1------1------1-...

0000301 P 250010000

0000302 P 530010000

0000303 TEMPF 250010000

0000304 TEMPF 215010000

0000305 MFLOWJ 340010000 0000306 MFLOWJ 305010000

0000307 RHO 100010000

0000308 HI1'TEMP 002100501

0000309 HIlEMP 002100110

0000310 HTTEMP 002100410

0000311 HTTEMP 002100510

0000312 HTTEMP 002100810

0000313 HTTEMP 002101010

0000314 HTTEMP 002101110

0000315 MFLOWJ 600000000

0000316 MFLOWJ 610000000

0000317 CNTRLVAR 4

0000318 PMPVEL 165

* ---- ADDED MINOR EDIT VARIABLE

0000331 P 100010000

0000332 VOIDG 230010000

0000333 VOIDGJ 317000000

0000334 VOIDGJ 347000000

0000335 HTTEMP 002101210

0000336 CNTRLVAR 2

0000338 VOIDG 225010000

0000338 MFLOWJ 180010000

0000339 MFLOWJ 100010000

0000340 TEMPF 712010000

0000341 TEMPF 714010000

0000342 TEMPF 716010000

0000343 TEMPF 718010000

0000344 TEMPF 225010000

0000345 MFLOWJ 720000000

0000346 MFLOWJ 722000000

0000347 MFLOWJ 724000000

0000348 MFLOWJ 726000000

0000349 MFLOWJ 728000000

0000350 MFLOWJ 731000000

0000351 MFLOWJ 709000000

0000352 MFLOWJ 225010000

0000353 MFLOWJ 225020000

0000354 MFLOWJ 719000000

0000355 MFLOWJ 741000000

- 151 -
0000356 KFLOWJ 215020000

0000357 CNTRLVAR 1

0000358 CNTRLVAR 7

0000359 CNTRLVAR 8

0000360 CNTRLVAR 10

0000361 CNTRLVAR 12

0000362 CNTRLVAR 71

0000363 CNTRLVAR 72

0000364 CNTRLPVAR 75

0000365 CNTRLVAR 77

0000366 HTTEMP 001100110

0000367 HTTEMP 001100410

0000368 HTTEMP 001100510

0000369 HITEMP 001100810

0000370 IITTEMP 001101010

0000371 HITEMP 001101110

, ACCUMULATOR, TRIPS, AND CONTROL VARIABLE

, ACCUMULATOR VALVE TRIPS

0000579 MFLOWJ 610000000 GE NULL 0 0.0 N

0000580 CNTRL VAR 4 LT NULL 0 0.939 L

0000682 579 AND -580 N

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

* ACCUMULATOR LEVEL CONTROL VARIABLE

20500400 ACCMLVL INTEGRAL -6.549E-3 2.10 0

20500401 VELFJ 610000000

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

* ECC CHECK VALVE

6000000 "ECC CHKVILV" VALVE

6000101 605010000 185000000 0.0 1.3869 1.3869 0100

6000201 0 0.0 0.0 0.0

6000300 TRPVLV

6000301 681

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

* ECCS HEADER TO PCS

6050000 "ECCS HEADR" SNGLVOL

6050101 5.989E-3 4.8247 0.0 0.0 90.0 2.2061

6050102 1.0165-5 0.0 10

6050200 0 4.29E+6 125472. 2600290. 0.0

* ---- ---- ---- ---- 1 ------ 1------1------ 1 ------- I --- * 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 ------ 1 ------ 1 ---- * ACCUMULATOR PIPE

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

- 152 -
6150000 "ACC PIPE " SNGLVO

6150101 0.01608 24.5486 0.0

6150102 1.0165-5 0.0 10

6150200 3 4.29E+6 303.2

* ------------ 1 ---- 1--- --- 1 ---- * ACCUMULATOR VESSEL

6200000 "ACCUMIULATR" ACCUM

6200101 1.254 1.8261563 0.0

6200102 2.286-5 0.0 10

6200200 4.29E+6 303.2

6201101 615000000 8.213E-3 6.7582

6202200 1.45 0.0 4.0251

* RENODALIZE REACTOR VESSEL

* ACTIVE CORE

2300000 "CORE PIPE

2300001 12

2300101 0.183262 2

2300102 0.171287 4

2300103 0.172986 6

2300104 0.171486 8

2300105 0.171455 10

2300106 0.177236 12

2300201 0.183262 1

2300202 0.170500 2

2300203 0.171287 3

2300204 0.144000 4

2300205 0.172986 5

2300206 0.170500 6

2300207 0.171486 7

2300208 0.144000 8

2300209 0.171455 9

2300210 0.170500 10

2300211 0.177236 11

2300301 0.1397017 12

2300401 0.0 12

2300501 0.0 12

2300601 90.0 12

2300801 1.27-7 0.012 12

2300901 0.0 0.0 3

2300902 0.66 0.66 4

2300903 0.0 0.0 7

2300904 0.66 0.66 8

2300905 0.0 0.0 11

2301001 00 12

2301101 00100 11

2301201 0 14965200. 124161

2301202 0 14963900. 125998

2301203 0 14962600. 128366

2301204 0 14961300. 130819

2301205 0 14959600. 133312

2301206 0 14958400. 135734

2301207 0 14957200. 137857

2301208 0 14956000. 139538

0.0 0.0 0.0

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

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

0.0 -90.0 -1.8261563

8.3202 0

* 0.67056 0.04445 0 0 0 0 ....-1------..1------1..-1

....-1------..1------..1--

....-1------..1----1--

0.

0.

0.

0.

0.

0.

0.

0.

2460710. .00000000

2460740. .00000000

2460770. .00000000

2460800. .00000000

2460840. .00000000

2460860. .00000000

2460880. .0

2460900. .0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

0.0

01

02

03

04

05

06

07

08

- 153 -
2301209 0 14954300. 1409880. 2460930. .0 0.0 09

2301210 0 14953100. 1420370. 2460950. .0 0.0 10

2301211 0 14952100. 1424970. 2460980. .0 0.0 11

2301212 0 14950800. 1428220. 2461010. .0 0.0 12

2301300 0

2301301 1.3752000 1.3752000 0.0 01

2301302 1.3873000 1.4831000 0.0 02

2301303 1.4047000 1.5229000 0.0 03

2301304 1.6861000 1.8848000 0.0 04

2301305 1.4469000 1.5896000 0.0 05

2301306 1.4747000 1.6113000 0.0 06

2301307 1.4997000 1.6387000 0.0 07

2301308 1.7952000 2.0126000 0.0 08

2301309 1.5299000 1.7418000 0.0 09

2301310 1.5361000 1.7545000 0.0 10

2301311 1.5359 1.7821 0.0 11

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

* LOWER CORE SUPPORT STRUCTURE

2250000 "L CORE SUP" BRANCH

2250001 2 0

2250101 0.2832456 0.5709989 0.0 0.0 90.0 0.5709989

2250102 3.81-6 0.095 00

2250200 0 14970400. 1230690. 2460590. .00000000

2251101 225010000 230000000 0.1134 1.5 1.5 0100

2252101 225010000 235000000 0.0 12. 12. 0100

2251201 2.0569000 2.0569000 0.0

2252201 .67052000 .67052000 0.0

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

* UPPER HEAD

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 14934100. 1413720. 2461390. 6.97239-6

2521101 250010000 252000000 0.0 0.37 0.37 0100

2522101 730000000 252000000 0.0 0.90+4 0.90+4 0003

2521201 1.7356 1.8386 0.0

2522201 .0602599 .15501 0.0

* ---------------- 1 ------ 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 14937200. 1422700. 2461320. 3.42343-5

2501101 245010000 250000000 0.0 0.37 0.37 0100

2501201 1.7359000 1.8386000 0.0

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

* UPPER END BOXES AND SUPPORT STRUCTURE

2400000 "UPR END BV" 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 230010000 240000000 0.1118 1.5 1.5 0100

- 154 -
2402101 235010000 240000000 0.0 12. 12. 0100

2401201 2.3404000 2.8789000 0.0

2402201 .67053000 .87895000 0.0

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

* UPPER CORE SUPPORT STRUCTURE - CROSS FLOW REGION

2450000 "UPR CR SUP" BRANCH

2450001 2 0

2450101 0.0 0.4933248 0.1280806 0.0 90.0 0.4933248

2450102 3.81-6 0.145 00

2450200 0 14942600. 1422680. 2461200. 2.43866-4

2451101 240010000 245000000 0.0 0.0 0.0 0100

2452101 245010000 251000000 0.0 0.0 0.0 0100

2451201 1.1094000 1.3074000 0.0

2452201 -3.75341-6 9.0743224 0.0

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

* LOWER PLENUM 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 14975700. 1230730. 24604

2151101 215010000 220000000 0.0 0.005

2152101 215000000 225000000 0.1499 1.5

2151201 5.02601-7 5.02570-7 0.0

2152201 1.6140000 1.6140000 0.0

-90.0 -0.3533183

80. .00000000

0.0O5W

1.5 ' 01000100

* ----.---- 1 ----.-- 1 ---- * CONTAINMENT BROKEN LOOP

8000000 "CONT BLHL "

8000101 0.0 1.0

8000102 0.0 0.0

8000200 2

8000201 0.0 1.0+5

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

HOT LEG

TMDPVOL

0.1 0.0

00

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

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

0.0 0.0

1.0 *

*

*

*

CONTAINMENT BACK PRESSURE BEHAVIOR TABLE MODIFICATION

BY Y.S.BANG AT 89/3/4

8000202 0.5 2.0+5

8000203 20.0 2.9+5

8000204 37.0 2.7+5

8000205 60.0 2.7+5

8000206 70.0 3.1+5

8000207 120.0 3.1+5

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

* CONTAINMENT BROKEN LOOP

8050000 "CONT BLCL "

8050101 0.0 1.0

8050102 0.0 0.0

8050200 2

8050201 0.0 1.0+5

1.0

1.0

1.0

1.0

1.0

1.0

---- 1 ---- -- ---- COLD LEG ---- ---- 1 ---- TMDPVOL

0.1 0.0

00

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

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

0.0 0.0

1.0

*

*

CONTAINMENT BACK PRESSURE BEHAVIOR TABLE MODIFICATION

BY Y.S.BANG AT 89/3/4

8050202 0.5 2.0+5 1.0

8050203 20.0 2.9+5 1.0

- 155 -
8050204 37.0 2.7+5 1.0

8050205 60.0 2.7+5 1.0

8050206 70.0 3.1+5 1.0

8050207 120.0 3.1+5 1.0

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

* 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

* 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

20300100 P 250010000

20300200 P 530010000

20300300 TEMPF 250010000

20300400 TEMPF 215010000

20300500 MFLOWJ 340010000

20300600 IFLOWJ 305010000

20300700 RHO 100010000

20300800 HTTEMP 002100501

20300900 HTTEMP 002100110

20301000 HTTEMP 002100410

20301100 HTTEMP 002100510

20301200 HTTEMP 002100810

20301300 HI'TEMP 002101010

20301400 HITEMP 002101110

20301500 MFLOWJ 600000000

- 156 -
20301600 MFLOWJ 610000000

20301700 CNTRLVAR 4

20301800 PMPVEL 165

* ---- ADDED MINOR EDIT VARIABLE

20303100 P 100010000

20303200 VOIDG 230010000

20303300 VOIDGJ 317000000

20303400 VOIDGJ 347000000

20303500 HTTEMP 002101210

20303600 CNTRLVAR 2

20303800 VOIDG 225010000

20303900 MFLOWJ 180010000

20304000 MFLOWJ 100010000

20304200 TEMPF 712010000

20304300 TEMPF 714010000

20304400 TEMPF 716010000

20304500 TEMPF 718010000

20304600 TEMPF 225010000

20304700 MFLOWJ 317000000

20304800 MIFLOWJ 347000000

20304900 CNTRLVAR 1 *S/G LEVEL

20305000 CNTRLVAR 7 *DOWNCOMER LEVEL(INTACT SIDE)

20305100 CNTRLVAR 8 *DOWNCOMER LEVEL(BROKEN SIDE)

20305200 CNTRLVAR 10 *CORE LEVEL

20305300 CNTRLVAR 12 *TOTAL COLLAPSED CORE LEVEL

20305400 CNTRLVAR 71 *RV MASS

20305500 CNTRLVAR 72 *PCS MASS

20305600 CNTRLVAR 75 *TOTAL INJECTED MASS

20305700 CNTRLVAR 77 *TOTAL DISCHARGED MASS

20305800 MFLOWJ 720000000

20305900 MFLOWJ 722000000

20306000 MFLOWJ 724000000

20306100 MFLOWJ 726000000

20306200 MFLOWJ 728000000

20306300 MFLOWJ 731000000

20306400 MFLOWJ 709000000

20306500 IFLOWJ 225010000

20306600 MFLOWJ 225020000

20306700 NFLOWJ 719000000

20306800 MFLOWJ 741000000

20306900 MFLOWJ 215020000

20307000 HTTEMP 001100110

20307100 HITEIP 001100410

20307200 HTTEMP 001100510

20307300 HTTEMP 001100810

20307400 HTTEMP 001101010

20307500 HTTEMP 001101110

20307600 CPUTIME 0

20307700 CNTRLVAR 81

* CONTROL VARIABLES

* 001-006 LEVEL CALCULATORS

* 001 STEAM GENERATOR LEVEL

20500100 SGLVL SUm 1.0 0.0 1

20500101 0.0 0.4445 VOIDF 503010000

- 157 -
20500102 1.2131 VOIDF 505010000

20500103 0.6096 VOIDF 508010000

20500104 0.6096 VOIDF 510010000

20500105 0.6096 VOIDF 510020000

20500106 0.6096 VOIDF 510030000

* 002 PRESSURIZER LEVEL

*20500200 PZRLVL SUM 1.0 0.0

*20500201 0.0 0.1815 VOIDF 415010000

*20500202 0.1524 VOIDF 415020000

*20500203 0.3967 VOIDF 415030000

*20500204 0.5289 VOIDF 415040000

*20500205 0.3967 VOIDF 415050000

*20500206 0.1943 VOIDF 415060000

*20500207 0.1029 VOIDF 420010000

*20500208 0.1029 VOIDF 420020000

* 007 REACTOR VESSEL DOWNCOMER LEVEL INTACT SIDE

20500700 RVDCLVLIN SUM 1.0 0.0

20500701 0.0 0.3302040 VOIDF 700010000

20500702 0.3951272 VOIDF 702010000

20500703 1.5200561 VOIDF 704010000

20500704 1.2616333 VOIDF 706010000

20500705 1.0792591 VOIDF 708010000

20500706 0.3533183 VOIDF 215010000

20500707 0.3741720 VOIDF 220010000

* 008 REACTOR VESSEL DOWNCOMER LEVEL BROKEN SIDE

20500800 RVDCLVLBK SUM 1.0 0.0

20500801 0.0 0.3302040 VOIDF 710010000

20500802 0.3951272 VOIDF 712010000

20500803 1.5200561 VOIDF 714010000

20500804 1.2616333 VOIDF 716010000

20500805 1.0792591 VOIDF 718010000

20500806 0.3533183 VOIDF 215010000

20500807 0.3741720 VOIDF 220010000

* 010 REACTOR VESSEL CORE COLLAPSED LEVEL

20501000 RVLVL SUM 0.1397017 0.0 1

20501001 0.0 1.0 VOIDE 230010000

20501002 1.0 VOIDF 230020000

20501003 1.0 VOIDF 230030000

20501004 1.0 VOIDF 230040000

20501005 1.0 VOIDF 230050000

20501006 1.0 VOIDF 230060000

20501007 1.0 VOIDF 230070000

20501008 1.0 VOIDF 230080000

20501009 1.0 VOIDF 230090000

20501010 1.0 VOIDF 230100000

20501011 1.0 VOIDF 230110000

20501012 1.0 VOIDF 230120000

* 011 UPPER/LOWER PLENUM COLLAPSED LEVEL

20501100 UDLVL SUM 1.0 0.0 1

20501101 0.0 0.7749094 VOIDF 260010000

20501102 0.6312304 VOIDF 255010000

20501103 0.286958 VOIDF 252010000

20501104 0.7850547 VOIDF 250010000

20501105 0.4933248 VOIDF 245010000

20501106 0.5867979 VOIDF 240010000

20501107 0.5709989 VOIDF 225010000

20501108 0.3533183 VOIDF 215010000

20501109 0.374172 VOIDF 220010000

* 012 TOTAL COLLAPSED CORE LEVEL

- 158 -
20501200 CCCLEVEL

20501201 0.0

20501202

* 013 BOTTOM BASE L!

20501300 BBLEVEL

20501301 1.298489

* ACCUMULATOR LEVEL

20500400 ACCMLVL

SUM

1.0

1.0

IVE L

SUM

-1.0

1.0

CNTRLVAR

CNTRLVAR

0.0

10

11

1.0 0.0

CNTRLVAR 12

1

1

0..1... .1. .

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

INTEGRAL -6.3480-3 2.0447

20500401 VELFJ 620010000

* ---------------- ------ 1 ------ 1 ---- * 060-072 PRIMARY SYSTEM MASS CALCULATOR

* 060 CORE MASS

20506000 COREMAS SUM 1.0 0.0

20506001 0.0 2.5602-2 RHO 23001

20506002 2.5602-2 RHO 2300

20506003 2.3929-2 RHO 2300

20506004 2.3929-2 RHO 2300

20506005 2.4167-2 RHO 2300

20506006 2.4167-2 RHO 2300

20506007 2.3957-2 RHO 2300

20506008 2.3957-2 RHO 2300

20506009 2.3953-2 RHO 2300

20506010 2.3953-2 RHO 2301

20506011 2.4760-2 RHO 2301

20506012 2.4760-2 RHO 2301

1

0000

20000

30000

40000

50000

60000

70000

80000

90000

00000

10000

20000

* 061 INTACT LOOP HOT LEG MASS

20506100 ILHbMASS SUDl 1.0

20506101 0.0 0.102752 RHO

20506102 7.57291-2 RHO

20506103 6.43178-2 RHO

20506104 7.96973-2 RHO

20506105 5.79614-2 RHO

* 062 STEAM GENERATOR PRIMARY MASS

20506200 SGPRIMASS SUM 1.0

20506201 0.0 0.335320 RHO

20506202 0.136356 RHO

20506203 9.21538-2 RHO

20506204 9.21538-2 RHO

20506205 6.99783-2 RHO

20506206 6.99783-2 RHO

20506207 9.21538-2 RHO

20506208 9.21538-2 RHO

20506209 0.136356 RHO

20506210 0.335320 RHO

* 063 PUMP SUCTION PIPING MASS

20506300 PMPSUMASS SUM 1.0

20506301 0.0 4.45625-2 RHO

20506302 4.45137-2 RHO

20506303 3.54278-2 RHO

20506304 4.87901-2 RHO

20506305 6.40548-2 RHO

20506306 1.77444-2 RHO

20506307 6.40548-2 RHO

20506308 1.77444-2 RHO

* 064 INTACT LOOP COLD LEG MASS

20506400 ILCLMASS SUM 1.0

20506401 0.0 9.91000-2 RHO

20506402 1.83849-2 RHO

0.0

100010000

105010000

110010000

112010000

112020000

0.0

114010000

115010000

115020000

115030000

115040000

115050000

115060000

115070000

115080000

116010000

0.0

118010000

118020000

118030000

120010000

125010000

130010000

155010000

160010000

0.0

135010000

140010000

- 159 -
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 3.54Z80-2 RHO 175010000

20506408 3.88950-2 RHO 175020000

20506408 3.88950-2 RHO 175020000

20506409 7.30598-2 RHO 180010000

20506410 6.44920-2 RHO 185010000

* 065 DOWNCOMER/LOWER PLENUM MASS

20506500 DCLPMASS 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

20506505 0.0986806 RHO 708010000

20506506 0.0432082 RHO 710010000

20506507 0.0578606 RHO 712010000

20506508 0.1581866 RHO 714010000

20506509 0.1217000 RHO 716010000

20506510 0.0986806 RHO 718010000

20506511 0.24520 RHO 215010000

20506512 0.29656 RHO 220010000

* 067 UPPER PLENUM MASS

20506700 CRUPMASS SUM 1.0 0.0

20506701 0.0 0.12094 RHO 225010000

20506708 0.0091280 RHO 235010000

20506709 0.0072325 RHO 235020000

20506710 0.0088095 RHO 235030000

20506711 0.1195494 RHO 240010000

20506712 0.1280806 RHO 245010000

20506713 0.1436936 RHO 250010000

20506714 0.1154214 RHO 251010000

20506715 0.083595 RHO 255010000

20506716 0.310967 RHO 260010000

* 068 BROKEN LOOP HOT LEG MASS

20506800 BLHLMASS SUM 1.0 0.0

20506801 0.0 5.75410-2 RHO 300010000

20506802 4.42927-2 RHO 305010000

20506803 6.78467-2 RHO 310010000

20506804 7.75291-3 RHO 315010000

20506805 1.72111-1 RHO 315020000

20506806 8.97552-2 RHO 315030000

20506807 8.97552-2 RHO 315040000

20506808 1.72111-1 RHO 315050000

20506809 1.82303-2 RHO 315060000

20506810 5.46687-2 RHO 315070000

20506811 1.82489-2 RHO 315080000

20506812 9.15000-2 RHO 380010000

20506813 4.80000-2 RHO 380020000

20506814 4.89000-2 RHO 380030000

* 069 BROKEN LOOP COLD LEG MASS

20506900 BLCLMASS SUM 1.0 0.0

20506901 0.0 4.79790-2 RHO 335010000

20506902 4.43927-2 RHO 340010000

20506903 3.62484-2 RHO 342010000

20506903 3.62484-2 RHO 342010000

20506904 3.10679-2 RHO 344010000

20506907 2.79000-2 RHO 370010000

- 160 -
20506908 7.00000-2 RHO 370020000

20506909 1.16500-1 RHO 370030000

* 070 PRESSURIZER MASS

*20507000 PZRMASS SUM 1.0 0.0

*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

*20507012 2.12609-3 RHO 430010000

* 071 RECTOR VESSEL MASS

20507100 RVMASS SUM 1.0 0.0 1

20507101 0.0 1.0 CNTRLVAR 65

20507102 1.0 CNTRLVAR 67

20507103 1.0 CNTRLVAR 60

* 072 PCS 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 CNTRLVAR 69

20507207 1.0 CNTRLVAR 70

20507208 1.0 CNTRLVAR 71 ,

* TOTAL INJECTION MASS

20507400 TOINFL SUM 1.0 0.0 1

20507401 0. 1.0 MFLOWJ 600000000

20507402 1.0 MFLOWJ 640000000

20507500 INJMASS INTEGRAL 1.0 0.0 1

20507501 CNTRLVAR 74

* TOTAL DISCHARGE MASS

20507600 TOBRFL SUM 1.0 0.0 1

20507601 0. 1.0 MFLOWJ 317000000

20507602 1.0 MFLOWJ 347000000

20507700 BRMASS INTEGRAL 1.0 0.0 1

20507701 CNTRLVAR 76

20507701 CNTRLVAR 76

20507800 OLDTIME SUM 1. 0. 0

20507801 0. 1. CNTRLVAR 79

20507900 NEWTIME SUM 1. 0. 0

20507901 0. 1. TIME 0

20508100 TSTEP SUM 1. 0. 0

20508101 0. -1. CNTRLVAR 78

20508102 1. CNTRLVAR 79

- 161 -
* END OF INPUT

- 162 -
APPENDIX D Update list for a updated RELAP5/MOD2 Cycle 36.0

/JOB

RN364T,T200.

/USER

ATTACH,OLDPL=REL364S.

PURGE,RE364TS/NA.

PURGE,RE364TX/NA.

PURGE,RE364TL/NA.

* IMPORTANT !! *

* THE UPDATE DIRECTIVE *

* SHOULD HAVE *COMPILE DEFINE

* AS THE FIRST DIERECTIVE

UPDATE,N=RE364TS.

UPDATE,P=RE364TS,Q,C=R5SEG.

REPLACE,R5SEG.

RETURN,OLDPL.

*DEFINE,RE364TS.

RETURN,RE364TS.

ATTACH, ENVRLX=ENVR41X.

LIBRARY,ENVRLX.

SELECTA,COMPILE,COMP.

LIBRARY.

RETURN,ENVRLX.

REWIND,CONP.

FTN5,I=COMP,DO,ET,STATIC,OPT=2,ROUND,LO=M/A/R/S.

RETURN,COMP.

REWIND,LGO.

ATTACH, RELAP5I=REL36IL.

GTR,RELAP5I,ADD.REL/*

*DEFINE,RELAP50=RE364TL.

LIBEDIT,P=RELAP50,I=O,B=ADD,LO=F,U,C.

LIBEDIT,P=RELAP50,B=LGO, I=O,LO=F,U,C.

RETURN,NULL,LGO,RELAP5I.

RETURN, RLP5FI, RLP5F2.

ATTACH,ENVRL=ENVR41L.

FILE,RSTIN,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,$FERCAP.$,$RPVCAP.$,$FTNRP2.$,$QZNTRY.$.

NOGO.

RETURN,RELAP50,ENVRL,COMPILE.

SKIP,KKK.

EXIT.

ENDIF,KKK.

DAYFILE,KNRRDAY.

REPLACE,KMRRDAY.

/EOR

*COMPILE DEFINE

*ID CBD3604

*D DMK3601.484

*D PLOTMD.24

- 163 -
901 FORMAT ('OPLOTFL SCRACH FILE GENERATED.,) *COMPILE DEFINE,SEGDIR

*COMPILE RELAP5

*D RJW3603.23

DATA PTIThE/"RELAP5/2/3","6.04-PSI","REACTOR LO","SS OF COOL", */

*/ ENDIF

*ID KWUO1 ALREADY IMPLEMENTED IN RELAP50LDPL36O4C,

WHICH IS USED AS BASIS

/ */ CORRECTIONS OF INDEX IN SUBROUTINE RACCUM

*1 *I RACCUM.618

IELV=I

*B DMK3602.581

I=IELV

*COMPILE DEFINE,SEGDIR,RACCUM

*ID EWU01

*I RACCUM.618

IELV=I

*B DMK360Z.581

I=IELV

/ */ END OF KWU-UPDATES TO CYCLE 3604

*COMPILE DEFINE,SEGDIR

*IDENT SKIO0

THESE UPDATES ARE RECOMMENDED BY SKI TO BE

IMPLEMENTED IN RELAP5/MOD2-36.04

SOURCE: LETTER FROM STUDSVIK (MR.SANDERVAG) ,/ TO KWU (MR.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.MASK(43) .AND.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..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=(.NOT.MASK(43).AND.IH) + lIlT

J=(.NOT.MASK(43).AND.IHTPTR(J)) + IHT

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

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

*/ END OF UPDATES SKI01

*/ START OF PSI UPDATE

- 164 -
*ID MARTIN

*1 PHAINT.9

COMON/IFLGZ/IFLAGZ(1000)

DIMENSION IFLAGICO100)

*I PHAINT.151

IIFL1=(I-IVtIVSKP)/IVSKP

IFLAG1(IIFL1)=O

*I PHAINT.294

TGSAT=TGSAT-40.*VOIDF (I) *I PHAINT.370

IF(FBUB.GT.O.O.OR.FSLUG.GT.O.O.AND.DIAMV(I).LT.O.018)

1 IFLAG1(IIFL1)=I

*I PHAINT.390

IF(DIANV(I).LT.O.018) THEN

FIC=65.0*VOIDG(I)*VOIDF(I)**3.0*RHOG(I)/DIA!V(I)

ENDIF

*I PHAINT.421

IF(DIAMV(I).LT.O.018) THEN

FIC1=65.0*VOIDG(I)*VOIDF(I)**3.0*RHOG(I)/DIANV(I)

ENDIF

*I PHAINT.424

IF(DIAIIV(I).GE.O.018) THEN

*I PHAINT.425

ENDIF

*I PHAINT.495

IF(DIAMV(I).LT.O.018) FIC1=FIC1*0.5

*I PHAINT.633

IF(DIANV(I).LT.O.018) THEN

FIC1=VOID*(FIC1*0.5+1.225*0.4*RHOG(I)*SLSLG*VOID**2.)

ELSE

*I PHAINT.634

ENDIF

*I PHAINT.656

IF(DIANV(I) .LT.0.018) FIC=FIC*O.5

*1 PHAINT.462

IF(DIAMV(I).LT.O.018) FIC=FIC*O.5

*I PHAINT.855

IIFL2= (I-IJ+IJSKP)/IJSKP

IFLAG2(IIFL2)=O

*I PHAINT.919

INDK=(K-IV+IVSKP)/IVSKP

INDL=(L-IVtIVSKP)/IVSKP

IF(IFLAG1(INDK).EQ.1.OR.IFLAG1(INDL).EQ.1) IFLAG2(IIFL2)=1 *D QFHTRC.156

HTV2(INDZ)=HCCHFA*EXP(-0.0175*TERI)+GTERII*EXP(-0.O12*TERI)

*D QFHTRC.178

FACBR = (1.+0.025*AMAX1(0.,SATI(IDX)-TENPF(IDX)))

HCBR=AMAX1(HTV2(INDZ),(CONVAP*TER•1*TERI2*((SATHG(IDX)-SATHG(IDX))

*D QFHTRC.179

1/AMAX1(ThPBDY-SATT(IDX) ,O.01)+0.68*CSUBPG(IDX) )*9.81/(2.*3.14159)

*D QFHTRC.180

2 *SQRT(9.81*TERNI/SIGMA(IDX))/VISCG(IDX))**O.25*0.62*FACBR)

VELD=AMAX1(VELG(IDX)-VELF(IDX),O.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.+0.35*CSUBPG(IDX)*AMAX1(TMPBDY-SATT(IDX),O.0001)

1 /AMAX1(SATHG(IDX)-SATHF(IDX) ,0.01) )**3.

HCFO=0.4*3.14159/4.*(6.*(1.-VOIDG(IDX) )/3.14159)**0.6666667

- 165 -
1 *(9.81*RHOF(IDX)*RHOG(IDX)*AMAX1(SATHG(IDX)-SATHF(IDX),0.01)

2 *TERM5*CONVAP/(AAX1(TMIPBDY-TEMPF(IDX),0.0001)*VISCG(IDX) 3 *(3.14159/6. )**0.3333333*DDROP) )**0.25

IF(VOIDG(IDX).LE.O.6)THEN

HCFB=HCBR

ELSE

IF(VOIDG(IDX).GE.O.8) THEN

HCFB=HCFO

ELSE

HCFB=(VOIDG(IDX)-0.6)/0.2*HCFO+(0.8-VOIDG(IDX))/0.2

1 *HCBR

ENDIF

ENDIF

*D QFHTRC.187,188

TERP=TERP2+HCFB

*D QFHTRC.209

1 *AMAX1(0.023*(REYN2)**0.4/DIANV(IDX) ,TER 4)

*D QFHTRC.221,223

VELD=AMAX1(VELG(IDX)-VELF(IDX),0.001)

DDROP=3.*SIGMA(IDX)/(RHOG(IDX)*VELD**2)

IF(DDROP.LT.I.5E-4) DDROP = 1.5E-4

IF(DDROP.GT.3.OE-3) DDROP = 3.0E-3

TERN5=1./(1.+0.35*CSUBPG(IDX)*AMAX1(TMPBDY-SATT(IDX),0.0001)

1 /(SATIHG(IDX)-SATHF(IDX)))**3.

HCFO=0.4*3.14159/4.*(6.*(1.-VOIDG(IDX))/3.14159)**0.6666667

I *(9.81*RHOF(IDX)*RHO G(IDX)*(SATHG(IDX)-SATHF(IDX))

2 *TERII5*CONVAP/(AMAX1(TMPBDY-TEMPF(IDX) ,0.0001)*VISCG(IDX) 3 *(3.14159/6. )**0.3333333*DDROP) )**0.25

HCFB=HCFO

*I VEXPLT.9

COMMON/IFLG2/IFLAG2(1000)

*I VEXPLT.322

CO=1.0

c1=1.0

IIFL2=(I-IJ+IJSKP)/IJSKP

IF(IFLAG2(IIFL3) .EQ.1) THEN

CO=1.2

C1=(1.0-CO*VOIDGA)/AI/AX1((1.-VOIDGA),1.OE-5)

IF(C1.LT.O.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)*DT

*D VEXPLT.508

DIFG=-SCRACH-(FRICGJ+C1*FJFG+VPGNX+HLOSSG)*DT

*I VIMPLT.8

CONNON/IFLG2/IFLAG2(1000)

*1 VIMPLT.435

CO=1.0

Cl=1.0

IIFL2=(I-IJ+IJSKP)/IJSKP

IF(IFLAG2(IIFL2) .EQ.1) THEN

CO=1.2

Cl=(1.0-CO*VOIDGA)/AIMAX1((1.-VOIDGA),1.OE-5)

IF(C1.LT.O.7) C1=0.7

ENDIF

*D VIMPLT.436

FJFG=(FIJ(I)*DX*(ABS(CI*VELGJO(I)-CO*VELFJO(I))+0.01)

- 166 -
*D VIMPLT.591

COEFV(IDG-1) = (FRICFJ+CO*FJFG+VPGNX+HLOSSF)*DT + SCRACH

*D VIMPLT.592

COEFV(IDG) =-(FRICGJ+CI*FJFG+VPGNX+HLOSSG)*DT - SCRACH

*C DEFINE, PHAINT, QFHTRC,VEXPLT,VIMPLT

*/ END OF PSI UPDATE

*COMPILE ACCUM,PHAINT,DTSTEP

*/ PROTECTS SIGMA (SURFACE TENSION) BY 1.OE-7 IN SUBROUTINE PHAINT

*DELETE,PHAINT. 200

DSTAR(I) =DIAMV(I)*SQRT(9.8*RHOFG/AMAX1(SIGMA(I),1.OE-7)) *DELETE,PHAINT.326 55 VCRIT=2.5*SQRT(SQRT(AMAX1(SIGMA(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 MINIMUM TIMESTEP DUE TO

*/MASS ERROR

*DELETE,DTSTEP. 161

IF (NANY .EQ. 0) WRITE (OUTPT,2003)

*/ REWET CRITERIA REDUCTION (89/5/23 AKSAN & ICAP) *IDENT MARTIN2

*I HTRC1.60

GGT = RHOF(IV)*VOIDF(IV)*VELF(IV)+

1 RHOG(IV)*VOIDG(IV)*VELF(IV) *I HTRC1.111

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(XE.GE.XEC) GO TO 2000

13 CONTINUE

*I HTRC1.82

IF(GGT.GT.-100.) GO TO 11

*D HTRC1.83

IF(TW.GT.1250.-TSAT) GO TO 2000

11 CONTINUE

*1 PSTDNB.28

GUT = RHOF(IV)*VOIDF(IV)*VELF(IV)+

1 RHOG(IV)*VOIDG(IV)*VELG(IV)

*I PSTDNB.29

IF(GGT.GT.-100.) GO TO 231

*D PSTDNB.30

IF(XE.GT.XEC.OR.TW.GT.(1250.-TSAT)) GO TO 235

*I PSTDNB.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

- 167 -
401 IF(XE.GE.XEC)TRANS=.FALSE.

IF(TRANS) THEN

GO TO 402

ELSE

GO TO 403

ENDIF

402 HTCF=AMAX1(HTBF, HFB)

HTCG=AMAX1(HTBG,HV)

QFFO=AMAX1(QTFBF, QFBF)

QFGO=AMAXI( 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(-5.0*THETA*AMIN1(ABS(TW-TWRTO),SQRT(DTSAT)))

ELSE

IF(GGT.GE.-100..AND.GGT.LE.O) THEN

FL=((EXP(-2.0*THETA*AMIN1(ABS(TW-TWRTO),SQRT(DTSAT)))

1 -EXP(-5.O*THETA*AMIN1(ABS(TW-TWRTO) ,SQRT(DTSAT) ) ) )/100. )*GGT+

2 EXP(-2.O*THETA*AMIN1(ABS(TW-TWRTO),SQRT(DTSAT)))

ELSE

FL= EXP(-2.O*THETA*AMIN1(ABS(TW-TWRTO),SQRT(DTSAT)))

ENDIF

ENDIF

FL = FL*AMIN1(1.,(((1.-ALPH)/O.05)**4)) *D PSTDNB.67

HFB = 0.92163*(SQRT(HFB/SIGMA(IV))

*I PSTDNB.69

HCBR = HFB

VAMA = AMAX1(VELG(IV)-VELF(IV),O.001)

VFGZ = VAMA**2.

XA= AMAX1(3.*SIGNM(IV),1.E-1O)

RDIAI =RHOG(IV)*VFG2/XA

DDROP = 1./RDIAM

IF(DDROP.LT. 1.OE-4) DDROP=1.OE-4

IF(DDROP.LT.3.OE-3) DDROP=3.OE-3

TERM5=1./(1.+O.35*CSUBPG(IV)*AMAX1(TW-TSAT,O.O01)

1 /AMAX1(SATHG(IV)-SATHF(IV),0.001))**3.

HCFO=O.2*3.14159/4.*(6.*(I.-VOIDG(IV))/3.14159)**0.6666667

1 *(9.81*RHOF(IV)*RHOG(IV)*AMAX1(SATHG(IV)-SATHF(IV),0.01)

2 *TERM5*THCONS**3/(AMAX1(TW-TEMPF(IV),O.O1)*VISCS 3 *(3.14159/6. )**0.3333333*DDROP) )**0.25

HCFO = O.O01*HCFO

IF(VOIDG(IV).LE.O.60) THEN

HFB=HCBR

ELSE

IF(VOIDG(IV).GE.O.80) THEN

HFB=HCFO

ELSE

HFB=(VOIDG(IV)-O.60)/O.2*HCFO+(O.80-VOIDG(IV))/0.2

1 *HCBR

ENDIF

ENDIF

IF(GGT.LT.O.) THEN

HHHH=A-AX1(1.E-7,RHOF(IV)-RHOG(IV))

- 168 -
HFB=1.09680*VOIDF(IV)*SQRT((1./i.)

1 *THCONS**3*RHOG(IV)*HHHH*(HFG+O.5*DTSAT*CSUBPG(IV))

2 /(VISCS*DTSAT))**.25

ENDIF

*C HTRC1,PSTDNB,PREDNB

*/ END OF AKSAN UPDATE

/EOR

*COMPILE SEGDIR

- 169 -

NRC FORM 335 U.S. NUCLEAR REGULATORY COMMISSION I. REPORT NUMBER

12-89) lAssired by NRC. Add Vol., Suop.. Rev..

NRCM 1102. and Addendum Numbert,. If sny.) 3201.3202 BIBLIOGRAPHIC DATA SHEET NUREG/1nA- 0032

(See instructions on the reverse)

2. TITLE AND SUBTITLE

Assessment of RELAP5/MOD2 Cycle 36.04 Using LOFT 3. DATE REPORT PUBLISHED

Large Break Experiment L2-5 ,,oNTM , EA

April 1990

4. FIN OR GRANT NUMBER

!5. AUTHOR(S) 6. TYPE OF REPORT

Young Seok Bang Technical

Sang Yong Lee

Hho Jung Kim 7. PERIOD COVERED hicus... Dares,

8. PER FORMING ORGANIZATION - NAME AND ADDR ESS (Ii NRC. provide Oivsion. Office or Region, U.S. Nuclear Regulatory Commission and ma,hng address" . contralor. provd..

nawe and mailing address.)

Korea Nuclear Safety Center

Korea Advanced Energy Research Institute

P.O. Box 7, Daeduk-Danji

Daejon - Korea 9. SPONSOR ING OR GANIZATION - NAM E AND ADD RESS tit NRC. tpoe *To as #bove" il contrcto'. Provide NRC Divisio. Office or Regio. U.S Nudist Reularor• Commanion.

and mailing address.)

Office of Nuclear Regulatory Research

U.S. Nuclear Regulatory Commission

Washington, DC 20555

10. SUPPLEMENTARY NOTES

11. ABSTRACT 1200 voras or less)

The LOFT L2-5 LBLOCA Experiment was simulated using the RELAP5/MOD2

Cycle 36.04 code to assess its capability to predict the phenomena

in LBLOCA. One base case calculation and three cases of different

nodalizations were carried out. The effect of different nodalization was studied in the area of the downcomer and core. For a

sensitivity study, another calculation was executed using an

updated version of RELAP5/MOD2 Cycle 36.04.

A Split downcomer with one crossflow junction and two core channels

were found to be effective in describing the ECC bypass and hot

channel behavior. And the updated version was found to be effective

in overcoming the code deficiency in the interfacial friction and

reflood quenching.

12. KEY WORDS/DESCR!.PTORS (List words or phrases that illtassistrasearchers in locating the report.) 13. AVAILABILITY STATEMENT

Unlimited

14. SECURITY CLASSIFICATION

Simulation of the LOFT L2-5 LBLOCA Experiment Using the ,rhisPage)

RELAP5/MOD2 Cycle 36.04 Code Unclassified

ITPs Reoont)

Unclassified

15. NUMBER OF PAGES

16. PRICE

NRC FORM 335 12-891


UNITED STATES

NUCLEAR REGULATORY COMMISSION

WASHINGTON, -D.C. 20555

OFFICIAL BUSINESS

PENALTY FOR PRIVATE USE, $300

SPECIAL FOURTH-CLASS RATE

POSTAGE Er FEES PAID

U USNRC 

1

PERMIT No. G-67