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WESTIGHOUSE NON-PROPRIETARY CLAS 3 Oregon State University Department of Nuclear Engineering ADVANCED THERMAL HYDRAULIC RESEARCH LABORATORY TEST ACCEPTANCE REPORT OSU-AP1000-05 AP1000 2-INCH COLD LEG BREAK WITH 3 OF 4 ADS 4 ADS ACTUATION AT PLANT-PROTOTYPIC PRESSURE Revision 0

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WESTIGHOUSE NON-PROPRIETARY CLAS 3

Oregon State UniversityDepartment of Nuclear Engineering

ADVANCED THERMAL HYDRAULICRESEARCH LABORATORY

TEST ACCEPTANCE REPORT

OSU-AP1000-05

AP1000 2-INCH COLD LEG BREAK WITH 3 OF 4 ADS 4ADS ACTUATION AT PLANT-PROTOTYPIC PRESSURE

Revision 0

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APP-LTCT-T2R-005 WESTINGHOUSE NON-ftOPREmARY CLAsS 3 REVMON 0

TEST ACCEPTANCE REPORT

OSU-APIOOO-05

AP1000 2-INCH COLD LEG BREAK wITH 3 OF 4 ADS 4ADS ACTUATION AT PLANT-PROTOTYPIC PRESSURE

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Date

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Oregon State University116 Radiation Center

Corvallis, Oregon 97331

© 2003 Oregon State UniversityAll Rights Reserved

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COPYRIGHT NOTICE

This document bears an Oregon State University copyright notice. The NRC is permitted to make thenumber of copies of the information contained in these reports which are necessary for its internal use inconnection with generic and plant-specific reviews and approvals as well as the issuance, denial,amendment, transfer, renewal, modification, suspension, revocation, or violation of a license, permit,order, or regulation subject to the requirements of 10 CFR 2.790 regarding restrictions on publicdisclosure to the extent such information has been identified as proprietary by Westinghouse, copyrightprotection notwithstanding. With respect to the non-proprietary versions of these reports, the NRC ispermitted to make the number of copies beyond these necessary for its internal use which are necessary inorder to have one copy available for public viewing in the appropriate docket files in the public documentroom in Washington, DC and in local public document rooms as may be required by NRC regulations ifthe number of copies submitted is insufficient for this purpose. Copies made by the NRC must includethe copyright notice in all instances and the proprietary notice if the original was identified as proprietary.

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TABLE OF CONTENTS

Section Title Page

LIST OF TABLES ..................... viiSUMMARY.................................................................................................................................................iX

1.0 INTRODUCTION.........................................................................................................................i-1

2.0 TEST OBJECTIVE .2-1

3.0 FACILITY DESCRIPTION .. 3-13.1 Instrumentation.............................................................................................................. 3-2

4.0 OSU TESTING PROGRAM MATRIX .4-1

5.0 TEST PROCEDURE .5-1

6.0 TEST RESULTS .6-16.1 Initial and Boundary Conditions .6-16.2 Inoperable Instruments .6-16.3 Key Data Plots .6-16.4 Test Evaluation .6-1

7.0 CONCLUSIONS .7-1

APPENDIX A DATA PLOTS .................... A-1

APPENDIX B TEST DATA .................... B-1

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LIST OF TABLES

Table Title Page

Table 4-1 OSU Test Matrx (Specified July 9, 2003) ....................................... 4-2

Table 6-1 Actual Test Initial Conditions ....................................... 6-3

Table 6-2 Sequence of Events ....................................... 6-5

Table 6-3 Inoperable Instruments for T2R-02-D Test ....................................... 6-7

Table 6-4 Data Plots for QL Reports for T2R-02-D by Component ........................... ............ 6-8

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SUMMARY

This report covers the test TR-02, 2-inch Cold Leg Break simulation loss-of-coolant accident (LOCA)performed on July 9, 2003. The objective of this test was to obtain thermal-hydraulic data for 2-inch ColdLeg Break simulation with ADS-4 actuation at plant-prototypic pressure conditions. The test performedmet the specified conditions. The top of the heater bundle was always covered during this event. The testwas performed for about 2200 seconds. The transient continued through Automatic DepressurizationSystem (ADS) actuation, core makeup tank (CMT), accumulator, and incontainment refueling waterstorage tank (IRWST) injection.

This report presents the initial assessment of the test data collected. If this test is to be used byWestinghouse to support APIOOO Design Certification, additional validation of the use of this informationwill be documented separately. In the interim, the list of invalid data channels may change.

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1.0 INTRODUCTION

The Department of Nuclear Engineering at Oregon State University is performing a series of tests for theU.S. Department of Energy (DOE). These tests are being conducted in the Advanced Plant Experiment(APEX-1000) test facility, which is a reduced pressure and height model of the two-loop WestinghouseAP1000 pressurized water reactor. The purpose of the testing is to:

* evaluate the thermal-hydraulic performance of the passive safety systems of the full-scaleAPl000, and

* to assess and validate the safety analyses techniques and computer codes used in predicting thetransient system behavior.

The AP1000 Long-Term Cooling Test is a 1/4 height scale, low-pressure integral systems test simulatingthermal-hydraulic phenomenon for the APl000 passive safety systems for small-break loss-of-coolantaccidents (LOCAs) and long-term cooling. It accurately models the details of the AP1000 geometry,including the primary system, the passive safety systems, and a part of the non-safety grade Chemical andVolume Control System, as well as a partial non-safety grade Normal Residual Removal System. Theinterconnecting pipe routings are also duplicated in the model.

The overall objective of the Long-Term Cooling Test program is to obtain test data at various modes ofoperation. The Oregon State University (OSU) experiments will examine the passive safety systemresponse for the small-break and large-break LOCA transition into long-term cooling. (The list of thetests to be performed is provided in the attached OSU Test Matrix provided in Section 4.0.) The facilitypermits a range of small-break LOCAs to be simulated at different locations on the primary system, suchas the cold leg, hot leg, core makeup tank (CMT) cold leg pressure balance line, and direct vesselinjection line. The break orientation (top or bottom of the cold leg) may also be studied. Selected testscontinue into the long-term cooling, post-accident mode in which the passive safety injection is from thereactor sump as well as the incontainment refueling water storage tank (IRWST). A large-break,post-accident, long-term cooling situation will also be simulated.

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2.0 TEST OBJECTIVE

The purpose of this test is to obtain thermal-hydraulic data for a 2-inch Cold Leg Break simulation withADS-4 actuation at plant-prototypic pressure conditions. The break is located in cold leg #3 which is anon-balance line cold leg. The data obtained from the test will be used to verify the AP1000thermal-hydraulic computer codes for AP1000 phenomena such as gravity injection, natural convection,and post-accident long-term core cooling behavior.

The acceptance criteria for the OSU tests are as follows:

* Test initial conditions will be achieved within a specified tolerance.

* Set points will be achieved within an acceptable tolerance band.

* All instrumentation should be operational before the test.

* Any critical instruments not operating will be identified to the test engineer before the tests.These instruments must be operational before and during the test or exceptions should beapproved

* A zero check of LDPs, DPs, and FDPs will be performed.

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3.0 FACILITY DESCRIPION

A detailed facility description for the OSU test facility is documented in Reference 1. The OSU testfacility has been specifically scaled, designed, and constructed to investigate the AP600 passive safetysystem behavior and to provide data for safety analysis computer code validation. The facility has beenmodified to model the AP1000.

The scaled test design accurately models the details of the AP1000 geometry, including the primarysystem and the pipe routings and layout for the passive safety systems. A detailed scaling report(Reference 2) was used to develop the test design modifications. The primary system consists of one hotleg and two cold legs with two active pumps and an active steam generator for each loop. Two CMTs areconnected to one primary loop, and the pressurizer is connected to the other primary loop as in theAP1000 plant design. Gas-driven accumulators are connected to the DVI lines. The discharge lines fromthe CMT, and one-of-two [RWST and reactor sump lines are connected to each DVI line. The AutomaticDepressurization System (ADS), consisting of stages 1, 2 and 3, simulates either one or two of theindependent trains used in the AP1000. The two-phase flow from the ADS stages 1-to-3 is separated in aswirl-vane separator and the liquid and vapor flows are measured to obtain the total ADS flow rate. Theseparated flow streams are then recombined and discharged into the IRWST through a sparger, preservingthe mass and energy flow into the IRWST. The injection from the reactor sump is also simulated. Notethat the OSU facility models both APIOQO primary and secondary sumps. The primary sump collects thecondensate return, the liquid break flow, and the liquid flow from the fourth-stage ADS; and will providelong-term injection to the reactor vessel. The secondary sump simulates the portions of containment thatwill remain dry during most events. This sump will collect water only when the primary sump reaches itsoverflow level, and provides no injection to the reactor vessel.

The time period for the experimental simulations includes not only the IRWST injection, but also thedraining of the IRWST and the sump injection to simulate the long-term cooling of the APIOOO. Thissimulation could be from several hours to a day. The time scale for the OSU test facility is one-half; thatis, events occur in half the normal time. To model the long-term cooling aspects of the transient, thetwo-phase flow from the break is separated in a swirl-vane separator and the liquid and vapor portions ofthe total flow are measured. The liquid fraction of the flow is discharged to the reactor primary sump asin the APIOOO plant. The vapor is discharged to the atmosphere. The capability exists to return a portionof the equivalent liquid flow to the IRWST and primary sump to simulate the condensate return from thepassive containment to the IRWST and primary sump. A similar approach is also used for thefourth-stage ADS valve on the hot leg. The two-phase flow is separated in a swirl-vane separator, the twostreams are measured, and the liquid phase is discharged into the primary sump while the vapor flow isdischarged to the atmosphere. Again, the capability exists to return a portion of the liquid equivalentadded to the IRWST and primary sump. In addition, all other steam vents from the facility are measured(e.g., the IRWST vent), and a portion of the liquid equivalent may be added back to the facility. Note thatnot all of the steam discharge would be returned as liquid equivalent. A portion of the discharge would beremoved to simulate the steam that is not available for recirculation because it provides containmentpressurization. The IRWST and primary sump can be pressurized in the OSU facility to simulate thecontainment pressurization following a postulated LOCA.

A multi-tube passive residual heat removal (PRHR) heat exchanger is located in the IRWST. The heatexchanger uses the same C-tube design as the APIOOO and has two instrumented tubes to obtain wall heat

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fluxes during the tests. There are primary fluid thermocouples, wall thermocouples, and differentialpressure drop measurements to determine when the heat exchanger begins to drain. The IRWST is alsoinstrumented with strings of fluid thermocouples, to determine the degree of mixing within the tank andto assess the temperature of the coolant that is delivered to the test vessel.

The reactor vessel for the OSU tests includes a 0.914-meter (3-foot) heated core consisting of forty-eight0.025-meter (1-inch) diameter heater rods. The heater rods have a top skewed power shape. The1000 kW of electrical power available at the OSU test site will be used to simulate decay heat. Wallthermocouples are swaged inside the heater rods to measure the heater rod wall temperature.Thermocouple rods in the heater rod bundle measure the axial coolant temperature distribution. Thescaled flow volume in the core is preserved as well as the flow volume in the test vessel upper plenum.There are simulated reactor internals in the upper plenum to preserve the flow area and to correctly scalethe fluid volume. The reactor vessel includes an annular downcomer into which the four cold legs and thetwo DVI lines are connected. The hot legs penetrate the reactor annulus and connect with the loops. TheAP1000 reactor vessel neutron reflector is simulated using a ceramic liner to reduce the metal heat releaseto the coolant.

There were no special/unique requirements for the test other than those specified in the Initial Conditions.The specified conditions were verified on the control board prior to test implementation.

3.1 Instrumentation

The instrumentation has been designed to calculate a transient mass and energy balance on the testfacility. All two-phase flow streams exiting the facility are separated, and each component is measuredseparately as a single phase flow using conventional measurement devices such as magnetic flow metersand vortex flow meters. Note that magnetic flowmeters are not designed for two-phase flow and willindicate erratically. Also note, the vortex flowmeters are referenced to 212'F and the LDPs arereferenced to 60'F. All vertical components have differential pressure cells that act as level instrumentsto measure the transient mass change in the component. The hot and cold leg diameters are sufficientlylarge in the OSU test facility such that a narrow range differential pressure cell can be used to determineif the flow becomes stratified.

Single flow measurements are made of the CMT, accumulator, IRWST, and sump flows into the reactorvessel through the direct vessel injection lines.

Various types of instrumentation are provided in the test facility; for example, thermocouples for coolantand wall temperatures, flowmeters, pressure transducers, differential pressure transducers, and weightanks.

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4.0 OSU TESTING PROGRAM MATRIX

The test matrix for the OSU test facility is shown in Table 4-1. To satisfy the test objectives, severaltransients will be performed to provide data on the AP1000 passive safety system response for a range ofbreak sizes, locations, orientations, and single failure assumptions. The break size orifices are scaledbased on simulating a 1-inch, 2-inch, or 4-inch pipe break.

The designation for this test is TR-02, which identifies the test as a design basis 2-inch Cold Leg Breakwith ADS-4 actuation at plant-prototypic pressure conditions. The test matrix may be adjusted for futuretests based on results and insights gained with each test.

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TABLE 4-1OSU TEST MATRIX (SPECIFIED JULY 9,2003)

Test Title Break Location and Size Single Failure Assumed

DBA-01-D Double-ended DVI Line break with Fail 1 of 2 lines in ADS-4 traincontinuation into long-term cooling

DBA-02-D Double-ended DVI Line break with Fail 1 of 2 lines in 1 ADS-4 traincontinuation into long-term cooling (Adjusted ADS-4 Resistance)

Single failure on non-pressurizer side

DBA-03-D Double-ended DVI Line break with Fail 1 of 2 lines in 1 ADS-4 traincontinuation into long-term cooling Single failure on pressurizer side

DBA-04-D 2-inch Cold Leg Break (CL #3) Fail 1 of 2 lines in 1 ADS-4 train

Single failure on pressurizer side

TR-02-D Transition Test ADS4 opening, 125 psig initial Fail 1 of 2 lines in 1 ADS-4 trainpressure and decay power 480 sec (No ADS 1-3)

TR-03-D Transition Test ADS4 opening, 85 psig initial Fail 1 of 2 lines in 1 ADS-4 trainpressure and decay power 1800 sec (No ADS 1-3)

TR-4-D Transition Test ADS4 opening, 85 psig initial No Failure of ADS-4 lines assumedpressure and decay power 480 sec (No ADS 1-3)

EN-01-D Entrainment Test with Revised Upper Internals, Fail 1 of 2 lines in 1 ADS4 train1000 kW reactor power, 14.7 psi

EN-01-D Entrainment Test with Revised Upper Internals, Fail 1 of 2 lines in 1 ADS-4 train700 kW reactor power, 14.7 psi

PRA-O1-D PRA Test - DEDVI with no accumulators No ADS-4 Failure assumed

PRA-02-D PRA Test - 3-inch Hot Leg Break with no No ADS-4 Failure assumedCMTs

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S.0 TEST PROCEDURE

The test was performed as per a written procedure. There were no special/mique requirements for thetest other than those specified in the initial conditions in Table 6-1. The specified conditions werechecked on the control board prior to test implementation.

The appropriate prerequisites were completed and initial conditions were satisfied. The required breaksimulation piping and break instrumentation were installed per P&ID drawing OSU 600904, Rev. 1. Abreak spool insert simulating the 2-inch Cold Leg Break in AP1000 was installed in the break spool incold leg #3 which is a cold leg without a CMT balance line. Flow from the break is directed horizontallyinto the break separator. The 100-percent flow nozzle was installed in the ADS 4-2 (on the hot leg 2) andthe 50-percent flow nozzle was installed in ADS 4-1 (on the hot leg 1). Flow nozzles that simulate fullflow for ADS-1, ADS-2, and ADS-3 were installed. As per the AP600 tests, ADS-3 has been scaled forfull flow from all three stages, and ADS-1 and ADS-2 are closed when ADS-3 is opened.

Fill and vent was performed per APEX Operations Manual Procedure OP-B.2. Instruments were checkedfor required calibration.

With the break valve TS-202 closed, flow was used to warm up the bypass line by opening isolationvalves RCS-901 and RCS-902. After the appropriate prerequisites were completed and the test facilityachieved specified initial conditions, the CMT warm-up bypass line isolation valves RCS-901 andRCS-902 were closed to maintain the < 800F condition at the top of the CMT-1. With the CMT balanceline valves (RCS-529 and RCS-530) placed in the open and automatic mode, both CMTs reached thereactor coolant system (RCS) pressure.

Once all other initial conditions were satisfied, a break through TS-202 was initiated. The transientcontinued through ADS actuation. After ADS-I was actuated, the RCS pressure was monitored until itreached approximately 100 psia. At this point a number of operator actions were taken:

1. ADS4-1 was manually actuated, and ADS4-2 was actuated approximately 30 seconds later

2. Accumulators were isolated for the remainder of the test

3. The heater rod power controller was adjusted to simulate decay heat levels at 800 seconds(determined from test DBA-04 as the properly scaled time of ADS-4 actuation)

4. The level of the CMTs was recorded. The CMTs were allowed to drain an additional 20 inches,and then were isolated to simulate the inventory at ADS-4 actuation level.

Since the IRWST was not pressurized to simulate full-height, the IRWST cut-in for full-pressureconditions could not be simulated. Instead, the test continued to depressurize until the lower IRWSTcut-in pressure was reached, and stable IRWST injection was established. The test was terminated at thistime. IRWST actuation was automatic and required no operator action.

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6.0 TEST RESULTS

The test results for test TR-02-D are provided in the following subsections.

6.1 Initial and Boundary Conditions

Table 6-1 provides a comparison of the specified and actual conditions for test TR-02-D. The values inthis table were averaged over approximately 2 minutes preceding the test. Test initial conditions wereachieved for the steam generator pressure, pressurizer pressure, pressurizer level, steam generator 01narrow-range level, and steam generator 02 narrow-range level. Test initial conditions for the hot legtemperature were found to be acceptable, and the results will not be adversely affected.

The actual power decay curves are provided in data plots in Appendix B. The measured maximum powerwas 905 kW which was less than the facility maximum power of 1000 kW. The programmed decay heatcurve was adjusted to account for this difference, and the differences between the actual and specifiedpower decay are considered acceptable.

PT-501 and PT-502 pressure instruments indicate the pressure changes in the CMT-1 and CMT-2.CMT-1 (PT-501) and CMT-2 (PT-502) confirm that 1 minute after the test button was pushed, bothCMTs reach RCS pressure.

The sequence of events is shown in Table 6-2. This table compares the actual sequence of events with thespecified timing. As can be seen in this table, all the events occurred at or very near to when the eventwas planned.

6.2 Inoperable Instruments

Table 6-3 provides a list of the instrumentation channels considered inoperable for the DBA-04-D test.

6.3 Key Data Plots

Table 64 provides a list of the instrumentation channels sorted by component, and includes instrumentnumber, units, and quick look plot number. The selection of channels was based on projecting an overallpicture of the test results, which would then be examined by referring to the detailed data plots or tapes.

6.4 Test Evaluation

The following observations were made during the test:

1. The peak power before the test was initiated was 905 kW. The decay heat curve was adjusted forthis value.

2. As was discussed in Section 5.0, the test required significant operator action to simulate ADS-4actuation at plant-prototypic pressure. These actions were performed properly, and ADS-4 wasactuated when the RCS pressure reached approximately 100 psia.

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3. The test procedure called for the test to be terminated when the RCS pressure reached theplant-prototypic IRWST cut-in pressure of 28 psia. This pressure was reached with no coreuncovery observed. In addition, the pressure eventually decreased to the scaled IRWST cut-inpressure of 18 psia and stable IRWST injection was established with no core uncovery observed.

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TABLE 6-1ACTUAL TEST INITAL CONDITIONS

Conditions Instrument No. Actual Comment

Pressurizer Pressure PT-604 370 psig

Hot Leg Temperature TF-141* 426°F#1 TF-205 427.8°F

TF-143 428.30F

Hot Leg Temperature TF-140* 427.8°F#2 TF-206 426.3°F

TF-142 428.4F

SG Pressure PT-301 286.6 psig#1 PT-302* 284.4 psig#2 PT-002 268.3 psig

Header

PZR Level LDP-601 uncompensated 65.1 inches

LDP-601 77.1 inches 440°F used for densityCompensated by SC-608 compensation

SG Level LDP-303 uncompensated 20.1 inches

#1 NR LDP-303 compensated by 24.3 inches 413°F used for density

average of TF-305 and compensationTF-307

SG Level LDP-304 uncompensated 20.8 inches#2 NR

LDP-304 compensated by 25 inches 414°F used for densityaverage of TF-306 and compensationTF-308

IRWST Temperature TF-701 72°F Accepted (< 80°F)

CMT Temperature#1 TF-529 72°F Accepted (< 80°F)#2 TF-532 75.20F

AccumulatorTemperature TF-403 73.3 0F Accepted (< 800F)

#1 TF-404 75.2 0F#2

IRWST Level LDP-701 91.9 inches

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TABLE 6-1 (Continued)ACTUAL TEST INITIAL CONDITIONS

Conditions Instrument No. Actual Conmment

Accumulator Level#1 LDP-401 35.8 inches#2 LDP-402 36.8 inches

Accumulator Pressure#1 PT-401 228.6 psig#2 PT-402 233.9 psig

CMT Level#1 LDP-507 57.6 inches#2 LDP-502 57.7 inches

CMT Pressure#1 PT-501 374 psig#2 PT-502 375.4 psig

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TABLE 6-2SEQUENCE OF EVENTS

Event Setpoint Actual Time (sec)

PB Depressed N/A -120

Break Valve(s) Open 0 0

Feed Pump Trip Osec 0

CMT01 Outlet Valve Open (RCS-535) 6.1 sec 3

CMT02 Outlet Valve Open (RCS-536) 6.1 sec 3

PRHR HX Outlet Valve Open (RCS-804) 6.1 sec 3

RCP #1 Trip 4.6 sec 5

RCP #2 Trip 4.6 sec 6

RCP #3 Trip 4.6 sec 6

RCP #4 Trip 4.6 sec 6

CMT #1 Level Low (LDP-507) 41 inches 359

CMT #2 Level Low (LDP-502) 41 inches 397

ADS #1 Actuation (RCS-601) CMT Level Low + 15 sec 375

ADS #2 Actuation (RCS-602) CMT Level Low + 62 sec 421

ADS #3 Actuation (RCS-603) CMT Level Low + 122 sec 481

Low Reactor Pressure (P-107) 40 psig 515

IRWST Valve Actuation (RCS-71 1) Low Reactor Pressure 517(<40 psig)

IRWST Valve Actuation (RCS-712) Low Reactor Pressure 517(<40 psig)

ADS 4-1 Actuation (RCS-615) CMT Low Low (17.14") and 474CMT Low (41") + 180 sec

ADS 4-2 Actuation (RCS-616) CMT Low Low (17.14") and 499CMT Low (41") + 180 sec

Accumulator Injection#1 (FMM-401) N/A 412

Accumulator Injection#2 (FMM402) N/A 410

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APP-LTCT-T2R-005 RmmoN O

TABLE 6-2 (Continued)SEQUENCE OF EVENTS

Event Setpoint Actual Time (sec)

IRWST InjectionDVI #1 (FMM-701) N/A 875

IRWST InjectionDVI #2 (FMM-702) N/A 872

CMT Empty N/A 584 down to 21 inch level#1 (LDP-507)

CMI Empty#2 (LDP-502) N/A 581 down to 22.75 inch level

6272-NP.doc-081803 6-6

6272-NP.doc-081803 6-6

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APP-LTCT-2R-005 REISION APP-LTCT-T2R-005 REVISION 0

TABLE 6-3INOPERABLE INSTRUMENTS FOR TR-02-D TEST

Instrument Number Instrument Type Inoperable Description

TW-202 Thermocouple InoperativeTW-204TW-205TW-206TW-209TW-803TW-804

TH-603 Thermocouple measuring heater Inoperative. temperature

FMM-202 Magnetic flow meter Inoperative

TF-170 Thermocouple measuring fluid InoperativeTF-221 temperatureTF-509TF-512

FVM-905 Vortex flow meter Erratic

6272-NP~~~~~~~~~~~~~~~~~~~~~doc-081S03 6-7~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

6272-NP.doc-081803 67

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TABLE 6-4DATA PLOTS FOR QL REPORTS FOR TR-02-D BY COMPONENT

Component Channel Units QL-Plot Comment

Reactor Vessel PT-107 psig 44

Pressure

Reactor Vessel Level LDP-127 inch of H2 0 29

Reactor Vessel LDP-140 inch of H2 0 31

Downcomer Level

Cold Leg #1 Fluid TF-107 OF 58Temperature

Cold Leg #2 Fluid TF-108 OF 59Temperature

Cold Leg #3 Fluid TF-103 OF 56Temperature

Cold Leg #4 Fluid TF-104 OF 57

Temperature

Reactor Vessel Fluid TF-120 OF 60Temp Upper Head

RCS Hot Leg #1 TF-143 OF 62Temperature

RCS Hot Leg #2 TF-142 OF 61Temperature

Pressurizer Pressure PT-604 (WR) and PT-603 psig 49,50

(LP Indication)

Pressurizer Liquid LDP-601 inch of H20 38 Sharp decrease followed

Level by rapid refill.

SG #1 Tube Level LDP-215 inch of H20 32

SG #1 Secondary PT-301 psig 45

Pressure

SG #1 Feed Flow Rate FMM-001 gpm 1

SG #2 Tube Level LDP-218 inch of H2 0 33

SG #2 Secondary PT-302 psig 46Pressure

6272-NP.doc-081803 6-8

6272-NP.doc-081803 6-8

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APP-LTCT-T2R-005 REmoN O

TABLE 6-4 (Continued)DATA PLOTS FOR QL REPORTS FOR TR-02-D BY COMPONENT

Component Channel Units QI-Plot Comment

Accumulators #1 and PT-401 and PT-402 psig 47,48#2 Pressure

Accumulators #1 and LDP-401 and LDP-402 inch of H20 34,35#2 Liquid Level

Accumulators #1 and FMM-401 and FMM-402 gpm 2,3#2 Flow Rate

Accumulators #1 and TF-401 and TF-402 "F 63,64#2 Liquid DischargeTemperature ._.

CMT #1 and #2 Liquid LDP-507 and LDP-502 inch of H20 36,37Level

CMT #1 and #2 Flow FMM-501 and PMM-504 4,5Rate

CMT #1 and #2 Liquid TF-501 and TF-529 and OF 65 - 68Temperature TF-504 and TF-532

PRHR Inlet Flow Rate FMM-802 gpm 11

PRHR Liquid Level LDP-802 inch of H20 40

PRHR Outlet Flow FMM-804 gpm 12Rate

IRWST Liquid Level LDP-701 inch of H20 39

IRWST Discharge Line FMM-701 and FMM-702 gpm 9, 10#1 and #2 Flow Rate

IRWST Fluid TF-701 and TF-709 OF 69,70Temperature :

ADS 1-3 Separator PT-605 psig 51Pressure

ADS 1-3 Separator FVM-601 scfm 16Steam Flow Rate

ADS 1-3 Separator FMM-601 gpm 6Liquid Flow Rate

6272-NP.doc-081803 6-9

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TABLE 6-4 (Continued)DATA PLOTS FOR QL REPORTS FOR TR-02-D BY COMPONENT

Component Channel Units QL.Plot Comment

ADS 4-1 and ADS 4-2 PT-611 andPT-610 psig 52,53Separator Pressure

ADS 4-1 Separator FVM-603 scfm 18Steam Flow Rate

ADS 4-2 Separator FVM-602 scfm 17Steam Flow Rate

ADS 4-1 Separator FMM-603 gpm 8Liquid Flow Rate

ADS 4-2 Separator FMM-602 gpm 7Liquid Flow Rate

Primary Sump Pressure PT-901 psig 54

Primary Sump Liquid LDP-901 inch of H20 41Level

Primary Sump FMM-901 and FMM-902 gpm 13, 14Injection Flow Rate

Secondary Sump LDP-902 inch of H20 42Liquid Level

Break Separator PT-905 psig 55Pressure

Break Separator Liquid LDP-905 inch of H20 43Level

Break Separator Flow FMM-905 gpm 15to Primary Sump

BAMS Steam Flow FVM-901 scfm 19Rate

BAMS Steam Flow FVM-902 scfrn 20Rate

BAMS/Primary Sump FVM-903 scfm 21Steam Flow Rate

6272-NP.doc-081803 6-10

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TABLE 64 (Continued)DATA PLOTS FOR QL REPORTS FOR TR-02-D BY COMPONENT

Component Channel Units QL-Plot Comment

BAMS/Separator FVM-905 scfm 22Steam Flow Rate -6 inch Pipe

BAMS/Exhaust Line TF-916 and SC-917 OF 71,72Temperature

PZR Heater Input KW-601 kW 27Power

Core Power Input KW-101, KW-102, kW 23-26Power KW-103, and KW-104

Reactor Vessel liquid LDP-115 inches of 28Level Between Top of waterVessel - Upper Support

Plate

Reactor Vessel Liquid LDP-139 inches of 30Level Between Bottom waterof Upper SupportPlate - Upper CoreSpacer Grid

Inner Core TH-1034 0F 73ThermocoupleMeasuring HeaterTemperature

Outer Core TH-309-4 OF 74ThermocoupleMeasuring HeaterTemperature

6272-NPAoc-061S03 6-11

6Z72-NP~doc081803 6-11

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7.0 CONCLUSIONS

The TR-02-D test was successfully completed, and the data logged in the DAS. All critical instrumentswere found to operate properly with the exception of those noted in Section 6.4. The test was found to beacceptable.

6272-NP.doc-08 1803 7-1

6272-NP.&x-081803 7-1

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APPENDIX ADATA PLOTS

6272-NP.doc-081803 A-i

6272-NP.doc-08180 A-1

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APPLCTER-O REmSON OAPP-LTa-nR-oo5 REnSIOND

a,b~c

Figure A- Reactor Vessel Pressure

6272-NP.doc-O8 1803 A-3

6272-NP.dm-08I803 A-3

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APP-LTCT-T2R-005 REVISON

abc

Figure A-2 Reactor Vessel Level

6272-NP.doc-081803 A-4

6272-NP.cloc-081803 A 4

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abc

Figure A-3 Reactor Vessel Downcomer Level

6272-NPAoc-061803 A-5

6Zn-NPxocW0880 A-5

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APP-LTCr-72R-005 REVISION APP-LTCT-T2R-OO5 REvISIONS

a,b,c

Figure A-4 Cold Leg 1 Fluid Temperature

6272-NP.doc-081803 A-6

6272-NP.dm-081803 An6

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APP-LTCTT2R-005 REVMON

a,b,c

Figure A-S Cold Leg 2 Fluid Imperature

62'72-NP.doc-O8 1803 A-7

6272-NP.d=M48803 A-7

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APP-LTI-7YR-003 REwS10N APP-LTCr-T2R-005 REVISION 0

a,b,c

Figure A-6 Cold Leg 3 Fluid Temperature

6272-NP.doc-O8 1803 A-S

6272-NP.doc{081803 A-8

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abc

Figure A-7 Cold Leg 4 Fluid Temperature

6272-NP.dac-081803 A-9

6272-NP.dw-081803 A-9

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APr-LTCrT2R-005; REVISON APP-LTCF-T2R-005 REVISION 0

a,bc

Figure A-8 Reactor Vessel Fluid Temperature Upper Head

6272-NP.doc-081803 A-b

6272-NP.doc-081803 A-10

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APP-LTCT-77R-005 REVISON OAPP-LTCT-flR-OOS REVISION 0

abc

Figure A-9 Reactor Coolant System Hot Leg 1 Temperature

6272-NP.doc-081803 A-li

6272-NP.doc-MI803 A-11

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AP-LTCT-T2R-005 REIONZ 0APP-LTCT-T2R-005 REVISIoN 0

abc

Figure A-10 Reactor Coolant System Hot Leg 2 Temperature

6272-NP.doc-081803 A-12

6272-NP.doc4081803 A-12

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APP-LTCT-T2R-005 REVISON OAFP-LTa-T2R..oo5 REVISION 0

a,b,c

Figure A-l Pressurizer Pressure - Wide Range

6272-NP.doc-081803 A-13

6272-NP.d=c481803 A-13

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APP-LTI-T2R-005 RVSoN 0APP-LTCT-T2R-005 REVISION 0

abc

Figure A-12 Pressurizer Pressure - Narrow Range

6272-NP.doc-081803 A-14

6272-NP.doc-081803 A-14

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abc

Figure A-13 Pressurizer Liquid Level

6272-NP.doc-081803 A-iS

6272-NPedm-081803 A-15

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APP-LT=-T2R-003 REVISON APP-LTCT-flR-OO5 REVISIONS

a,b,c

Figure A-14 Steam Generator 1 Ihbe Level

627-NP.doc-081803 A-16

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atbc

Figure A-iS Steam Generator 1 Secondary Pressure

6272-NP.doc-0S 1803 A-17

62-NP.doc-W1803 A-17

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APP-LTCT-2R-OO5I REP~soT O

abc

Figure A-16 Steam Generator 1 Feed Hlow Rate

6272-NP.doc-08 1803 A-iS

6272-NP.doc-081803 A-18

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APP-LTCT T2R-OSRS REvisioN

a,b,c

Figure A-17 Steam Generator 2 hbe Level

6272-NP.doc-081803 A-19

6272NP.doc-81803 IA-19

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I I

APP-LTC-2R-005 RION APP-LTCT-TZR-005 REVISION 0

a,b,c

Figure A-18 Steam Generator 2 Secondary Pressure

6272-NP.doc081803 A-20

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abc

Figure A-19 Accumulator 1 Pressure

6272-NP.doc-081803 4.21

62MNP.doc-081803 A-21

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APP-LTC:T-TI2R-003 REVMON APP-LTCT-T2R-005 Rn'wON 0

ab,c

Figure A-20 Accumulator 2 Pressure

6272-NP.doc-08 1803 A-22

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ab,c

Figure A-21 Accumulator 1 Liquid Level

6272-NP.dac-08 1803 Nfl

62n-NP.doc-81803 A-23

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I

APP-LTCT-T2R-005 REVISIONi 0APP-LTa-nR-005 REVISION 0

abc

Figure A-22 Accumulator 2 Liquid Level

6272-NP.dac-081803 A-U

6272-NP.cloc-081903 A-24

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a,b,c

Figure A-23 Accumulator 1 flow Rate

6272-NP.doc08 1803 A-25

62-NP.doc-81803 A-25

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ab,c

Figure A-24 Accumulator 2 Flow Rate

6272-NP.doc-081803 A-26

6272-NP.doc-081803 A-26

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abc

Figure A-25 Accumulator 1 Liquid Discharge Temperature

6272-NP.doc-081803 Nfl

6272-NP.doc-081803 A-27

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APP-LTCT-T2R-005 REVISON

a,b,c

Figure A-26 Accumulator 2 Liquid Discharge Temperature

6272-NP.doc-081803 A-28

6272-NP.docz081803 A-28

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a,b,c

Figure A-27 Core Makeup Tank 1 Liquid Level

6272-NP.doc-081803 A-29

6272-NP.doc-081803 A-29

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a-bc

Figure A-28 Core Makeup Tank 2 Liquid Level

6272-NP.doc-081S03 A-30

6272-NP.docO081803 A-30

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APP-LTCTTOO00 REVISION APP-LTCT-TZR-005 REVISION 0

abc

Figure A-29 Core Makeup Ink 1 Flow Rate

6272-NP.doc-081S03 A-31

6272-NP.dm-081803 A-31

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abc

Figure A-30 Core Makeup Tank 2 Flow Rate

6272-NP.doc-081803 A-32

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abc

Figure A-31 Core Makeup Tank 1 Liquid Temperature - Bottom

6272-NP.doc081803 A-33

6272-NP.doc 08103 A-33

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a,b,c

Figure A-32 Core Makeup Tank 1 Liquid Temperature - Tbp

6272-NP.doc-08 1803 A-34

6272-NP.doc-081803 A-34

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abc

Figure A-33 Core Makeup Tank 2 Liquid Temperature - Bottom

6272-NP.doc-08 1803 A-35

6272-NP.dom081803 A-35

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APP-LTCT-T2R-005 REMsoOAPP-LTCT-flR-OO5 REVISION 0

a,b,c

Figure A-34 Core Makeup Tank 2 Liquid Temperature - Top

6272-NP.dacOSlSO3 A-36

6272-NP.doc-081803 A-36

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ArPP-LT C-72 R-005O RavmSIoN 0APP-LTa-TZR-OOS REVISION 0

abc

rigure A-3l Passive Residual Heat Removal Inlet Flow Rate

6272-NP.doc-081803 A-37

6272-NP.dwM 0180 A-37

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abc

FIgure A-36 Passive Residual Heat Removal Liquid Level

622-NP.doc-081803 A-38

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Figure A-37 Passive Residual Heat Removal Outlet now Rate

6272-NPAac-081803 A-39

627MP~doc-081803 A-39

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a,b,c

Figure A-38 IRWST Liquid Level

6272-NP.doc-081803 A-40

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abc

Figure A-39 IRWST Discharge Lne 1 Flow Rate

62'72-NP.doc-081803 A-41

6272-NP.dcZc-81803 A-41

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APP-LTCT-T2R-005 RmsioN 0

a,b,c

Figure A-40 IRWST Discharge Line 2 Flow Rate

6272-NP.doc-081803 A-42

6272-NP.doe-081803 A-42

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APP-LTCT-T2R-005 RESiON 0

a,b,c

Figure A-41 RWST Fluid Temperature - Bottom

6272-NP.doc4-1803 - 43

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APP-LTCr-T2R-005 REVISION

abc

Figure A-42 IRWST Fluid Temperature - Top

6272-NP.dac-0S1803 A-44

62-NP.dw-81803 A4

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a,b,c

Figure A-43 ADS 1-3 Separator Pressure

6272-NP.doc-081803 A-45

6272NP.doc-081803 A-45

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APP-LTCT-T2R-005 RzvSoN APP-LTCT-T2R-OOS REVISIONS

abc

FIgure A-44 ADS 1-3 Separator Steam Flow Rate

6272-NP.doc-0S1803 A-46

62-NP.doc-081803 A-46

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ab,c

Figure A-45 ADS 1-3 Separator Uquid Flow Rate

6272-NP.doc-081S03 A-47

6272-NP.doc-081803 A-47

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ab,c

Figure A-46 ADS 4-1 Separator Pressure

6272-NP.doc-081803 A-48

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Figure A-47 ADS 4-2 Separator Pressure-

6272-NP.doc-08 1803 A-49

6272NP.dc481803 A-49

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abc

Figure A-48 ADS 4-1 Separator Steam Flow Rate

6272-NP.dac-081803 A-50

6272-NP.doc-081803 A-50

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ab,c

Figure A-49 ADS 4-2 Separator Steam Flow Rate

6272-NP.doc-081803 A-Si

6272-NP dclm-81803 A-51

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L l l~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~

APP-LTC-T2R-oo5 REVMSON

a,b,c

Figure A-SO ADS 4-1 Separator Liquid flow Rate

6272-NP.doc-081803 A-52

6272-NP.dcc081803 A-52

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a,b,c

Figure A-SI ADS 4-2 Separator Uquid Flow Rate

6272-NP.dac-08 1803 A-53

6272eNP.doc 08180 -A-53

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Figure A-52 Primary Sump Pressure

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6272-NP.cloc-0818M3 A-54

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a,bc

Figure A-53 Primary Sump Liquid Level

6272-NP.docAJ8lRO3 A-55

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APP-LTCT-T2R-005 REMsoO

a-bc

Figure A-54 Primary Sump 1 Injection Flow Rate

0

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6272-NP.doe-081803 A-56

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abc

Figure A-55 Primary Sump 2 Nection Flow Rate

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6Z72NP.doc-081803 A-57

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abc

Figure A-56 Secondary Sump Liquid Level

6272-NP.doc-0S 1803 A-58

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ab,c

Figure A-57 Break Separator Pressure

6272-NP.doc-081S03 A-59

62-NP.dc<08180 A-59

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a,b,c

Figure A-58 Break Separator Liquid Level

62'72-NP.doc-081803 A-60

6272-NP.doc -081803 A-60

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abc

FIgare A-59 Break Separator Flow to Primary Sump

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abc

FIgure A-60 BAMS Steam How Rate - 6-inch Une

6272-NP.doc-081803 A-62

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a,b,c

Figure A-61 BAMS Steam Flow Rate - 10-inch Line

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abc

Figure A-62 BAMS/Primary Sump Steam low Rate

6272-NP.doc-081803 A-64

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a,b,c

Figure A-63 BAMSISeparator Steam Flow Rate - 6-inch Pipe

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6272-NP.doc-081803 A-65

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abc

Figure A-64 BAMS/Exhaust Line Temperature - 10-inch Line

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ab,c

Figure A-65 BAMS/Exhaust Line Temperature - Header

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ab,c

Figure A-66 Pressurizer Heater Input Power

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a,b,c

7

Figure A-7 Core Power Group 1 Input Power

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abc

Figure A-68 Core Power Group 2 Input Power

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a,b,c

Figure A-69 Core Power Group 1 Alternate Input Power

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62n-NP ic08180B A-71

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a,b,c

Figure A-70 Core Power Group 2 Alternate Input Power

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6272-NP.doc 0880 A-72

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ab,c

Figure A-71 Reactor Vessel Liquid Level Between Top of Vessel - Upper Support Plate

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6272NP.doc-08803 A-73

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a,b,c

Figure A-72 Reactor Vessel Liquid Level Between Bottom of Upper Support Plate -Upper Core Spacer Grid

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a,bc

Figure A-73 Inner Core Thermocouple Measuring Heater Temperature

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6272-NP~dw-08180 A-75

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aFbuc

Figure A-74 Outer Core Thermocouple Measuring Heater Temperature

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APPENDIX BTEST DATA

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