ML20049J194
| ML20049J194 | |
| Person / Time | |
|---|---|
| Site: | Surry  |
| Issue date: | 02/28/1982 |
| From: | Hendrixson E, Lozito E, Snow C VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.) |
| To: | |
| Shared Package | |
| ML18139B790 | List: |
| References | |
| VEP-FRD-47, NUDOCS 8203120247 | |
| Download: ML20049J194 (71) | |
Text
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V .E P - F R 0 - 47 l
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t Vepco i
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SURRY UNIT 2, CYCLE 6 s.
STARTUP PHYSICS TEST REPORT t .
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FUEL RESOURCES DEP.ARTMENT
. e20a5}??i e"NOoF.la.,tvic and Power Company DOCK 05000g
VEP-FRD-47 SURRY UNIT 2, CYCLE 6 STARTUP PHYSICS TEST REPORT BY ERIC S. HENDRIXSON Roviewed By! Approved 8 C.
c.1L T. Snow, Nuclear Fuel Engineer E E J Lo"=ito out irector H,uclear Fuel Operation Subsection H ear Fue peration Subsection Nuclear Fuel Operation Subsection Fuel Resources Department Virginia Electric and Power Co.
Richmond, Va.
February, 1982
, , _ - - ,.m._ . - - , , - _ _ - - , , , - - - - - - - a _.,- . _ - - . -- - . - - - - -
CLASSIFICATION / DISCLAIMER Tho data, techniques, information, and conclusions in this report have boon pgepared solely for use by the Virginia Electric and power Company (the company), and they may not be appropriate for use in situations other than those for which they were specifically prepared. The company therefore makes no claim or warranty whatsoever, express or implied,as to their accuracy, usefulness, or applicability. In particular, THE COMPANY MAKES NO WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, NOR SHALL ANY WARRANTY BE DEEMED TO ARISE FROM COURSE OF DEALING OR USAGE OF TRADE, with respect to this report or any of the.
data, techniques, information, or ' conclusions in it. By making this report available, the company does not authori=e its use by others, and any such use is expressly forbidden except with the prior written cpproval of the Company. Any such written approval shall itself be doomed to incorporate the disclaimers of' liability and disclaimers of untranties provided herein. In no event shall the Company be liable, under any legal theory whatsoever (whether contract, tort, warranty, or strict or absolute liability), for any property damage, mental or physical injury or death, loss of use of property, or other damage resulting from or arising out of the use, authori=ed or unauthori=od, of this report or the data, techniques, information, or conclusions in it.
D i
ACKNOWLEDGEMENTS The author would like to acknowledge the cooperation of the Surry Pc'we r Station personnel in performing the tests documented in this report. Also, the author would like to express his gratitude to Mr. C.
T. Snow, and Dr. E. J. Lozito for their aid and guidance in preparing
-this report.
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TABLE OF CONTENTS SECTION TITLE PAGE NO.
Classification / Disclaimer.... ............. i Acknowledgements........................... ii List of Tables............................. iv List of Figures............................ v Preface.................................... vi -
1 Introduction and Summary................... 1 2 Control Rod Drop Time Measurements......... 10 3 Reactor Coolant System Flow Measurement.... 15 4 Control Rod Bank Worth Measurements........ 17 5 Boron Endpoint and Worth Measurements...... 22 6 Temperature coefficient Measurements....... 26 7 Power Distribution Measurements............ 31 8 References................................. 41 APPENDIX StartuP Physics Test Results and Evaluation Sheets.......................... A.1 O
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LIST OF TABLES TABLE TITLE P4 E NO.
1.1 Chronology of Tests................................ 4 2.1 Hot Rod Drcy Time Summary.......................... 12 3.1 Reactor Coolant System Flow Measurement Summary.... 16 4.1 Control Rod Bank Worth Summary..................... 19 5.1 Boron Endpoints Summary............................ 24 6.1 Isothermal Temperature coefficient Summary......... 23 7.1 Incore Flux Map Summary............................ 33 7.2 Comparison of Measured power Distribution param-eters With Their Technical Specifications Limits... 34 b
e iv
l LIST OF FIGURES FIGURE TITLE PAGE NO.
1.1 Core Loading Map......................................... 5 1.2 Beginning of Cycle Fuel Assembly Burnups................. 6 1.3 Incore Instrumentation Locations......................... 7 1.4 Burnable Poison and Source Assembly Locations............ 8 1.5 Control Rod Locations.................................... 9 2.1 Typical Rod Drop Trace....................,.............. 13 2.2 Rod Drop Time - Hot Full Flow Conditions................. 14 4.1 Bank B Integral Rod Worth - HZP.......................... 20 4.2 Bank B Differential Rod Worth - HZP...................... 21 5.1 Boron Worth coefficient.................................. 25 6.1 Isothermal Temperature Coefficient - HZP, AR0............ 29 6.2 Isothermal Temperature Coefficient - HZP, B-Bank In...... 30 7.1 Assembly Power Distribution - HZP, AR0................... 35 7.2 Assembly Power Distribution - HZP, B-Bank In............. 36 7.3 Assembly Power Distribution - I/E Cal. - Flux Map........ 37 7.4 Assembly Power Distribution - I/E Cal. - Flux Map........ 38 7.5 Assembly Power Distribution - I/E Cal. - Flux map........ 39 7.6 Assembly Power Distribution - HFP, Eq. Xenon............. 40 V
PREFACE The purpose of this report is to present the analysis and ovoluation of the physics tests which were performed to verify that the surry 2, Cycle 6 core could be operated safely, and to make an initial oveluation of the performance of the core. It is not the intent of this report to discuss the particular methods of testing or to present the dotalled data taken. Standard test techniques and methods of data enelysis were used. The test data, results and evaluations, together with the de tailed startup procedures, are on file at the Surry power Station. Therefore, only a cursory discussion of these items is included in this report. The analyses presented includes a brief summary of each test, a comparision of the test results uith design prodictions, and an evaluation of the results.
The Surry 2, Cycle 6 Startup physics Tests Results and Evaluation Shoets have been included as an appendix to provide additional information on the startup test results. Each data sheet provides the follouing information: 1) test identification, 2) test conditions (dosign), 3) test conditions (actual), 4) test: results, 5) acceptance criteria, and 6) comments concerning the test. These sheets provide a compact summary of the startup test results in a consistent format. The design test conditions and design values of the measured parameters were conpleted prior to startup physics testing. The entries for the design values were based on the calculations performed by Vepco's Nuclear Fuel Engineering Group.1 During 'he tests, the data sheets were used as guidelines both to verify that the proper test conditions were met and vi
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i to facilitate the preliminary comparison between measured and predicted tact results, thus enabling a quick identification of possible problems occuring during the tests. The Appendix to this report contains the finci completed and approv C 'orsion of the Startup physics Tests j Recults and Evaluation Sheets.
S vii
Soction 1 INTRODUCTION AND
SUMMARY
On November 7, 1981 Unit No. 2 of the Surry Power Station was chutdown for its fifth refueling. During this shutdown, 68 of the 157 fual assemblies in the core were replaced with fresh fuel assemblies.
Tho sixth cycle core consists of 6 batches of fuels a once-burned batch frca Cycle 2 (Batch 4A5), a once-burned batch from Cycle 4 (Batch 6A2),
tuo once-burned batches from Cycle 5 (Batches 7A and 7B), one twice-burned batch from Cycles 4 and 5 (Batch 6B2), and one fresh batch (Botch *). The core loading pattern and the design parameters for each batch are shown in Figure 1.1. ruel assembly burnups are given in Figure 1.2. The incore instrumentation locations are identified in Figure 1.3. Figure 1.4 identifies the location and number of burnable poicon rods and source assemblies for Cycle 6, and Figure 1.5 identifies the location and number of control rods in the Cycle 6 core.
On December 28, 1981 at 1745, the sixt,h cycle. core achieved initial criticality. Following criticality, startup physics tests were parformed as outlined in Table 1.1. A summary of the results of these tacts follows:
- 1. The drop time of each control rod was confirmed to be within the 1.8 second limit of the Surry Technical Specifications 2
- 2. The reactor coolant system flow rate was confirmed to be greater than the minimum limit specified in the Final safety Analysis Report 3 1
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- 3. Individual control rod bank worths for all control rod banks were measured using the rod swap technique
- and were found to be within 7.3% of the design predictions. The sum of the individual control rod bank worths was measured to be within 0.3% of the design prediction. These results are within the design tolerance of 215% for individual bank worths (210% for the rod swap reference bank worth) and the
, design tolerance of 110% for the sum of the individual l
control rod bank uorths.
- 4. Critical boron concentrations for two control bank configurations were measured to be within 16 ppm of the design predictions. These results were within the design tolerances and also meet the accident analysis acceptance i criterion.
- 5. The boron, worth coefficient was measured to be within 7.2%
of the design prediction, which is within the design tolerance of 110% and meets the accident analysis criterion.
I
- 6. Isothermal temperature coefficients for two control bank configurations were measured to be within 1.0 pcm/*F of design predictions. These results are within the design tolerance of 23 pcm/*F and also meet the accident analysis acceptance criterion.
- 7. Core power distributions at HZP indicated that with the excep-tion of several core locations in the flux map taken with Control Bank B nearly fully inserted (S2-06-02), the measured assemblyuise power values were within the established design 2
tolerance. Moasured assemblyuise power distributions for =ero-power flux aaps were generally within 10" of predicted power distributions, while the difference for at power maps was generally less than 5%. The deviations of power distribution at HZp had no adverse consequences since, for all maps, the hot channel factors were measured to be within the limits of the Technical Specifications.
In summary, all startup physics test results were acceptable.
Datailed results, together with specific design tolerances and cecoptance critaria zor each measurement, are presented in the cypropriate sections of this report.
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Table.1.1 SURRY 2 - BOL CYCLE 6 PHYSICS TESTS CHRONOLOGY OF TESTS l l . I l l Referencel l Test i Date l Time l Power l Procedurel i I I I I I I I L I I I l Hot Rod Drop-Hot Full Flow 112/27/811 2200 l HSD l PT-7 l l Ro ac tivi ty Computer Checkout 112/29/811 0600 l HZP lPT28.11(B)I I Boron Endpoint-ARO 112/29/811 1030 i HZP lPT28.11(C)l l Tomperature Coefficient-ARO 112/29/811 1354 l HZP lPT28.11(D)l l Flux Map-ARO 112/30/811 0202 i HZP l OP-57, I l l l l l PT28.2 l l Benk B Worth 112/30/811 0530 i HZP IPT28.11(E)l l Boron Endpoint-B In 112/30/811 1139 I HZP lPT28.11CC)l l Tcmperature Coefficient-B In 112/30/811 1205 l HZP lPT28.11(D)l l Flux Map-B In 112/30/811 1424 i HZP l OP-57, I l l l l l PT28.2 l l Bank D Worth - Rod Swap 112/30/811 2200 l HZP lPT28.11(F)l l Bcnk C Worth - Rod Guap 112/30/811 2243 i HZP IPT28.11(F)l l Bcnk A Worth - Rod Swap 112/30/811 2343 i HZP lPT28.11(F)I I Bcnk SB Worth - Rod Swap (12/31/811 0015 1 1. Z P IPT28.11(F. .
I Bank SA Worth - Rod Suap 112/31/811 0048 l HZP lPT28.11(F)!
I a'.x Map - HI Calibration I 1/1/82 1 0448 1 47% i OP-57, I I l l l l PT28.2 l l Flux Map - HI Calibration l 1/1/82 l 1108 1 59% l OP-57, I l l l l l PT28.2 l l Flux Map - NI Calibration i 1/1/82 1, 1809 l 68% l OP-57, I I l l I l PT28.2 l l RCS Flow Measurement i 1/27/821 1301 1 100% 1 ST-52 l l l l 1 1 l l Flux Map - HTP, Eq. Xenon i 2/10/821 1340 l 100% l OP-57, 1 l l l l l PT28.2 l 1 1 I I l- 1 4
FIGURE 1.1
$URRY UNIT 2 - CYCLE 6 CL9E LOADING MAP R P N N L K J H G F E D C S A l 65 I8 1 68 l l W41 ! 2P6 I W11 1 1 1 1 l l l 7A l8 l8 l 78 l8 l8 l 7A l l IL2 l ISP7 I I6P1 1 4H1 l SP2 1 6P3 I OL6 l I 2 I I I I I l 7B l8 l8 l 78 1 78 l 78 l8 l8 l 78 l l 2N3 iI OPo lI 3P1 l I CH7 l XH5 l CH3 l 2P1 1 4P3 l CH4 1 I 3 I I I I I I l 75 l 78 l8 f.7B l8 1 7A l8 1 78 I8 1 7B l 78 I II 1H7 II IH2 1I 3P9 Il 1H3 Il SP9 Il OL9 l IPS l IN9 I IP3 l 2No l CH1 1 4 I I I I I I l 7A l8 l8 1 65 l8 1 7B l8 l 78 l8 l 6B l8 l8 l 7A 1 Il OLS Ii TF4 ll 2PS Il W22I l CP6i l CH2I l IP6 Il 1NO l 3P7 I H24 I OP3 l 4P6 l ILO l 5 I i I I i 18 l8 1 75 l8 l 6A l 78 l 68 1 78 8 6A l8 l 7B 1
l8 l8 I II SP0 lI SP8 1i 3H4 1l SPL Il V27 1I 4Ho'I l W40I 1 4H6 I Vol l IPO l 4H2 i OPS l 1P1 1 6 I I I I I I l 65 l8 1 75 l8 1 78 l 75 l 6A .J 8 l 6A l 78 1 78 I6 1 78 l8 l 68 l l W29 Il 5P5 1I 3HS I I 3P6 l1 3H1 ll LN6 il V13 l 14P4 l IV14 l 2H5 1 4H7 1 4P9 1 3N6 1 3P3 l W20 1 I 7 I I I I I I i 18 1 78 1 78 l 7A l8 l 68 l8 l 4A l8 l 68 l8 1 7A l 78 l 78 l8 l Il 6P6 1 I 4N9I l 3NSI l OL3I 1 3P5 I l 450I i SP4I l 319 I l 6P5 Il WOF l'4P8 l OLI l 2N6 1 2H7 I IP4 l 8
! 6S I I I i
!8 1 7B l8 l 78 l 78 l 6A i8 l 6A 1 78 I 7B 1 1 l8 I 78 l8 l 68 l
!l W32 lI SP6 Il 2N1 i1 0P7 l ! 2N9 I! !!!2 i iV15 l OP1 l I V11 l 2H2 l ONS l 3P8 l 4H4 1 3PO I WO4 1 9 i I I I I I I I l8 !8 1 75 l8 1 6A l 78 l 68 1 78 l 6A 18 l 78 l8 l8 l Il 4P5 1l 2P4 ii CH9I l 6P6 Il V25 I1 3H9I l W26l l SN1 l V09 l 6P2 l IH1 1 4P2 l IPT l 10 i I I I I i l 7A l8 I8 l 65 l8 i 7B I8 1 78 l8 1 68 I8 l8 1 7A I i!-111- li IPS l CP4 i l lW47 1i 4D1 1I 3H7 Il OP2 I l IN4 1 6P4 i W36 l 6PO i 2P2 l OL7 l 11 I I I I I I l I 75 I 7B l8 l 78 l8 l 7A I8 l 78 l 1 78 l8 l 78 l ll OH6 I l 4NOI l 2P9I l IN8 lI 2P3 lI OL8 l OP9 l 3H3 l 6P7 l SH0 I 3H2 l 12 l i I I I I l 78 l8 I8 1 75 l 78 1 78 l8 l 8' l 75 I I CHS Il 2P6 Il 2PO 1I 2H4 1 4M5 1 4H3 l SP3 l IP2 l 3HO l I 15 I I I I I I l 7A l8 l8 l 78 l8 l8 1 7A i II OL4 1I 4P0 I1 3P2 l 2NQ l 4P7 l 2P7 l OL2 1 14 I I I e i I 6a I8 16s i I l--> SATCH
- I l--> ASSEr2LY 10 l WOS* 1 1P9 l W4d i 15 l l l l l l l FUEL ASSEMBLY DESIGN PARAMETERS BATC14 4A5 6A2 6B2 7A o 73 8 Initial Enrichment (w/o'U235) 2.606 2.906 3.203 3.126 3.406 3.607 Burnup at BOC-6 (MWD /KIU) 11,129 12,651 20,856 16,851 15,252 0 Assembly Type 15X15 15X15 15X13 15X15 15X15 15X15 -
Number Os Assemblies 1 8 16 12 52 68 Fuel Rods Per Assembly 204 204 204 204 204 204 5
1 I
FIGURE 1.2 SURRY UNIT 2 - CYCLE 6 BEGDO4ING CF CYCLE FUEL ASSEr$LY BURNUPS R P N M L K J H 6 P E D C 8 A I H41 1 2P6 l W11 l l 177081 0 1 175921 1 I l I l l 1L2 i SP7 l 6P1 1 4H1 1 5P2 l 6P3 l OL6 l l 165911 0 1 0 1 148201 a 1 0 1 161751 2 I I I I I I I I I 2H3 I OPS l 3P1 l OH7 l IN5 l OH3 l 2P1 1 4P3 l ON4 I i 16730l 0 1 0 l 168691 148321 167201 0 1 0 l 166791 3 I I I I I l l l I l l 1H7 1 1H2 1 3P9 l 1H3 l SP9 l OL9 l 1P5 1 1H9 1 1P3 1 2NS l CH1 l l 166911 100891 0 l 145051 0 1 17649l 0 1 144821 0 1 104351 169731 4 I i 1 I I I I l l l l l l OL5 l 3P4 1 2P5 l W22 i OP6 l OH2 l IP6 l ING l 3P7 l W24 I QP3 l 4P6 l LLO l i 166081 0 1 0 1 249911 0 l 176951 0 1 176141 0 1 246971 0 1 0 1 164481 5 l I I I I I I I I I I I I l l 5PU l 5P8 l 3H4 l SP1 l V27 l 4N8 l W40 l 4N6 l V01 l IPO l 4H2 l OP5 l IP1 1 I O I O I 145801 0 1 127731 129901 23227l 136331 125711 0 l 147521 0 1 0 1 6 I I I l l i I l i I I I l 1 l W29 l 5P5 l 1NS 'l 3P6 1 3H1 1 1H6 l V13 1 4P4 i V14 l 2H5 1 4H7 I 4P9 1 3H6 l 3P3 l W20 l l 179144 0 l 169991 0 l 17594l 129861 124821 0 l 126231 129951 176171 0 1 170321 0 1 177091 7 I I I I I i I i i I I I I i l I I 6P6 l 4H9 l 3H8 l OL3 l 3P5 l W50 1 5P4 1 319 l 6P5 l WO7 l 4P8 l OL1 l 2H6 l 2H7 l IP4 l l 0 l 147501 149621 177551 0 1 233041 0 1 111291 0 1 233861 0 l 176501 149668 151901 0 l 8 I l I I i l I i i l I l- 1 I I 'l I W32 i SP6 1 2H1 1 OP7 l 2H9 l 5H2 l V15 l OP1 1 V11-~l 2H2 l ONS I 3PS l 4H4 1 3PO I WO4 I l 17483l 0 l 170031 0 1 174431 133471 125761 0 l 128711 129091 174351 0 l 169671 0 1 17697l 9 1 I I I I I I I I I I I I I I I I 4P5 1 2P4 l ON9 l 6P6 l V25 1 3H9 l W26 1 5N1 l V09 l 6P2 l IH1 1 4PZ l IP7 l 1 0 1 0 1 146091 0 1 124571 129201 233001 129641 128521 0 1 148641 0 1 0 1 10 l l I I I I I l I I I I I I I Ill l IPS I OP4 l W42 1 4P1 1 3H7 l OP2 1 1H4 1 6P4 l W36 l 6PO l 2P2 l OL7 l l 164991 0 1 0 l 247151 0 1 172691 O l 17614l 0 1 24579l 0 1 0 l 163551 11 1 I i 1 l l I I l I l 1 l l 1 ON6 1 4HO l 2P9 l 1HS l 2P3 l OLS I OP9 l 3H3 1 6P7 I SHO l 3H2 l l 168021 101241 0 1 147031 0 1 176351 0 1 146061 0 1 104061 166571 12 I I I I I I i 1 I I I I I ON8 l 2P6 l 2PO l 2H4 1 4HS l 4H3 l 5P3 l IP2 l 3HO l l 170031 0 1 0 l 169201 149541 169951 0 1 0 1 168361 13 I I l ! I I l I I l l OL4 1 4PO l 3P2 1 2HO I 4P7 1 2P7 l OL2 I i 164751 0 1 0 l 155841 0 1 0 1 163771 14 I I I I I I I I I WO5 l 1P9 i W48 I I l--> ASSEMBLY ID 1 176351 0 l 177531 15 I l- > ASSEMBLY BURNUP l l l l 1 - 1 e
9 4
6
s
- FIGURE 1.3 SURRY LHIT 2 - CYCLE 6 IHc0RE INSTRUMU4TATIcH LOCATIONS R P N n L K J H G F E o C 8 A I i i i i i no 1 Tc 1 1 1 I I I l l l 1 I i l I l l Tc I I Tc I m i I 2 1 1 I l ! I I I I m I i l i m I i l i no l I Tc l no l Tc I I Tc I I Tc I 3 I Tc I I I I l i I I I I I i l l I I i l 1 I I I I I m i I I m i I m 1 Tc I I i 4 I Tc I I I I I I I I I I I I I I I I I i 1 l l l 1 m I i m i I m i I m l Tc I tio i Tc I I Tc I re i Tc I I Tc I 5 I
I I I I I I I I I I I I I I I I I I m I i i i i i i i i i I Tc I I no 1 Tc Im i I I I l 6 i i Tc I I I I I I I I I I I I I I I I I I I I I I I I I 1. I I I I I I 7
I Tc I Tc I no l I l l No l I m i I Tc 1 m i I no 1 I I I I I I I I I I I I I .I l i I I I I m i I m i I I l l l 1 I m i I I I Tc I Tc I I Tc I Tc l te i Tc I I Tc I m l Tc I e I no l Tc I Tc I I I I
! I _I I I I I I I I I I I I l i I I I I I I I m I I I I I I I Tc I re i Tc I I I I I no I 9 I I I I Tc I m i I 1 I I I I l- 1 I I I _ ___ I _ l -I I I I I I te i I I I no I 1 : I I I I no i I l Tc ! l l l Tc l l l 1 Tc I m i I Tc I to I I I I I I I I I I I I
.I I I I I I I I I to i i no i I i i i i l i Tc I m i Tc I I Tc I I Tc I no l I I i 11 I I I I' I I I I I I I I I I I I l l l m I i l I i i m i I no I i Tc l l Tc l l l l Tc 1 tio l Tc 1 12 I I I I I I I I I I I I i 1 i l i m i I m i I l l I I a l Tc I I Tc I I I 13 I I I I I I I l i I l m l l l l l l l 14 l Tc I I I I m i I Tc I I I I I I I I I m - nova 8LE DETECTOR I l l l I m l Tc ! TC i 15 Tc - THERtioCOUPLE
- 1 1 I I G 8 9
e 4
9 5
7
FIGURE 1.4 SURRY UNIT 2 - CYCLE 6 8URHA8LE POI 5CH AND SOURCE A55Et2LY LCCATICHs R P N M L K J H G F E D C 8 A i l i l i i l i 1 I I I I l l l l 1 1 I I I I i 16 I i 16 I I I 2 I I I I I I I I I l l l 1 l I i l i I i 12 I to I l ss l I to i 12 1 1 3
, I l- 1 I I i l I I I i 1 I I I I i I i l i I I I i 16 l 1 to i I to i 1 16 I I I 4 l _ _._ . I I I l I I I I I I I e 1 I I I I I i 1 1 1 I I I i It ' l 16 I I to I i to 1 I to I i 16 1 12 I I 5 l 1 I I I I I I I i 1 1 I i i I l i I I I i l 1 I I I I I I to i I to l I 4 I I 4 I I to i I to i I 6 I I I I I I I I I I I I I I i i 1 1 1 1 I I I I I I I i 1 1 1 1 16 I I 20 l I 4 I I to 1 1 4 1 I to I i 16 I I 7 l' l I I I I I I l i I I l i I I I I I I I i i l I I I I i i i l I ss 1 I I I 20 l I to l l to l I to 1 I I I I a 1 -l l I I l i I I I I I I I l I I I l i I i .I l i I I I I I I I I i 16 I I to i I 4 1 I to i I 4 I I to 1 i 16 I I 9 I I I I I I I I I I I I I I I I I I i 1 1 I I I I I I I I I I I to i I to i I 4 I I 4 I I to i I to I I lo 1 I I I I I I I I I I I I I I i l l l l l 1 1 I l l I I I i 12 1 16 l I to i I 20 l 1 20 1 I 16 l 12 I i 11
, I I I I I I I I I I I I I I
. I I I I I I I I I I I I I l l 16 1 I to l I to I i 16 I I i 12 l I I I I I I I I I I l '
i I I l l I I l l I I I 12 I to 1 I ss i I to i 12 I i 13 I I I I I l i I I I I I I I I I I I I I i 16 I i 16 I I i 14 I I I I I I I I I i i I
) F;E5H SURHA8LE POISCH ROOS i I l l 15
- sEC0t!A%f SOURCE l l l l S
9 8
FIGLWE 1.5 SLTRT UtIIT 2 - CYCLE 6 CCNTROL RCD LCCATICNS R P N M L K J N G F E D C S A 180*
I LOOP C l l l l LCCP S 1 OUTLET l l l l INLET N-41 l
%l l l*l l l SA l l" ll SA ll*! l/l N-43 l l 3 I I I I I I I I I I I IC i Ie I l i Ia l lC l l 4 I I I I I I I I I I I I I I I se i l SP l l SP l l se 1 l i 1 5 l l l i I I I I I I I l l i IA l l8 l lD l lC l lD l l 5I lA l 6 LCoP C I I I I I I I I I l l l l l LOOP S INLET N
l l l SA l l SP l l 58 l l 58 l l SP l l SA l l l g CUTLET 7
. A! I I I I I I I I I I I I I i 1/
90 - l l0 l l l lC l l l lC l l l lD l l - 270, 8 I I I I I I I I I I I I I I I I I I I sA I I sP 1 i sa 1 i sa I l SP l 1 SA l i 1 9 l l I I l_1 I I I I I I I I I I IA I Ia 1. I OI IC l l0 1 I5 I IA l 10 I I I I I I I I I I I I I I I I I l sa l l SP l i SP l l SS I I I i 11 1 I I I I I I I I I I I I I i iC i 1a I I i Ia I iC i i 12 I I I I I I I I l i l l I I I I SA l l SA l l l l 13 H-44 l l l l l l l l l l N-42 I lA I IO 1 iA l i 14 I I I I I I I I
/ I l l l % 15 LCOP A l l l l LOOP A BSCRIE2 MATERIAL CUTLET INLET G-IN-CD l O'
FutCTION NUMBER OF CLUSTERS tITR!L BANK D 8 2NTROL bat 3 C 8 2NTROL bat 2 8 8 2HTROL BANK A 8 1UTCCWN BANK $8 8 4UTDCW4 BANK SA 8 8 (SPARE RCD LOCAlICNSI 8 9
l Scotion 2 CONTROL ROD DR0p TIME MEASUREMENTS The drop time of each control rod was measured at cold and at hot RCS conditions in order to confirm satisfactory operation and to verify thct the rod drop times were less than the maximum allowed by the Technical Specifications. The hot control rod drop time measurements woro run with the RCS at hot, full flow conditions ( 547 'F, 2235 psig) and are described below.
The rod drop time measurements were performed by first withdrawing o rod bank to its fully withdrawn position, and then removing the covchle gripper coil fuse and stationary gripper coil fuse for the test rod. This allows the rod to drop into the core as it would in a normal plant trip. The data recorded during this test are the stationary gripper coil voltage, the LVDT (Linear Variable Differential Trcnsformer) primary coil voltage and a 60Hz timing trace which are rocorded via a visicorder. The rod drop time to the dashpot entry and to the bottom of,the dashpot are determined from this data. Figure 2.1 provides an example of the data that is recorded during a rod drop time accourement.
As shown in rigure 2.1, the initiation of the rod drop is indicated by the decay of the stationary gripper coil voltage when the stationary coil fuse is removed. A voltage is then induced in the LVDT primary coil as the rod drops. The magnitudo of this voltage is a function of the rod velocity. When the rod enters the dashpot section of its guide 10
=. . _ ._ . . -
tuba, the velocity slows causing a voltage decrease in the LVDT coil.
Tho LVDT voltage then reaches a minimum as the rod reaches the bottom of tho dashpot. Subsequent variations in the trace are caused by the rod bouncing. This procedure was repeated for each control rod.
The measured drop , times for each control rod are recorded on rigure 2.2. The slowest, fastest, and average drop times are summari=ed in Tchle 2.1. Technical Specification 3.12.c.1 specifies a maximum rod drop time from loss of stationary gripper coil voltage to dashpot entry of 1.8 seconds with the RCS at hot, full flow conditions. All test results met this limit.
1 11 8 e e
I I
Table 2.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST
' HOT ROD DROP TIME
SUMMARY
! ROD DROP TIME TO DASHPOT ENTRY
)
i l SLOWEST ROD l FASTEST ROD l AVERAGE TIME l'
, l I l l I I I I l X-14, 1.27 sec. I C-9, 1.18 sec. I 1.22 sec. l I l l I I l l I
\
ROD DROP TIME TO BOTTOM OF DASHPOT i
, l. SLOWEST ROD l FASTEST ROD l AVERAGE TIME l I l l I l 1 1 I l
- I G-7, 1.93 sec. I J-9, 1.76 sec. I 1.26 sec. I I I I I I I I i
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FIGURE 2.2 SURRf UNIT 2 - CYCLE 6 80L FHYSICS TEST RCD OROP TIME - HOT FULL FLC'A CCH0!TICH3 R P H M L K J H G F E D C B A l I i l l I I I i l i I I l l 1.22 l l 1.22 l l 1.21 l l l l 1.82 l l 1.89 l l 1.a2 l l 2 l i I I I I l i I I I i 1.20 I i 1.20 1 1 1 I i l I i 1.e4 l l 1.a9 I I I I 3 I I I I I I I I I I l 1 1.2c 1 1 1.23 I I I i 1.2 3 I i 1.21 I I I i 1.81 I i 1.sa l I I i 1.87 I i 1.86 I I 4 I I I I I I I I I I I I I i l 1 1.21 1 1 1 1 1 1 1.21 I i 1 1 1 I I i 1.83 I i l i i i 1.se i l l I 5 I I I I I i _I I I I I I I i 1 1.22 1 1 1.19 I i 1.24 I i 1.23 I i 1.21 l l 1.22 I i 1.24 1 1 1.ao 1 i 1.7a 1 i 1.sa i 1 1.81 I i 1.85 I i 1.92 I i 1.91 1 6 l =l l I I I I I I I I I I I I l 1 1.24 I I I i 1.24 I i 1.26 I I I i 1.20 I I I i 1 1 1.89 I I I i 1.e4 I i 1.93 I I I i 1.90 l I I 7 I I l l I I I I I I I I I l -- 1 I I i 1.22 i i l i 1.19 I I l l 1.24 I I I i 1.25 I I I i 1.91 I I I i 1.8o l I I i 1.as ! I I i 1.91 1 I a l i I I I I I I I I I I I I I i 1 I i 1.20 1 1 1 1 1.21 I i 1.21 1 l l l 1.18 l l l l I 1 1.86 I I I i 1,76 I i 1.e3 I I I i 1.as I i I 9 1 I I I I I I I I I I l l I I I i 1.19 l 1 1.23 I i 1.23 I i 1.22 I i 1.24 I i 1.21 1 1 1.23 I i 1.as I i 1.sa l i 1.s7 I i 1.es I i 1.as I i 1.a7 l l 1.89 I to I I I I I i l I l i i i i I I i I i 1.22 I I I I I i 1.23 I I I I I I I i 1.90 l i I I I i 1.82 I I I i 11 1 I I I I I I I I I I I I I I i 1.20 l i 1.20 l l I i 1.24 I i 1.20 l i i I 1.as I i 1.e4 I I I i 1.a6 I i 1.as I i 12 I I I I I l i I I I -I _I
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( ,
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l c /
Section 3 - j'i
.. ~ f,
.1 REACTOR COOLANT SYSTEM FLOW MEASUREMEN.T '
+
The reactor coolant flow rate is measured in order to verify that tha minimum flow rate requirement is cat'isfied. The RCS flow rate is datormined using the calcrimetric measurement technique. precision colorimetric data (i.e.,) -feeduater temperature, feeduater flow, and stata pressure) are obtained in order to; accurately determine tpe
/
secondary-side heat rate. The primary-side anthalpy rise is determined from the RCS pressuto,and the temperature increase associated with each i
RCS loop. The flou for each RCS loop is determined by establishing a primary-side to secondary-side heat balance. Steam generator blowdoun hoot loss, system h.o r.t losses, and the power produced by the reactor taken' into account in the heat balance.
coolant pumps are A reactor e coolant flow measurer;2nt was performed at 100% pousr. This data was, analy=ed using the RXFLOW5 computer code. A. summary of the results for i
this test is given in Table 3.1. As shown by this table, the results domonstrated that the RCS flow limit was met. '
+
,4 I
J f
o
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- f
. /
15 a
./ ,
o
__ _ _ - I
Table 3.1 SURRY Z - CYCLE 6 BOL PHYSICS TEST REACTOR COOLANT SYSTEM FLOW MEASUREMENT
SUMMARY
r
)
e I percent l ' Loop A l Loop B l Loop C ITotal Flou l Minimum Floul I power JTlou (gpm)lPlou (gpm)lFlou (gpm)l (gpm) l Limit * (gpm)l i I I I I I I +
1 1 1 I I I I -
l 100 % l 102,341 1 99,599 l 103,628 1 305,568 1 265,500 1 I I I I I I I
- FSAR Section 4.1.3; Letter from J.'H. Ferguson (Vepco) to H. R. Denton (NRC) dated April 28, 1981 (Serial No. 232);
Letter from C. M. Stallings (Vepco) to E. G. Case (HRC) dated Movember 16, 1977 (Serial No. 516),
e r
/
16 mm-w.
4 Section 4 CONTROL ROD BANK WORTH MEASUREMENTS Control rod bank uorth measurements were obtained for all control and shutdown banks using the rod swap technique. The first step in the rod suap procedure was to dilute the most reactive control rod bank (hereafter referred to as the reference bank) into the core and measure its reactivity worth using conventional test techniques. The reactivity
' changes resulting from the reference bank movements were recorded continuously by the reactivity computer' and were used to determine the differential and integral worth of tlm raference bank (Control Bank B).
At the completion of the reference bank reactivity worth measurement, the reactor coolant system temperature and boron concentration were stabilired such that the reactor was critical with the reference bank near full insertion. Initial statepoint data for the rod swap maneuver were obtained by moving the reference bank to its fully inserted position and recording the core reactivity and moderator temperature. At this point, a rod suap- maneuver uns performed by withdrawing the reference bank while one of the other control rod banks (i.e., a test bank) was- inserted. The core was kept nominally critical throughout this rod swap and the maneuver uns continued until the test bank was fully inserted and the reference bank was at the position at which the core was just cr.tical. This reasured critical position (MCp) of the referenca bank with the test bank fully inserted is the major parameter of interest and was used to determine the integral reactivity worth of the test bank. Statepoint data (core reactivity, moderator temperature, 17
and the differential worth of the reference bank) were recorded with the i l
reforence bank at the MCP. The rod swap maneuver uns then performed in roverse order such that the reference bank once again was near full insertion and the test bank uns once again fully withdrawn from the l coro. The rod swap process was then repeated for all of the other control rod banks (control and shutdown).
A summary of the results for these tests is given in Table 4.1. As chaun by this table and the Startup physics Tests Results and Evaluation Shsots given in the Appendix, the individual measured bank worths for all of the control and shutdown banks were within the design tolerance (210% for the reference bank and 115?. for the test banks). The sum of ths individual rod bank worths was measured to be within 0.3% of the design prediction. This is well within the design tolerance of !10% for the sum of the individual control rod bank uorths.
The integral and differential reactivity worths of the reference bank (Control Bank B) are shown in Figures 4.1 and 4.2, respectively.
Tha design predictions and the measured data are plotted together in ordor to illustrate their agreement. In summary, all measured rod worth values were satisfactory.
18
P Table 4.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST CONTROL ROD BANK WORTH
SUMMARY
l l MEASURED l PREDICTED l PERCENT DIFFERENCE l l 1 WORTH l WORTH l l l BANK l (PCM) 1 (PCM) l (M-P)/P X 100 l i I I l l l B-Reference Bank l 1371 l 1355 l + 1.2 l l D 1 1115 l 1156 l - 3.5 1
,1 C l 793 1 836 1 - 5.1 l l A l 595 l 562 l + 5.9 l l SB l 848 1 906 l - 6.4 l l SA i 1134 l 1057 i + 7.3 I i Total North l 5856 1 5872 l - 0.3 l l l l l l i
9 4 9 19
l l
l l
l l
l FIGURE 4.1 1 1
SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST BANK B INTEGRAL ROD WORTH - HZP S BANK WITH ALL OTHER RCOS OUT PREDICTED M t1EASURED O
O .
' t . 1 . 1 i i e i 09 i 1 e { . i 8 i i e 6 . i i i e i I e
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v O 40 80 120 160 200 228 BANK B POSITION (STEPS) 20 I t
FIGURE 4.2 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST BANK B DIFFERENTIAL R00 WORTH - HZP 5 BANK WITH ALL OTHER R005 0U'
-- PREDICTED M ttERSURED C
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120 160 200 228 0 40 80 BANK B POSITION (STEP) 21
Section 5 BOROM ENDPOINT AND WORTH MEASUREMENTS Boron Endpoint With the reactor critical at hot =ero power, reactor coolant system boron concentrations were measured at selected rod bank configurations to enable a direct comparison of measured boron endpoints with design Prodictions. For each measurement, the RCS conditions were stabili=ed with the control banks at or very near a selected endpoint position. The critical boron concentration was then measured. If necessary, an adjustment to the measured critical boron concentration was made to secount for off-nominal core conditions, i.e., for rod position and noderator temperature.
The results of these measurements are given in Table 5.1. As shown, in this table and in the Startup physics Test Results and Evaluation Shoots given in the Appendix, all measured critical boron endpoint values were within their respective design tolerances. All measured values met the accident analysis acceptance criterion. In summary, a l.'.
results usare satisfactory.
l l
Boron Worth Coefficient The measured boron endpoint values provide stable statepoint data from which the boron worth coefficient was determined. A plot of the boron concentration as a function of integrated reactivity can be constructed by relai.ng each endpoint' concentration to the integrated 22
h l
rod worth present in the core at the time of the endpoint measurement.
Tha value of the boron coefficient, over the range of boron endpoint concentrations, is obtained directly from this plot.
The boron worth plot is shown in rigure 5.1. As indicated in this figure and in the Appendix, the boron worth coefficient of reactivity ums measured to be -7.63 pcm/ ppm. The. measured boron worth coefficient is within 7.2% of the predicted value oh-8.44 pcm/ ppm and is well within the design tolerance of 210%. The measurement result also met ths accident analysis acceptance criterion. In summary, this result was satisfactory.
23
4 I
Table 5.1 )
SURRY UNIT 2 - CYCLE S BOL PHYSICS TEST BORON EMDPOINTS
SUMMARY
l l Measured l Predicted i Difference l I control Rod l Endpoint i Endpoint l M-P l l Configuration 1 (ppm) l (ppm) l (ppm) l I I I l i I I I I i l ARO l 1452 l 1445 l 7 l l l l 1 I l B Bank In l 1277 l 1293
- l -16 l l l l l l
- Tho predicted endpoint for the B Bank in configuration has been adjusted for the difference between the measured and predicted values of the endpoint taken at the ARO configuration as shown in the boron endpoint Startup Physics Test Results and Evaluation Sheets in the Appondix.
l
{
24 6
FIGURE 5.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST BORON WORTH COEFFICIENT C ENDMINI MERSUREMENTS 2400 2000 h ___
N
_g_ _ _ _ _
x 3 __ _
1600 \ UC B
\
E N
~
g -
y H
\ __
1200 s- --
E _ \ .I' xq _ _ _ _ _ _
s ___
I 8 __ __
_A_ _ _ __ _ _ _ _ _.. g _ __
w g 800 x g __ _ _ _ _ _ _. _ _ _ _ -_ _
h - - -
400 -
N q _ _ _ _ _ ._
x_ __ ._._ _ _ _ _ __
__ _ _ __ _. _ h _ _ _ _ _
0 0
- 200 1240 1280 1320 1360 1400 1440 1480 1520 BORON CONCENTRATION (PPN)
l l
Ocction 6 TEMPERATURE COEFFICIENT MEASUREMENTS l The isothermal temperature coefficient measurements were accomplished by controlling the RCS heat gains / losses with the steam dump valves to the condenser, and/or steam generator blowdown, catablishing a constant and uniform heatup/cooldoun rate, and then monitoring .the resulting reactivity changes on the reactivity computer.
Those measurements were performed at very low power levels in order to minimi=e the effects of non-uniform nuclear heating, thus, the moderator end fuel were approximately at the same temperature (between 542-547 'F) du'ing r these measurements. To eliminate the boron reactivity effect of outflow from the pressurl=er, the pressuri=er level was maintained constant or slightly increasing during these measurements.
Isothermal temperature coefficient measurements were performed at various control rod configurations. For each rod configuration, rocctivity measurements were taken during both RCS heatup and cooldoun ramps during which the RCS temperature varied approximately 3'F.
Racctivity was determined using the reactivity computer and was plotted cgoinst the RCS temperature on an x-y recorder. The temperature coefficient was then determined from the slope of the plotted lines. The x-y recorder plots of reactivity changes versus RCS temperature for each accourement are shown in Figures 6.1 and 6.2.
The predicted and measured iso'hermal t ' temperature coefficient values are compared in Table 6.1. As can be seen from this summary and from the Startup physics Test Results and Evaluation Sheets given in the 26
> s.A - - a-L-- - - G .a 4 - -& ----s -- ---*+2 KA-= -J-I I
l Appondix, all measured isothermal temperature coefficient values were j uithin the design tolerance of 23 pcm/'r and met the accident analysis l
cccaptance criterion'. In summary, all measured results were catisfactory.
I 4 9 27
m Table 6.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT
SUMMARY
I BANK l l IIS0 THERMAL TEMPERATURE COEFFICIENTl IPOSITION l l I (PCM/*F) l l (steps) lTEMPERATUREl BORON I l l l RANGE lCONCENTRATI0HI l COOL l l l DIFFER. 1 IB I D l ('F) I (PPM) IHEATUPl DOWN LAVER.lPRED.I (M-P) l i I I I I I I I I I I I I I I I I I I i 1228 1228 I 542 - 546 l 1445 l-3.77 l-3.03 1-3.401-4.421 +1.02 l l l l l l l 1 l I l 1 21 1228 1 542 - 547 l 1286 l-6.24 l-6.36 l-6.301-6.781 +0.48 1 4
I I I I I I I I I I I
. 28
~.
/
Tigure 6.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, ARO Illi !!'! llll Ill! l {! lllIt! IIpi til nt' n:j
' }:::::l: ::h:"
!!: .' :H- lit: pj ljh liit du lih Ilt !.!: lin ..: ni llll .o riu to.
h ...
nr*- -
-C
n._1 ll . *llll l.ll.
. "- fr-
- l'."p'. :. !., !.n.,. .!j.,a t.!,!i ijk.. !!l!. !.!h.. ll1 llp. 'I.~j[. 7**l*'
=.. :p. :. j:.:.i l
.n. . .
- ,:. :pj
- n. :::: n:: tju pp! rn. ep: s. -
in:- .:.:n .:.:::... .
=
=. ....
nn t= :n: tu: .r utu l. lrn n: tn ln ptn!p: .n l!"!! .p:n . :: nu t. o n: t a- .t. .
n rn =_. ..' .... .....
,f.II[L 6 'it [fhv.... m..a t 4**
=_. . I . =._.I =. .
II{
=. l_. = . . ::..~.. . . P -n._. ... bi .." .:.n. -:;*.
. 1. *. !...
- t.;..:.9!.!!: t. . .w !... !!
[2.g.i, . .tn .._-l._. .1 . . . ...
m n::n r ... _ __:~ : uw nu t= nu an:- u.pn pie nt nr:m tur e :- n==.+05)== a-- =::f== :=t:n :nn = p! = unrau tm an: ttmt!p!;tpn: 1.1: . . 1 .
t a= :rg"!a!n :.:t pp lip: :ptu tu :l!.3.#oqj;.I u -
nn '
p_.
.= I n t
- \ :i:- - -: n r;=- =".u: n.r in: .t. . . ln: t . nm i "fil;i nultril ..
. . ..r '... . . h. h.j.i. .,ij,i IM, Li l.t ljll l[.[. :6 i ,;l. nkli...j.pr
-l:
- h. : ..~ n. . v.
,,!:... .:' :!.. .. ::.n. . .n.6:11, . r. n . 3 .
[ ,ll..i
,c , . e i.
ll{r.ll......nt lF "r. .:.' :: :
- !!!! ii !!!! !!!! !!ii lii dl !!ii liil llll IfllWI IMllli llll !!i! %
.nr" n.;. . .
4
.!.f.i! ....
ljk.. lll.,,,ln. .a'y -i . .l H. ..ll,
...n g;:. p. i u. n.wl0 t
. i t.h 6
1l.; llll llll II.;[
i j, h. [jp..
e.g "! l Ip:
i . .
,i : ..... . . . . .
r 9 e i :'h ;-
- I@U 4: l:l.ll-lh! "li'l].l1:n ;;p e.ngt : : t.e
- !;; q. 'i!
p="
. .::l::: :
- r I'lh: : "1"!! t "! Hel!Il lj"D [.ln 1 u , ,,
.;g1,. : .iinlu. . n..:.
... .., ..g. ;
i ., --!-! a I .l "ie . h. iI t i . } "h i p i. r.
- r.! h:n ...::-
..: ...! .m. . n. i. !! .I .
- i. . .. =.
. .nr.. l. u. . .. . . ( ..-
=
.p.
... . . . . n, n . .. It..l. i. h..lh.,i;.rl.I,i
. i.l.. ,o.. h. ,i. h. . ,u. . ;. .i. t:.t ;1.ll.
t ll, l r. :x .;!.. ..
=. .=_..Lu n =. .. .r. ... h. : . .~. . . h. . .
- : . l. u,.t.u..
- . _m... s. .. . :.l...u. u.. .. . . . .
= t 1. . . . . .' ' ;. , pn ::.: L- ;r.n!'=;*;; j. !Tuj'- iy !
Q l=
== = = .i.= i =.;. H ]::.:{=:\: = = = . n- u n Tr[a.m::].: tm !!:nl fn. :In:! Ulill..;Iy!nf:uu i. N:
o
= :n i: rn nn un -: h Im
.- :.c tit:- t= tm Rh [et tt: puInu. m t:n
- :w\h:gru w =:l$.==s=n=
n = _=-: =
=ut= :m)
- n. : = n == n l=:
_ = nit.
rn
. . . .. N. . 14.- .p..t.pyTT- ,_ 4.p,. ,
,... , 4 a.
M . .
- ;lc.
.1@1L. . tp.. .H.
g g . . ;.- = = q. =... =. 1. .=._nn.. _ .... _ . ..nu m.:. :ll.e. %m.. .
E.. \.+,4t q'.1 I. l f.. . . .
.I.:-
g; - g.
<: .. . p.t .
M' r** "r:['l!: '1 ,'rr-
,t t.t
. ~ . . ~ . . . .-
M a.: = . . =.=...t.=
. .. . =. =._ .:n :. :;n. "I;.n.. :::.:.h.1i: I:..
. . . ~ ~ .~ . o.
t ..n. t.. ...
., :.t. } [,...... f"t;
- n. . . 1 ]. .!: .itn. ll a .
un itn ,t pi:t rI p t
.II- lp11 pt.lhyp! tjp up nr = u.: n- n r g; =.:jr: - =.-
-n = -tm= =an t. h":h h' :m tr :i t. .,'F.h! :m
.. .t w n= . . .
a ....: un= .:.. = .= .
.:.: ini n :n :;n nn :n M:n mi IPl 'rli .l 'M!!! Unpi n..... ptp: !!
-= . n p -: :- :. := f=:ni I:r uf. 1:p: n t.!: It t: !!! . 31.: n !tt. L.1 .
- J .C.n: ~! .;:n 40 W;L blu 4; 4 n 12.c ;" :Mtj
.=--*
li.:.n = nr= nu un m: w: .imt'u=m .:M er un[= di! m. j L=_=_.-{.
g.
.=
.= -.!.n m.._.4..: :::t=.~
_=
=:g ==
.._+
t.:n. . .t =n. ..m m.
- 4. p
.'n. .:..n. .. r l.'n..:....
p:i I,t:.. i . ,
.g g , . . . .
t t.t n. .;.:.a. .
- . t
- g. gta.g,t.4 i. . *.
.,g.
7 ". . g.".. rI. n.. ..g..
. . n. . ! ! I;.
l un -an p- tr;ol:: h: np: nn :s!:n im :ntilh pu! lIl lhn: nh n ln t ..n. n ... :f n a t. n.
. n: :le . ~n- en t:n tr rnl:- ::
+lll. .!..
;.1.jl.
I'll .!.t U. i .. ! .@.n.II:!,114.
- u. .r . . .:t8...
.u
; t. . n. n..I:.I 4
. , I. n.. . u.
u '. i : : ..ll "I : ! :.l... 1. . . !.t.
"t t
' r. ...r n. . =. . . .d.
1 . q ... . si ip Philitil:Elli iiniOiiilisi lii1Ru.iiHlHH :llii J;u 4 nl;;n [;gljg .jjg[gg[.j m ... ... . [j[g g!.j.
. . . o.,
,;j j;.
tpi .:nr tr;jn:'jj! p" h b M b !- - gum j"j "Ulll:! h IU fM 1M' +
-,n l":
VERTICAL SCALE 1 F/ inch u p- ;u:n tgj ..pt.i ' . - tn 11: llp en.t tht
. u :t.. !; ' litt hH 1.h'[oit. : p!-
-u r p HORIZONTAL SCALE 10.0 pcm/ inch ntn. n ny:':tl ttr
!.p! :pi;.. up!
. :U.
. .ll{l ((,n: l..n p. {:dm..;:
.~ m - - -'
. . . _ _ . - . . ._ a -
REACTIVITY'(PCM) 29
l l Figure 6.2 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, B-BANK IM
. . . .,g, 6.. ..., ... ., ......... . . . . .
. ,,, g*.
1p.
.i
... g .. .n. n.: =
- - . . .... . ... . , .g g p i. : o r.s u .... u. n.u. . n. . .i.. .n.=.. :. =. . -
- r. .n
.=. n.r n u.: t =.. I..., Im.i n 1.. nr u...::.*r .1.I r.h+ .; .l...,:.e:n i .n- 1i. t. rl.
2 ..
= . .t. .=. .l....
n; "lp: "n ;.tn c: un - n ... t= .,= In=- .unja
=nn . = * = - ==nn :n: :;;u pn :;} abr. lry : ..ne .= = r= n 2 ._
- i. itu ..rnu e!I;.p!m r h.n ..k. =n n:=r :h= : = nnInu :::m un an .m . . . . - t ,
..:au
- r .nj=;=njn:
=:=.== r = a n: ,hp: t ie:
lj.l gIll- gI;rb;"." g, w~ ?h- pin. q.: :. :i::: .:u
.n: ~;n
= nr r- nn = :n: h:n"i!h: ul - un n .gt. li <;.pt;Ii!l-!
- t. .l. .:![l r =
=:=
n :.:n :;, g r. .. :, un
~
r- :u :-- :n t: unl=:tn nu p::n y,4. ..h N: ipt
.M,:;:. :.x :.n finn jj!.;. ..
r t
- apt. ifh: t[!i in:
i. m i:ln::{un nn n-
.: un -
={=
un un =t=cnten"nin
!!!I I!!!!!!! li!!Tl! r!*l !! E ik !!!!!!
"i:
.!liElliiiN!R E! Ei filii!!!. ini 'li!! l!!! I!!l l!!:[!!! lii!!!N! ill!lIIi! IIif .:. n
- j:-
- .: .N
- y nn :
.:.. n un nn inu n;jini;;-
rn hn: nu un ni n! .b n n nc :,.- '::t hn 4i . lrlt enj i ien il n
- r njj Itjh. l"injji.! n: un n
;*w:;::jn: ne. ,. -
- ln
= p:-
u- r= :n; un :ci ;: p:n ;:n [n: n:: ui: Hh; un "i;; lly n.li jip: nr :.. ..:j:...
- u. ::p. .n Ml:.:
in
....-- = .:n r. un. .;p: ..; n: ":a ut h. un er n- uh .!.h nn .m on .. 1 nh l.:
W- #- .t u-un-- =-- - :n- *t =. rL--
. . :::: nt .1' :.s : tr . t=. n. .:. -' a- =--
b-;-: e.. n_u.-- un- _ d.. ..e.._ g e..:. ....n. . u. . . . . . . . _=. .tuu.
. ...=.
n..P. ..: =..t. ru".. .n. .ra . . . . .. ... . .-. -.. . =- =". 9=-
...ie. . . ...
+- ;n =
....sv r .an +a: ;nuut.ut nl.!. u iu =N: r:. n p: ,:lnn,g==
;tr P :t:1 - :l.... -. t li,b Uh- r'h. :i n, .: ati l;.p: hy; .~il;: f 1.n :re =r =l=:r m ==lnw :-
- u- -
- .= . ..
.in - n w
a: n nin=a =nul== ..=: nn .+I:
= r +1 m :=:nn ::- ur .n .. : .lJ;:n Ig4[r L}pa rR"h:I:nh:5: nu n u.:y: yplnc
- ~ n ru : nF n:I;hnu h gI:
t~r :Lu nu r a an = unkn. :. Ea. . = t u-
.p= unt=
pjj uni;. rp; 1.,; i :rp inF(in is(i.n
$ n g i.i.ji.E. ii.i_i]~i.i..i.:. . .i.fi.h. D. i. li.F a .ri rt i"F: 'h i M.1,1iu: m lhri 0[i itli 3litej"l;. i Ifi.7 ;J;;.. Jhi. .... .t. . .
=
' l"l .j-li.1 j"il pn : i. . . i. i.ji.a t ::!;.i. !!!.7;r, im o t ll tjg .;.Il g}l tt jj'I jj I!jh4! i.
- ljlr li y i.t...
t ia-
..-. 1.!.!!..Pi.
. t. t.l .'ii 9. 6,. n. .g iii ljjI gn I .l i.i.ri. .
- nl: M Kn[...
....t:. :
- p: .:n: nn ;j"I .. k'ip::h'uj ptj t ... n.:gn::
n'= =l= .= .nt M:nl[g';
.:h r - ::n1:r" =,:- .= -~l;.:
E u. ;.n.:::: ::*:t.I .2nnirut n: Ipti a:tu[.p'. .
- t. .n. : ntC:!! n= .: G. =
5-a a . .- ,... ... I %.
- ,}O ' U. ..g! plt.t,1$.b.
l N. ..!t' 'tf la.:!. L. t,fi.: . ,. n. M.
- k. :,.l,..l ,
n.. n..
. fn. . .*. =-. . .. . n. !.
. . ....f. ..
. . . . .. . . . . ._tf. *. :. :.. .
. :n. .t ' l. l. t . !.
. ..I. .:11 'In.O.. . .3...
1 1.!l. t.i"t. . t.11[.I. 1 Y.t[n1 .
$!fbE! EE 5!I!! .I ![f! !!hl}[! !!f! $f {lkhlll} [fll l ll[f ll[l I!Nih ((N $! !i[! h I!i! If!!' !!!! IN! lNI '!!!.
- iiM a : - i! !!! !!iHW !!!!IN! W! !!!! !)H lil! !ill l!!! liii Uli iU!!!iNm !i!! Hij lili !!!!!!; !!!!:!: :: i u au .:.. [;;..
n= nin-m n-.:n :=
.:- :. :. ;nn
- r:. . .,.
t.. ut:iiT:}sl;n;l;:n
, h : n .? ! g.i! ttn q1: ." in:
t; ..:t I:t:g1.2 ru t
- sp ntrgtgrg ir :
;5' ilb re; . =t:..d t t ;
- *"*.--n.:[:... - te" -'~~* -
i:; * -~ i tpH" ; t~ {=. nn n-- =t= HH "lh;t till;t n :n::*h: hn t-:h': I M: (.t~:H 'r}"H 1o F/tnch u"t:m =f ,t :
"- A e VERTICAL SCALE n?=
=*n:.
..l= =.~} ':-- == in nr! hn i
r: [!!'ll[.i!! h"h%nr!
. N
;t h-((;:; lif:t I"~1Nt h{p::a 10.O pcm/ inch
.}bb 3Ii5I !55I!ili !!!i li!! lf!!IiN! !!!! I.
~
1 {.1]j [{}} (((( ij(( j@} HORIZONTAL SCALE
- ... . :::... :a. in ...: .:n. ?nlll"!j :in tj: 4;{j n j.g;1:["ll g. . _
- t.: . .l"la tr; ::t:: In. .! . l. _ . . _ .
1;.n.,;; 7nt:;.!,lin: :". Itn .. . _ _ _ . . REACTIVITY (PCM) b 30
l - l Soction 7 POWER DISTRIBUTION MEASUREMENTS
~
The core power distributions were measured using the incore movable datoctor flux mapping system. This system consists of five fission detsetors uhich traverse fuel assembly instrumentation thimbles in 50 core locations (see Figure 1.3). For each traverse, the detector output ic continuously monitored on a strip chart recorder. The output is also scanned for 61 discrete axial points by the PRODAC p-250 process conputer. Full core, three-dimensional power distributions are then datormined by analy=ing' this data using the- Westinghouse computer program, INCOREF.
- INCORE couples the measured flux map data uith predetermined analytic power-to-flux ratios in order to determine the pousr distribution for the whole core.
A list of all the flux maps taken during the test program together With a list of the measured values of the important power distribution parameters is given in Table 7.1. T1.e measured power distribution paremeter values are compared with their Technical' Specifications limits in Table 7.2. Flux Maps 1 and 2 were taken at zero power. These flux maps serve as the base case design checks. Figures 7.1 and 7.2 show the resulting radial power distributions associated with these flux maps. , Those maps indicated the presence of some assemblyuise relative power vclues in excess of the design tolerance, but all measured hot channel
. factor values were within the Technical Specifications limits. Flux Maps ,
I 3 through 5 and Map 7 were taken over a wide rangc of power levels and control rod configurations. These flux maps were taken to check the 31
l - l l ot-power design predictions and to measure core power distributions at various operating conditions. Maps 3 through 5 also provide incore/excore calibration data for the nuclear instrumentation system. The radial power' distributions for these maps are given in Figures 7.3 through 7.6. These figures show that the measured relative assembly pouar values are generally within 5% of the predicted values. In conclusion, all power distribution measurement results were considered to be acceptable with respect to the design tolerances, the occident analysis acceptance critaria, and the Technical Specification limits. It is therefore anticipated that the core will continue to op3 rate safely throughout cycle 6. t 32
TABLE 7.1
' SURRY UNIT 2 - CYCLE 6 80L PHYSICS TESTS IHCORE FLUX NAP SutR1ARY I I i i i l i 1 1 2 I I I I I I I I I I Buntal l I F-QtT) HOT l F-DH(H) HOT l CDRE F(Z) l l 4l 1 l l l l 1 UP l IBANK l CHAHHEL FACTOR I CHHL.F ACTOR l NAX l 31 QPTR I AXIAll NO.I l NAP INAPI DATE I NHD/IPWRl D l l l IFtXYll 1 0FF l 0F l l DESCRIPTIDH lHO I l NTU 18%)lSTEPSI l lAXIAll l l l lAXIAll I HAX l l l SET ITHINl ' l l l 1 l l ASSYlPIHlr0114Tl F-9t Til ASSYlPINIF-OH HilPOINTl F(Zll i NAX ILOCl IX) IBLESS I l_l_ ; l_ i __I_____.I 1.__ I I l _ _ '_ _ t i I I I l _I l_1 i l i l i i i i l i I I I I I I I I I I I lARO l 1112-30-811 01 01 223 1 0071 GHI 20 l 2.260 1 0071 GHI 1.488 l 21 11.476l1.42511.e'.71 14El 24.831 47 l l l l l l l l l I I I I I I I I I i 1 1 I IB AT 23' 1 2112-30-811 01 11 228 i K0*l DNl 14 l 2.641 l K091 DNl 1.799 l 20 11.39211.71011.0251 NEl 19.211 44 l l I i i i l l l 1 1 I I i l i I I I I I I II/E CAL. I 3i 1- 1-821 101 471 184 l 8061 del 32 1 1.982 l K141 KLI 1.446 1 32 11.305l1.40411.005l HEl -0.541 48 i .
1 I I I I I I I I I I l l 1 1 I i ! ! I I II/E CAL. I 41 1- 1-821 171591 180 l 8101 DKl 33 l 1.962 l 806l del 1.426 1 33 11.306l1.38311.004l SWI -6.001 48 l l l 1 i i i l l I I I I I I I I I I I I I II/E CAL. I 51 1- 1-821 221 681 204 l K141 KLI 22 l 1.853 1 0071 GHI 1.422 l 23 11.25511.37311.005l SW1 5.941 48 I . I 51 l i I I I I I I I I I I i 1 1 I i l l lHFP, EQ. XENOH I 71 2-10-821 111611001 228 i F041 FLI 33 l 1.749 1 0071 GHi 1.387 1 34 11.21411.33811.004l SW1 -2.191 47 l HOTES3 HOT SPOT LOCATI0tl5 ARE SPECIFIED BY GIVING ASSET 1BLY LOCATIONS (E.G. H-8 IS THE CENTER-OF-CORE ASSET 1BLYl. LJ FOLLOWED BY THE PIH LOCATICH (DEtt0TED BY THE "Y" C00RDIllATE WITH THE FIFTEEN ROWS OF FUEL RODS = LETTERED A THROUGH R AND THE "X" C00RDIllATE DESIGttATED IH A SINILAR NAIR4ER). Ill THE "Z" DIRECTIOP4 THE CORE IS DIVIDED INTO 61 AXIAL POINTS STARTING FR0tt THE TOP OF THE CORE.
- 1. F-QtT) INCLUDES A TOTAL UNCERTAINTY OF 1.08
- 2. F-DiHHI ItiCLUDES A NEASUREt1ENT LR4 CERTAINTY OF 1.04
- 3. FIXY1 IS EVALUATED AT THE NIDPLAt4E OF THE CORE
- 4. QPTR - QUADRANT POWER TILT RATIO.
- 5. FLUX t1AP S2-6-6 WAS TAKEN OH JANUARY 24. 1982 AT 99X POWER. THIS FLUX NAP WAS NOT TAKEH AT EQUILIBRIUtl Cot 40ITI0tl5 BUT WAS HEEDED FOR POWER SHAPE VERIFICATI0tl. ALTHOUGH THIS NAP WAS NOT PART OF THE FORT 1AL PHYSICS TESTING PROGRAN. IT PROVIDED VERIFICATI0H OF ACCEPTABLE POWER SHAPE AllD PEAKING FACTORS.
r
(..............,....- .. . Table 7.2 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TESTS COMPARISION OF MEASURED POWER DISTRIBUTION PARAMETERS WITH THEIR TECHNICAL SPECIFICATION LIMITS I I I I l l F-S(T) HOT I F-DH(N) HOT l l l CHANNEL FACTOR 1 l CHANNEL FACTOR 2 l lMAPI l l IMO.I MEASI LIMITlMARGINl MEASl LIMITlMARGINI I I I I (%) i I I (%) l I I I I I I I I l 3 l 1.981 4.36 1 54.6 l 1.451 1.71 1 15.2 l l 4 1 1.961 3.70 1 47.0 I 1.431 1.68 l 14.9 l l 5 l 1.851 3.13 1 40.9 l 1.421 1.65 l 13.9 l l 7 1 1.751 2.18 l 19.7 l 1.391 1.55 1 10.3 I I I I I I I I i 1 Tha technical specification limit for the heat flux hot channel factor, F-2(T) is a function of core height. The value for F-SCT) listed above is the maximum value of F-9(T) in the core. The technical spacification limit listed above is evaluated at the plane of maximum F-2(T). The minimum margin values listed above are the minimum parcent difference between the measured values of F-9(T) and the technical specifications limit for each map. All measured F-S(T) hot channel factors include 8% total uncertainty. 2 Tha measured values for the enthalpy rise hot channel factor, F-dH(N) include 4% measurement uncertainty. 34
1 Figure 7.1 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST ASSEBLYWISE POWER DISTRIBUTION HZP, ARO O N K J. H G F E D C 0 A P M L
................ F2EDICTED .
. 61rIDICits .
. 0.39 . 0.70 . 8.19 .
. 0.39 . 0.70 . 0.39 . . PIA $UE!D . 1 j
. P!A5up[0 .
)
0.9 0.9 . 1.4 .FCT 01FFEEf f.1't. -
. PCT 01FFla mCE. .
l
. 0.42 . 0.95 . 0.97 . 1.01 . 0.97 , 0.95 . 0.42 .
. 0.43 . 0.97 . 0.99 1.03 , 0.99 . 0.97 . 0.43 . t 1.7 . 2.6 . 1.6 . 1.2 . 1.4 . 2.3 . 3.6 , - -
. 0.46 . 0.96 . 1.12 . 1.10 . 1.21 . 1.10 . 1.12 . 0.96 , 0.46 .
0.47 . 0.97 . 1.14 , 1.21 . 1.23 . 1.21 . 1.19 1.00 . 0.49 . 3
. 1.5 . 0.9 . 1.6 . 2.6 . 1.5 . t.4 . 3.2 . 4.2 . 5.6 .
0.46 . 0.91 . 1.14 . 1.24 . 1.24 . 1.16 . 1.24 1.24 . 1.14 . 0.91 0.66 . 4 0.47 . 0.91 . 1.14 . 1.25 . 1.26 . 1.20 1.20 . 1.29 , 1.14 . 0.94 . 0.49
. 0.6 . 0. 7 . 0.3 . 0.4 . 1.4 . 1.9 . 3.7 . 4.0 . 3.7 . 3.6 . 5.5 .
0.42 . 0.96 . 1.14 . 0.97 . 1.20 . 1.22 . 1.21 1.22 . 1.20 . 0.97 1.14 , 0.96 0.42 .
. 0.42 , 0.96 . 1.14 0.90 . 1.19 1.20 . 1.21 1.23 . 1.22 . 1.00 . 1.16 . 1.01 . 0.46 . 5 0.0 . 0.5 . -0.5 . -1.3 . 0.0 . 0.0 . 1.7 . 2.4 . 2.1 . 5.4 9.0 .
. 0.1 . -0.1 .
0.95 . 1.11 . 1.24 . 1.20 . 1.16 . 1.20 . 1.02 . 1.20 . 1.16 . 1.20 . 1.24 . 1.12 0.95 . 6
. 0.95 . 1.13 . 1.24 . 1.10 . 1.13 . 1.14 . 0.90 . 1.14 . 1.13 . 1.21 . 1.28 . 1.10 . 1.02 3.2 . 5.5 - 7.8 .
. 0.9 . 0.9 . 4. 2 . -0. 9 . -2. 2 . -4.1 . -4.1 . -4.5 . -2. 6 . 1.5 .
. 0.39 . 0.97 . 1.10 , 1.24 1.22 . 1.20 . 1.15 . 1.17 . 1.15 . 1.20 . 1.22 . 1.24 . 1.10 . 0.97 . 0.39 7
. 0.30 . 0.98 . 1.20 . 1.24 1.20 . 1.15 . 1.07 . 1.10 . 1.07 . 1.14 . 1.24 . 1.19 . 1.24 . 1.04 . 0.41 ,
-2.2 . 4.3 . 1. 9 . 0.1 . 1.3 . 3. 9 . -4.4 . -4.1 . 4. 7 . -5. 0 . 1. 7 . 4.5 . 5.7 . 6.6 . 6.6 .
. 0.70 . 1.01 . 1.21 . 1.16 . 1. 21 . 1. 02 . 1.17 . 1. 0 7 . 1.17 . 1. 0 2 . 1. 21 . 1. le 1.21 . 1.01 . 0.70 .
0.60 . 1.01 . 1.23 . 1.15 . 1.19 . 0.99 . 1.00 . 0.99 . 1.09 . 0.95 . 1.21 , 1.22 1.20 1.08 . 0.75 . 4 1.9 . 0.3 . -1.4 . t.9 . -7.2 . -7.4 . 4.4 . 4.3 . -0.2 . 5.2 . 6.0 . 6.7 . 7. 3 . -
. .t.t . -0.6 .
. 0.19 . 0.97 . 1.14 . 1.24 - 1.22 . 1.20 . 3.15 . 1.17 . 1.15 . 1.20 . 1.22 1.24 1.18 . 0.97 . 0.39 .
. 6.18 . 0.90 . 1.21 . 1.24 . 1.21 . 1.17 . 1.09 1.09 . 1.07 . 1.13 . 1.19 . 1.27 . 1.23 . 1.03 . 0.42 . 9
. 2.2 . 4. 3 . 2.4 . 9.1 . - 0. 4 . - 2.1 . -4. 9 . -6.5 . -7.1 5.3 -2.6 . 3.0 . 4.1 . 6.1 . 7.5 .
. 0.95 , 1.12 . 1.24 . 1.20 . 1.16 . 1.20 . 1.02 . 1.20 . 1.16 . 1.20 , 1.24 . 1.12 0.95 .
0.97 . 1.15 . 1.25 . 1.19 . 1.13 , 1.14 0.96 . 1.14 . 1.11 1.16 , 1.25 . 1.15 . 0.99 . 10
. 1.7 . 2.7 . 0. 4 . -0. 7 . - 2. 6 . -4. 4 . -5. 2 -5.0 , -4.1 . -1.7 . 0.6 . 2.6 . 4.7 .
0.42 S.94 1.14 . 0.97 . 1.20 . 1.22 . 1.21 . 1.22 . 1.20 . 0.97 - 1.14 . 0.96 . 0.42 . 11 0.45 . 0.94 . 1.15 . 0.97 . 1.14 . 1.19 . 1.17 , 1.10 , 1.17 . 0.96 . 1.15 0.99 . 0.44 .
. 2.5 . 2.5 . 1.1 . 0.4 . 1.4 . -1.5 . -3.5 3.1 . .t.2 . -1.4 . 1.0 . 3.0 . 4.3 .
0.46 0.91 . 1.14 . 1.24 . 1.24 , 1.16 . 1.24 - 1.24 . 1.14 . 0.91 . 0.46 . 0.40 . 0.92 . 1.13 . 1.25 . 1.te . 1.14 , 1.22 . 1.23 . 1.13 . 0.92 . 0.44 . If
. 2.4 1.1 . -0.4 . 0.4 . 0.5 . -1.2 . -1.4 -0.6 . -0.2 . 1.7 . 3.9 . ,
0.46 . 0.96 . 1.12 . 1.10 . 1.01 . 1.14 . 1.12 . 0.96 . 0.46 . 13 0.40 . 0.99 . 1.14 . 1.10 . 1.21 , 1.19 . 1.13 . 0.97 . 0.44 .
. .- . . 2.9 . 3.5 . t.4 . 0.1 . -0.4 1.1 . 1.4 . 1.4 2.7
.. . ........................... ........t.....~....... . ...
. 0.42 . 0.95 . 0.97 . 1.01 . 0.97 . 0.95 . 0.42 . 14
. 0.43 . 0.99 1.00 . 1.04 . 1.00 . 0.97 . 0.43 .
. 3.5 . 4.5 . 3.1 . 2.2 . 2.5 . 2.1 . 1. 3 .
AbfPAGE . STAR @ARD . . 0.39 0.70 . 0.39 . . C.*1 . S.73 . M O . . PCT 01FFt2fflCt. 15
. Dtv1Ai!OM . .
. st.106 . . 5.7 . 4.6 3.0 . . s t.s .
SUMMARY
DATE1 12/30/81 PC'.4ER I 0% HAP N01 St-6 1 F-Q(T) s f.260 QPTR1
. CCNTPOL RCO PCSITICNSI 0 BA!;K AT 223 GTEPS F-CH(H) = 1.488 t.'W 0.992 i NE 1.017
.______.___[__________
FtZ) = 1.476 SW 0.992 l SE 0.999 F(XY) = 1.425 BURfAJP z 0 tM)/NTU A.O s 24.83t%) 35
l Figure 7.2 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST ! ASSEMBLYWISE POWER DISTRIBUTION HZP, B-BANK IN same J 5 A O P N M L K M G F
.E O C- .. .
.............. FPtDIC1tD
. FTt01CitO . . 0.45 . 0.82 . 0.45 . . .
. 0.47 . 0.80 . 0.47 . . Mt11LTED . 1
. r2A!Gt0 .
. PCT DIFFt0ENCE.
.PCF DIFFt5tNCE.
. 4. 3 . -2.4 4.5 .
. 0.39 . 0.94 . 1.05 . 1.15 . 1.05 . 0.94 0.39 .
. 0.41 . 0.98 . 1.07 . 1.15 . 1.07 . 0.98 . 0.41 . t 4-- ~-
. 5.0 . 4. 3 . 1. 7 . 0.3 . 1.8 . 4.3 . 5.8 .
. 0.40 . 0.80 . 0.95 . 1.17 . 1.30 . 1.17 . 0.95 . 0.40 . 0.40 .
0.42 . 0.82 . 0.97 . 1.21 . 1.29 . 1.20 0.99 . 0.e5 . 0.43 . 3 3.3 . -0.9 . 2.1 . 5.1 . 6.3 . 8. 0 .
- 4.4 , 2.4 2.6 . . .
, 0.40 . 0.76 . 0.87 0.45 . 1.16 . 1.13 . 1.16 . 0.65 . 0.87 , 0.76 . 0.40 .
4 0.41 . 0.77 . 0.87 . 0.65 . 1.17 . 1.25 . 1.19 . 0.68 . 0.91 . 0.80 . 0.43 . 2.9 . 2.2 . 9.1 . 0.3 . 1.0 . 1.7 . 2.8 4. 3 . 4. 8 . 5. 3 . 9.1 .
. 0.39 . 0.80 . 0.47 . 0.81 . 1.10 , 1.32 1.40 . 1.32 1.10 . 0.81 . 0.47 . 0.80 , 0.39 0.87 . 0.81 . 1.08 . 1.13 1.=0 . 1.34 . 1.11 . 0.83 . 0.90 . 0.28 . 0.45 . 5 0.40 . 0.81 1.7 . 1.6 . 0.2 . -0.6 -1.1 . -1.5 . 0.3 . 1. 9 . 1. 7 , 2.3 4.2 . 9.6 . 14.7 .
.................................. ...... 1.33 ............. ...... ............................ . .
. 1.51 . 1.32 . 1.10 . 0.65 . 0.95 . 0.94 0.94 . 0.95 . 0.65 . 1.10 . 1.32 - 1.51 0.47 . 1.03 . 1.06 . 6
. 0.94 0.94 . 0.64 , 1.09 . 1.*8 . 1.43 , 1.24 , 1.41 . 1.28 . 1.11 --
-0. 7 . -0. 8 . -1. 3 . - 0. 9 . - 3. 4 -5.5 . - 7. 0 . - 6. 8 . - 3. 5 . 1.6 , 3.5 . 8.7 . 12.7 .
.. 0.45
. . ,. 1.05
. . .. 1.17 . . ..1.16 . . ..1.32 . . ..1.51 . . ..1.59 . . ..1.65
. . ..1,59 . . ..1.51 . . ..1.32 . . . 1.16 . . .. 1.17 . . ..1.05 . . . .0.45. .. . . . . . . . . . . . . .
0.45 , 1.03 . 1.13 . 1.13 . 1.30 . 1.44 1.44 . 1.49 . 1.44 . 1.41 . 1.34 . 1.21 . 1.25 . 1.16 . 0.49 . 7
- 0. 2 . -1. 9 . =3.3 . *1.9 -0.9 . -4.4 . -9.1 . -9. 6 . -9. 4 . -6. 8 . 1.7 . 4. 7 . 6.9 9.9 . 10.4 .
. 0.82 . 1.15 . 1.30 . 1.23 . 1.40 1.33 . 1.65 . 1.57 . 1.65 . 1.33 , 1.40 . 1.23 . 1.30 . 1.15 . 0.82 .
1.23 . 1.40 . 1.28 . 1.36 . 1.26 0.92 . 8 0.E2 1.14 , 1.26 . 1.*1 1.33 . 1.*8 , 1.50 . 1.42 . 1.52 3.9 . 4. 5 . 9.6 . 11.8 . * ,
~
. 9. 2 . -1.1 . - 3. 3 . - 2.1 . -1. 2 . - 3. 9 . - 9. 2 . -9.1 . -8. 0 . - 7.1 . - 0. 2 0.45 . 1.05 , 1.17 , 1.16 . 1.32 . 1.51 . 1.59 . 1.6 5 . 1. 5 9 . 1. 51 . 1. 32 1.16 . 1.17 . 1. C5 . 0.45 .
l
. 0.45 . 1.08 . 1.24 . 1.16 . 1.28 . 1.46 . 1.47 . 1.53 . 1.47 , 1.43 . 1.31 . 1.21 . 1.*5 . 1.15 . 0.51 . -- 9 i . 0.2- 2.9 . 5.5 . 0.1 -2.6 . -3.6 . -7.0 . -7.5 . -7.4 . -5.2 . -0.5 . 4.5 . 6.3 . 9.5 . 13.4 0.95 . 0.65 .' 1.10 . 1.32 . 1.51 . 1.33 . 1.51 1.32 . 1.10 . 0.65 . 0.95 . 0.94 .
0.94 . 10 0.99 . 1.00 . 0.66 . 1.08 . 1.27 . 1,41 . 1.25 . 1,44 . 1. 26 . 1. C8 , 0. 6 7 . 1. 01 . 1. 0 3 . t t 5.5 , 5.3 . 1. 4 . -1. 2 . - 3. 7 . -6. 5 . -5.6 . -4. 8 . -4. 6 . -1.2 . 3.1 6.0 . 9.1 . ,-- 0.39 0.80 . 0.47 . 0.81 . 1.10 . 1.32 . 1.40 . 1.3* , 1.10 0.81 . 0.87 . 0.80 . 0.39 .
. 0.42 , 0.85 . 0.90 . 0.82 . 1.07 . 1.25 . 1.35 . 1.28 , 1.06 0.79 . 0.90 . 0.86 . 0.43 . 11 6.1 . 6.0 . 3.5 . 0.3 . -1.4 . -4. 8 . - 3. 2 -2.7 . -3. 0 . -2. 9 . 3.3 . 7.4 8.8 . ..
. 0.40 . 0.76 . 0.47 . 0.65 . 1.16 . 1.23 . 1.16 . 0.65 . 0.87 . 0.76 . 0.40 i
. 0.43 . 0.79 . 0.47 . 0.65 . 1.14 . 1.22 . 1.15 . 0.64 , 0.87 . 0.80 . 0.43 . It l -* - . 6.7 . 4.2 . 0.3 . -0.1 . -1.2 . -1.3 . -0.4 . -1.3 . 0.4 5.4 . 8.8 .
~ ~ ~
0.40 , 0. C0 . 0. 95 . 1.17 . 1. 3 0 . 1.17 . 0.95 . 0.80 . 0.40 . 13 0.43 , 0.46 . 1.01 . 1.18 . 1.31 . 1.21 . 0.98 . 0.84 . 0.43 . ~- - -* - --*
~----- - 6. 9 . 7.1 . 7.1 . 0.2 . 0.7 . 3.0 . 3.8 , 4.5 . 7.2 .
. - .............................. ~................................
0.39 . 0.94 . 1.05 1.15 . 1.05 . 0.94 0. 39 '.~ ~ 0.42 . 1.C2 . 1.11 . 1.20 1.10 . 0.93 , 0.41 . 14
. 7.1 . 7.8 . 5.5 . 4.2 . 4.5 . 4.4 . 3.7 .
. 0.45 . 0.82 . 0.45 . . Avt0 AGE .
. 57ANDA20 .
, PCT DIFFF9tHCE. 15
. OtVIA71CN . . 0.49 . 0.88 . 0.47 .
a 4.3
. as.144 .
. 4.0 . 7.4 . 5.0 . .
SUMuRY DATE1 12/30/81 PCWER: 1% MAP N01 S2 2 CCNTRot. R03 POSITIONSI F-Q(T) 8 2.641 QPTR: D BMM AT 228 STEPS F-OH(H)
- 1.799 NW 0.982 l HE 1. (t15
--l----------
B BAPE AT 23 STEPS 0.994 l SE 1.009 F(Z) a 1.392 SW F(XYl 1.710 bum 4UP 8 0 TED/MTU A.O = 19. 21( %) 36
1 ! Figure 7.3 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION I/E CALIBRATION - FLUX MAP W P. M M L K J H 6 F . E , O C S 6 '
. PEE 01CTED . . G.40 . 0.69 . 0.40 . . Pet 01CTED .
. MEA 1URfD . . 0.40 . 0.70 . 0.40 . r'115URED 1
. PCT 01FFERENC2. . 0.8 . 0.6 . 1.3 . .. PCT DIFFletNCE..
. 0.44 0.96 . 0.97 . 0.97 . 0.97 . 0.96 . 0.44
. 0.46 . 0.97 . 0.97 0.97 . 0.97 . 0.98 . 0.45 . 2
. . 3.9 . 1.2 . 0.4 . -0.1 . 0.9 . 2.1 . 1.9 . .
~* - - ...................... ........................................
. 0.49 . 0.94 . 1.12 . 6.17 . 1.20 . 1.17 . 1.12 . 0.98 . 0.49
. 0.50 0.99 . 1.13 . 1.16 . 1.19 1.18 . 1.14 . 0.99 0.50 *
. 3.4 1.8 . 0.6 . 0.4 . =0.7 . 0.5 . 1.4 . 1.8 . 1.7 .
-- ~
. 0.49 . b. 93 . 1.15 . 1.24 . 1.23 . 1.16 1.23 . 1.24 . 1.15 . 0.93 . 0.49 .
. 0.4 9 . 0. 94 . 1.15 . 1.23 . 1.23 . 1.16 . 1.23 . 1.26 . 1.16 , 0.95 . 0.51 . 4
~ . 1.4 0.9 0.0 . -0.4 -0.3 . 0.1 . 0.5 . 1.* . 1.2 . 1.4 . 3.9 .
0.44 . 0.94 . 1.15 . 0.98 . 1.16 . 1.21 . 1.20 - 1.21 . 1.14 . 0.96 . 1.15 . 0.98 . 0.44
. 0.44 . 0.97 . 1.14 0.97 . 1.17 . 1.19 . 1.18 . 1.19 . 1.17 . 0.98 . 1.17 . 1.02 .'O.47 . 5
. -0.2 . -0. 2 . -0. 3 . - 0. 6 . -0. 6 . -1. 8 . -2. 0 . -1. 2 . -0.1 . 0.3 . 1. 7 . 5.0 . 8.0 .
. 0.96 . 1.12 . 1.24 . 1.18 . 1.10 . 1.16 . 1.03 . 1.16 . 1.10 . 1.16 . 1.24 . 1.12 . 0.96 .
. 0. 96 . 1.13 . 1.24 . 1.14 . 1.07 . 1.13 . 0.94 . 1.13 . 1.06 . 1.18 . 1.26 . 1.17 . 1.02 . 6
. 0.6 . 0.6 . 8.1 . -0.1 . -2. 3 . -4. 6 . -4. 7 . -4. 4 . - 3.5 . 0.2 . 1. 7 . 4.4 . 6.6 . .
. 0.40 . 0.97 . 1.17 . 1.23 . 1.21 . 1.18 . 1.15 . 1.17 - 1.15 . 1.18 . 1.21 . 1.23 . 1.17 . 0.97 0.40 .
0.39 . 0.97 . 1.19 . 1.23 . 1.20 . 1.14 . 1.07 . 1.11 . 1.09 . 1.13 . 1.22 . 1.26 . 1.21 1.01 . 0.41 . 7
. -2.4 . -0.1 . 1. 3 . 0.2 . -0.6 . -3.5 . -7.0 . -5.8 . -5.3 . -4.2 . 0.5 . 2.3 . 3.0 . 4.6 . 4.4
. 0.69 . 0.97 . 1.20 . 1.16 . 1.20 . 1.03 . 1.17 . 1.06 . 1.17 . 1.03 . 1.20 . 1.16 . 1.20 . 0.97 . 0.69 .
0.68 . 0.9e . 1.22 . 1.15 . 1.19 . 0.99 1.09 . 1.01 . 1.10 . 0.96 . 1.19 . 1.18 . 1.22 . 1.00 . 0.73 . s
-2.6 . -1.2 . 1. 3 . -0. 6, . -1. 3 . - 3. 0 . - 7. 2 . -6. 6 . -6. 3 . -4. 0 . -1. 3 . 1.8 . 1.9 . 3.2 . 5. 0 . -
. 4.40 . 0.97 1 17 . 1.23 . 1.21 . 1.1a . 1.15 . 1.17 . 1.15 . 1.18 . 1.21 . 1.23 . 1.17 . 0.97 . 4.40 .
0.39 . 0.94 . 1.23 . 1.23 . 1.19 . 1.15 . 1.06 . 1.09 . 1.07 . 1.12 . 1.17 . 1.24 . 1.20 . 1.01 . 0.42 . 9
. -2.4 . 1.2 . 4.5 . 0.4 . -1.3 . -2.7 . -5.9 . -6.9 . -7.3 . -5.6 . -2.4 . 0.4 . 2.3 . 4. 3 . 6.3 .
- 0. 96 . 1.12 . 1. 24 . 1.18 . 1.10 . 1.14 . 1. 0 3 . 1. la . 1.10 . 1.18 . 1.24 1.12 . 0.96 .
1.00 1.17 . 1.26 - 1.17 . 1.06 . 1.12 0.97 1.13 . 1.05 . 1.17 . 1.25 . 1.15 . 1.01 . 10
. 4.5 . 4.5 . 1.4 . -0.4 -3.1 . -5.6 . -4. 9 . -. 7 . - 3. 9 . -0. 9 . 0.5 . 2.6 . 5.0 . .
. 0.44 0.96 . 1.15 . 0.98 . 1.18 . 1.21 . 1.20 1.21 . 1.18 . 0.98 . 1.15 . 0.94 . 0.44
. 0.46 . 1.02 . 1.14 . 0.98 . 1.17 . 1.16 , 1.18 , 1.16 . 1.16 . 0.99 . 1.16 . 1.00 . 0.46 . 11 i . 4.2 . 4.2 . 2.6 . 0. 6 . -1. 0 . - 2. 2 . -2. 2 . -2.1 . -1.5 . 0.4 . 1.4 2.4 . 3.9 .
l .... ................................................................................... ..
. 0.49 . 0.93 . 1.15 . 1.24 . 1.23 . 1.16 . 1.23 . 1.24 1.15 . 0.93 . 0.49
. 0.51 . 0.96 1.15 . 1.25 . 1.24 . 1.15 . 1.22 . 1.25 . 1.16 . 0.95 . 0.50 . It
. 3.9 . 2.6 . 0.6 . 1.0 . 0.7 . -1.0 . -0.6 . 1.0 . 1.2 . 1. 7 . 2.5 .
. 0.49 . 0.93 . 1.12 . 1.17 . 1.20 . 1.17 . 1.12 . 0.98 . 0.49 0.51 . 1.04 . 1.17 . 1.17 . 1.10 . 1.19 . 1.16 . 1.00 . 0.50 . 13
.. - - . 5.3 . 4. 7 . 4.0 . -0.4 . -1.4 1.2 . 3.5 . 2.4 . 2.0 . . .- -
...... m e.................................n................... * "
. 0.44 0.96 . 0.97 0.97 . 0.92 . 0.94 . 0.44
. 4.47 . 1.02 . 0.99 0.90 . 0.98 . 0.99 0.45 . 14
. 6.7 . 6.5 . 2.7 . 1.2 . 1. 7 . 2.4 . 3.6 . -
. 57ANDA00 . . 0.40 . 0.69 0.40 . AVERAGE .
DEVIATION . . 0.42 . 0.72 . 0.40 . . PCT 01FFERENCE. 15
. *2.01a . . 5. 7 . 4.1 . 1. 9 . . = 2.5 .
E'.EMARY r,Ap gol 52-6 3 DATE1 1/ 1/82 PC'4ER 1 47% CC'4 TROL RCD POSITI0t*S1 F-Q(T) = 1.982 CPTR1 D DAt* AT 184 STEPS F-CH(H) = 1.446 h"4 0.992 l NE 1.005
...........l..........
F(Z) = 1.305 EL4 1.004 l SE 0.999 - F(XY) = 1.404 BLmp = 10 t*WO/NTU A.O = -0.54(%) i l i 37 I 1
Figure 7.4 SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST ASSEMBLWISE POWER DISTRIBUTION I/E CALIBRATION - FLUX MAP O P N M g N $ F E O C S 6 L J
. PWEDICitD .
8.41 . 0.71 . 0.41 . . PRf0ICTED .
. MEASUat0 0.41 . 0.71 . 0.41 . nfA5'Jt0 . 1
.PC7 O!FFERENCg. . -0.0 . -0.2 . 0.6 .
............ .. .................................................. ..PC7 Dif.FERENCE.
- ~ 0.45 . 0.96 . 0.97 . 0.90 . 0.97 . 0.96 . 0.45 .
4.45 . 0.97 . 0.97 . 0.97 . 0.97 . 0.97 . 0.45 . I
- 1. 3 . 0.8 . -0.0 . -0.6 . 0.3 . 1.6 . 1.5 .
0.50 . 0.97 . 1.11 . 1.17 . 1.20 . 1.17 . 1.11 . 0.97 . 0.50 .
. 0.51 4 0. 9 8 . 1.12 . 2. a s . 1.19 . 1.18 . 1.13 . 0. 9 9 . 0. 51 . 3
. 1.2 . 1.1 . 0.9 . 0.5 . -0.9 . 0.6 . 2.3 . 1. 9 . 1.5 .
. 0.50 . 0.94 . 1.14 . 1.23 . 1.21 . 1.15 , 1.21 . 1.23 . 1.14 0.94 . 0.50
. 0.50 . 0.95 . 1.15 . 1.23 . 1.21 . 1.15 . 1.22 . 1.26 . 1.16 . 0.96 . 0.52 .
4
. 0.4 4.4 . 0.9 . 0.4 =0.3 . -0.1 . 0.4 . 2.4 . 1.9 . 1.6 . 3.5 .
0.45. 0.97. 1.14- 0.9s , 1.16 . 1.20 . 1.20 . 1.20 . 1.16 . 0.98 . 1.14 - 0.97 . 0.45 .
. 4.45 . 0.97 . 1.14 . 0.93 . 1.17 . 1.19 . 1.17 . 1.19 . 1.17 . 0.99 , 1.16 . 1.02 , 0.44 . 5
. 0.2 . -0.2 . 0.5 . 0.4 . 0.2 . -1.4 . -1.6 . -1.2 . tot . 1.0 1.9 . 4.6 . 7.2 .
. 0.96 . 1.11 . 1.23 . 1.16 . 1.10 1.19 . 1.04 . 1.19 . 1.10 . 1.16 . 1.23 . 1.11 . 0.96 .-
0.97 . 1.11 . 1.24 . 1.17 . 1.04 . 1.14 . 0.99 . 1.13 . 1.05 . 1.17 . 1.25 . 1.16 . 1.01 . 6 1.3 . 1. 3 . 0. 9 . 0. 6 . -1. 7 . -4. 4 . -4.6 . -5.2 . -4.4 . 0.3 . 1. 3 . 4.3 . 6.0 .
. 0.41 . 0.97 . 1.17 . 1.21 . 1.20 . 1.19 . 1.17 . 1.18 . 1.17 . 1.19 . 1.20 . 1.21 . 1.17 . 0.97 . 0.41 . 7
. 0.39 . 0.97 . 1.20 . 1.23 . 1.20 . 1.15 . 1.08 . 1.11 . 1.09 . 1.13 . 1.21 . 1.25 . 1.20 . 1.01 . 0.43 .
. -4.7 . -0.1 . f.7 . 1.1 . -0.1 . - 3. 3 . - 7. 0 . 6. 2 . -4.4 . -5.4 . 0.5 . 3.0 . 3.0 . 4.2 . 3.9 .
, 0.71 . 0.98 . 1.20 . 1.15 . 1.20 . 1.04 . 1.18 . 1.10 . 1.16 . 1.04 . 1.20 . 1.15 . 1.20 . 0.98 . 0.71 .
0.64 . 0.96 .- 1.23 . 1.16 . 1.19 . 1.01 . 1.10 . 1.03 . 1.11 . 0.98 . 1.19 1.16 . 1.22 . 1.00 . 0.74 a
, -4.9 . -4.0 . 1.7 . 0.4 . -0.7 . -2.4 -7.2 -4. 9 . -4. 3 . -6. 0 . -0. 8 . 2.2 . 1.8 . 2.4 . 3.4 .
.4.41 . 0.97 . 1.17 . 1.21 . 1.20 1.19 . 1.17 . 1.18 . 1.17 1.19 . 1.20 . 1.21 . 1.17 . 0.97 . 0.41 .
0.39 . 0.97 . 1.22 . 1.22 . 1.20 . 1.17 . 1.10 , 1.11 . 1.0,. 1.13 . 1.17 . 1.23 . 1.20 1.00 . 0.43 . 9
, -4.7 . 0.1 . 4.6 , 1.0 . -0.2 . -1.9 . - 5. 4 . -4. 3 . -6. 5 . -5. 4 - -t.5 . 1.1 . 2.4 . 3.6 4.4
. 0.96 . 1.11 . 1.23 . 1.16 . 1.10 . 1.19 . 1.04 . 1.19 . 1.10 , 1.16 1.23 . 1.11 , 0.96 . -
. 1.00 . 1.16 . 1.25 . 1.17 . 1.07 . 1.13 . 0.99 . 1.15 . 1.07 . 1.16 . 1.24 . 1.14 . 1.01 . 10 4.5 . 4.5 , t.0 0.1 . -3.6 . -5.4 . -4. 2 . - 3.7 . -2. 9 . - 0. 3 *. 1.1 3.0 . 5.0 l ............................................................................................
. 0.45 . 0.97 . 1.14 . 0.98 . 1.16 . 1.20 . 1.20 . 1.20 . 1.16 . 0.96 . 1.14 . 0.97 . 0.45
. 0.47 . 1.01 . 1.16 . 0.98 . 1.16 . 1.19 . 1.18 . 1.20 . 1.17 . 0.99 . 1.15 . 0.99 . 0.46 . 11
. 4.2 . 4.2 . 2.5 . 0.3 . -0.6 . -1.1 . -1.1 4 -0.6 . 0.2 . 0.9 . 1.2 . 2.3 . 3.9 .
-- 0.50 . 0.94 . 1.14 . 1.11 . 1.21 . 1.15 . 1.21 . 1.23 . 1.14 . 0.94 . 0.50 . -
. 0.52 . 0.96 . 1.14 1.25 . 1.24 . 1.16 . 1.22 . 1.25 . 1.15 . 0.95 . 0.51 . It
. 3.8 . 1.4 . 0.3 . 2.1 . 2.4 0.2 . 0.3 , 1. 7 . 1.3 . 1.2 , 1.9 .
- - - - . 0.50 . 0.97 . 1.11 . 1.17 . 1.20 . 1.17 . 1.11 . 0.97 . 0.50
. 0. 5 2 . 1. 0 2 . 1.15 . 1.l a . 1.19 . 1.19 . 1.15 . 1. 0 0 . 0. 51 . 13
. 4.1 . 4.4 3.4 . 4.4 . -0. 7 . 2.0 . 3.7 . 2.6 . 1.4 *
- , ---- - ..............................................s.......,........ --
l . 0.45 . 0.96 . 0.97 . 0.98 . 0.97 . 0.96 . 0.45 . ' . 0.47 . 1.00 . 0.94 . 0.99 1.00 . 1.00 0.46 . 14 l . 4.4 4.1 . 1.4 . 1. 3 . 3.4 3.8 . 3.6 .
. 0.41 . 0.71 . 0.41 . AvtpAGE .
STANDARD . . OtVIATIQH . . 0.42 . 0.74 . 0.42 . .PC7 O!FFERENCE. 15 3.4 s 2.4
. s1.114 . . 3.3 . . 3.8 . . .
SUMMARY
MAP NO2 St-6 4 DATE1 1/ 1/82 PCWER1 59% CCNTROL RCD POSITIONS 1 F-QtT) = 1.962 QPTH1 D BANK AT 180 STEPS F-OH(N) = 1.426 NW 0.993 l NE 1.003
..........[.._-__
F(Z) = 1.303 SW 1.004 l SE
- J00 F(XY) = 1.383 eURNUP = 17 MWD /MTU A.O = -6. 0 0( % )
38
Figure 7.5 l SURRY UNIT 2 - CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION 1/E CALIBRATION - FLUX MAP G p M M L M J M 0 F t 0 C 0 A
. PetCIC1t3 . . 0.42 . 0.74 0.42 . . PSt3!CTED .
. Mt&5Unto . . 0.41 . 0.74 . 0.42 . . MlASUREO , 1
.PC7 OIfftBENCE. . -1.7 . -1.0 . -0.3 . .PC7 OIFFEstt:CE. .
. 0.44 0.95 . 0.90 . 1.03 . 0.90 0.95 . 0.44'.
. 0.44 0.96 . 0.97 . 1.08 . 0.90 . 0.97 . 0.45 . t
. 0.9 . 0.3 . -0.9 . -1.4 . -0.2 . 1.7 . t.0 .
. 0.49 . 0.96 . 1.10 1.17 . 1.21 . 1.17 . 1.10 , 0.96 0.49
. 4.49 . 0.96 . 1.10 - 1.17 . 1.19 . 1.17 1.12 . 0.90 . 0.50 . 3 0.9 . 0.9 . 0.5 , 0.1 -1.3 . 6.4 . 2.0 . 2.3 . 2.5 ,
0.49 . 0.92 . 1.12 . 1.21 1.21 . 1.15 . 1.21 . 1.21 1.12 0.92 -- 0.49 . 0.49 . 0.93 . 1.13 . 1.21 . 1.20 . 1.15 , 1.21 . 1.44 . 1. a . k. w . 0.51 . 4
. 0.0 . 0.5 , 0.6 . *0.1 . -0.4 . 9.2 , 0.7 . 2.2 . 2.0 . 2.0 3. 3 ,
. 0.44 . 0.96 . 1.12 . 0.97 . 1.17 . 1.20 . 1.19 . 1.20 . 1.17 . 0.97 . 1.12 . 0.96 . 0.44
. 0.44 . 0.94 . 1.12 . 0.97 . 1.17 . 1.19 1.17 . 1.19 . 1.17 . 0.90 . 1.14 . 0.99 . 0.46 . 5
. 0.9 . 0.9 . 0.3 . -0.4 . -0.4 . -1.4 1.7 . -1.2 0.0 0.9 . 2.0 3.7 . 5.2 .
. 0.95 1.10 . 1.21 . 1.17 . 1.15 . 1.20 . 1.04 . 1.20 . 1.15 1.17 . 1.21 . 1.10 . 0.95 .-
0.96 . 1.11 . 1.21 . 1.17 . 1.13 . 1.15 . 0.99 1.14 . 1.10 . 1.10 . 1.25 . 1.14 . 1.00 . 6
-1. 0 . -4. 2 . -4. 6 . -4. 9 . - 3. 6 0.5 , t.5 , 3.9 , 4.9 .
0.0 . 0.0 . 0.3 . 0. 3
. 0.42 . 0.93 . 1.17 . 1.21 1.20 . 1.20 . 1.17 . 1.10 , 1.17 . 1.20 , 1.20 . 1.21 1.20 . 1.01 .. 0.42 1.17 . 0.90 .
7
. 0.40 . 0.97 . 1.10 . 1.21 . 1.11 - 1.17 . 1.10 . 1.11 . 1.10 . 1.14 . 1.22 . 1.25 2.5 0.43 .
. -4.0 -1.1 0. 7 . 4.4 . 0.1 . - 3. 0 . -4. 3 . 5. 0 . -6. 0 . -5.0 . 1.0 3.5 . 3.6 . 3.0 .
. 0.74 1.01 . 1.21 . 1.15 . 1.19 , 1.04 . 1.10 . 1.10 . 1.10 . 1.04 . 1.19 . 1.15 . 1.21 , 1.03 , 0.74 0
0.71 . 1.00 . 1.22 . 1.15 . 1.19 1.02 .' 1.11 - 1.03 . 1.11 . 0.90 . 1.19 . 1.17 . 1.22 . 1.04 . 0.76 .
. -4.1 -2.3 . 0. 7 . - 0.1 . - 0. 3 . - 2. 2 . 6. 5 . 6. 6 . -6. 0 - -5.5 . -0.1 2.1 . 1.0 . 1.4 . 3.0 .
. 0.42 0.95 , 1.17 . 1.21 . 1.20 , 1.20 . 1.17 . 1.10 , 1.17 . 1.20 . 1.20 . 1.21 1.17 . 0.93 . 0.42 .
9
. 0.40 0.90 . 1.22 . 1.22 . 1.20 . 1.10 . 3.12 1.11 . 1.09 1.15 1.10 . 1.21 1.10 1.00 . 0.43 .
-4.0 . 0.4 4. 7 . 0.9 . -0.7 . -1.7 . -4.6 . 6.0 . -6.5 -4.5 , -t.1 . 0.6 , 1.2 2.5 . 4.0 .
. 0.95 1.10 , 1.21 1.17 . 1.15 . 1.20 . 1.04 , 1.20 1.15 . 1.17 . 1.21 . 1.10 . 0.95 .
1.00 . 1.15 . 1.14 . 1.16 1.12 . 1.15 . 1.00 . 1.16 . 1.12 1.17 . 1.22 . 1.12 . 0.99 . 10
. 4.7 . 4.7 . 1.0 . =0.5 . -2.4 -4. 3 , . 3. 0 . - 3. 3 . -t.3 . 0.2 . 0.0 . 2.1 . 3.6 .
. 0.44 0.96 . 1.12 . 0.97 . 1.17 . 1.2t . 1.19 . 1.20 . 1.17 . 0.97 1.11 , 0.94 0.44 . 11
. 0.44 . 0.99 . 1.14 .
0.97 , 1.16 . 1.19 . 1.10 . 1.*0 . 1.14 . 0.90 . 1.13 . 0.9m . 0.45 . 3.5 . 3.5 . 1.9 -0.1 . - 0. 7 . -1.1 . -1. 0 . -0. 0 - 0.9 . 0.7 . 1.2 . 2.1 . 3.2 . l l 0.49 . 0.92 . 1.12 . 1.21 . 1.21 . 1.15 . 1.21 . 1.21 . 1.12 . 0.92 . 0.49 j i
. 0.50 . 0.94 . 1.12 1.23 . 1.22 . 1.15 . 1.21 . 1.24 - 1.14 . 0.t4 . 0.50 . 12
- . 2.3 . 1.3 . -0.1 . 1. 3 . 1.6 . -0.3 . 0.6 2.2 - 1.5 . 1.2 . 2.6 .
- . 0.49 . 0.96 . 1.10 . 1.17 . 1.21 . 1.17 . 1.10 . 0.96 . 0.49 . 13 0.51 . 1.02 . 1.14 . 1.17 . 1.19 . 1.19 . 1.14 . 0.99 . 0.50
. 4.2 6.1 . 4.2 . 9.1 . -1.3 . 1.0 . 4.4 3.1 . 1. 7 .
- - - ~~~ 0.44 . 0.95 0.*0 . 1.03 . 0.90 . 0.95 . 0.44 14
. 0.47 . 1,00 . 0.99 . 1.03 . 1.00 . 0.99 . 0.46 6.1 . 4.9 . 1.0 . 1.0 . 2.6 . 3.7 . 4.5 . .
0.42 . 0.74 . 0.42 . Avtract .
. STA8 CARO .
0.43 . 0.76 0.43 . . ..PC7 01FFletHCt. 15
. CEVIATICH . = 2.2
. s1.776 . 3.0 . 3.0 2.9 . . .
CUMMARY DATE! 1/ 1/82 FCWER1 60% MAP HO: S2 5 CC ITRCL RC3 P35ITICHS: F-QtT) = 1.853 GPTRt D CA!M AT 204 STEPS F-CHfH)
- 1.422 W 0.991 1 NE 1.003
__________l__________ F(Z) = 1.255 5'J 1.005 l SE 1.001 F(XY) = 1.373 BURNUP s 22 tL'0/MTU A.O z 5.94(%) 39 l
l I ytn2a t*9 SnHHA GNII 3 - 3 ADIT 9 EOI' dHASI3S 12SI VSS3NEINMIS3 dom 3H GISIHIEn1 ION H3d' 30' X3NON 5 d N W 1 3 f N 9 J a 3 0 3 V
..............a._...._
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- t*2
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- 1.g . g.g...... .
0* 69*
- t
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- 1* 20
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* .0*t * -t*0 * -t*( * *3** * -t*4 * -t*5
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- t*4 * **9 **0 *......... . . - .9
- 0 *
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................................'t* -1 9 * -t*5 * -t'9 * -t*9 * -2*6 *..........................................'9 O 2*2
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96* 0*2 * -0*T * -0*9 * -t*2
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- t*2
- 0.g . g.g . . s'.g..*.
............'..........................................'9. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . _ ... 9. g
' 0
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* -9*t 8*91* **1*5 0*69 * *C*0 t'tG* 0* *1*31
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........................................................................................................5
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- 0.g . g.g . g.g . g.g......_ . . . -
- 0* 45
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8*fO
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it
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- t.v e u w n* t s. .s .g.3. . . .3,...
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. g.g . . -
S1TWWYNA WVd MC: S2 4 OY131 2/I0/92 dom 35: I00% 30115C1* 50C DOS 11IONSI J-D)1( z I*496 04152 0 9V4M Y1229 513dS J-OHIN( z I*ESI NM 0*662 l H3 I*002
.__. __.__g_________.
J)2(
- I*2I9 SM I*009 l S3 I*002 J r( a I*EES Gnd4Vfd z III9 WMCWM( Y*O x -2'I6)%(
70
L L - _ .. . .. . Soction 8 REFERENCES
- 1. M. E. Paul, S. A. Ahmed, "Surry Unit 2, Cycle 6, Design Report," HFE Technical Report No. 209, Vepco, November, 1981
- 2. Surry Power Station Technical Specifications. l
- 3. Surry Power Station Final Safety Analysis Report.
- 4. T. K. Ross, W. C. Beck, " Control Rod Reactivity Worth Determination By The Rod Suap Technique," VEP-FRD-36A, December, 1980.
- 5. T. J. Kunsitis, "RXFLOW, A Computer Program to Calculate Reactor Flou and Thermal Output," NFO-CCR-8, Vepco, December, 1979.
- 6. " Technical Manual for Westinghouse Solid State Reactivity Computer,"
Westinghouse Electric Corporation.
- 7. W. Leggett and L. Eisenhart, "The INCORE Code," WCAP-7149, December, 1967.
i l l 41
4 1 APPENDIX STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEETS l
/
J e 42 .
'I f
/
~
jut, y , p SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PHY::ICS Tt:ST hESULTS AMD EVALUATIDH 51:37.T I l Test Descriptic,ns, Reactivity Computer Checkout R3ference i Proc Hs /Section: PT28.11/ APP. B Gequence Step Mos b II l Bank Positions (Steps) ! RCS Temperature C'T): 547 Test l l Power Level (% T.P.): 0 Canditions! SDA: 228 SDB: 228 CA: 228 l Other (specify): (Design) l CB: 228 CC: 228 CD
- l Belou Huclear Heating l l *At the just crit. Position 1
III I Bank Positions (Steps) 1 RCS. Temperature ('T): fY& f Test ! l Poues Level (% T.P.):d conditions! SDA: 228 SDB: 228 CA: 228 l Other (Specify): CD /4f (Actual) l CB: 228 CC: 228 I g g gsss=# W 4* ( # #sr M l Date/ Time Test Performed l I l /$l2fl01 0 4*'N l Measured parameter i O = Mensured Reactivty using0 -comp c IV l (Description) l D = Inferred React from react period e I I l 1 o , 24.1 -21.o to's -ns sz.s 4s.g l Measured Valuu ; 0' =Z 111 .jp J! ' -re.* Test l l %b m,,41 p ,gy .ss.Lj,9 , g ,, Rosults l I I Design value l l (Actual Conditions) ! %D = lCo c ~ t
} ##
t tx 100% 5 4.0% l_ l l Design Value l I (Design conditions) I %D = f(A c -O g ) /D e lx 100% 5 4.0%
.I I l Referance l WCAP 7905, Rev. 1. Table 3.6 I I I I V l TSAR / Tech Spec l Not Applicable Acceptance l I Criteria l I l' Reference i Mot Applicable i I I
l Design Tolerance is met : /YES Ho VI I Acceptance criteria is met : # YES HO
, Ccaments l-l l Allouable Range = 2 *[/, [gga l
Completed By - 1Id O Evaluated By: N Test Engf er / Recommended for s , Approval By : C d '==<4 HTO Engineer A.1 .
5 31 q SURRT POtlER STATION UNIT 2 CTCLE 6 STARTUP Pl!YSICS TEST RE::ULTS AND EVALUATICH OHEET I I Test
Description:
' Critical Boron Cencentration - ARO Proc Ho /::ection: PT23.11/ APP. C Sequence Step Hot ~[ 13forence ! Bank Positions (Steps) l RCS Temperature ('T): 547 II I Tost ! l Power Level (% T.P.): 0 I Other (specify): canditions! SDAt 228 SDB: 228 CA: 228 l Belou Huclear Heating (Dosign) ! CB 228 CC: 228 CD 228 i I III l Bank Positions (Steps) 1 RCS TemPeratura (*T): 511.2 Test l I Pouer. Level (% T.P.): 0% SDA Z28 SDB 2a8 CA: 226 1 Other (Specify): Canditions! (Actual) l CB:228 CC: 228 CDsa28 i S e /o w O u c /c ar McMy I Date/ Time Test Performed: I. I 1 2 /2.7 /61 /030-//00 l I l Mens Parameter i
'IV l (Description) l ( C g )he, ; Crit Boron Conc - ARO I I I I I Measured value 1 (C s)b" l 'f 5 2. ppen Test i i Raoults ! l l Design Value i I (Actual Cond) I ce= / '/'/5 250 ppm i I l Design Value i 1 (Design Cond) 1 Cg = 1445 1 50 ppm ,
I I I Reference ! VEP-TRD-HTE-209 I I I I V l TSAR / Tech Spec l " Ca xCO 5 15,115 per Accoptancel I Criteria i Reference 1 TSAR Section 14.2.5 1 1 1 Design Tolerance is met : /YES NO I Acceptanco Criteria is met a g.YES Ho i VI l Ccaments !"C6 * ~8.44 Pcm/ ppm f or prelimin ary an:1ysis i I"c = - 7.33 P ff* b fed
/
d y5 l . _ Ccapleted By: * - JA!@lda Evaluated By: O M test Ehgi er Recommendef. for C >g Approval By s' $ A.2 HTO Engineer
Jtil 3 ? 1983 3URRY POWER ::TATICH thMIT 2 CYCLE 6 STARTUP PflYOICO TEST RESULTS AND EVALUATICH S!!E~T I l Test Description Isothermal Temperatu:e Coefficient-ARO Reference ! Proc Ho / ections'PT28.11/ APP. D Sequence Step Hot B II l Dank Positions (Steps) l RC3 TemPe:atu:e (*T): 547 Test i I Pouer Level (% T.P.): 0 Conditions! SDA: 228 ODB: 228 CA: 228 l Other (specify)8 (Dasign) I CD 228 CC: 228 CDs 228 l Belou Huclect Heating I I III I Bank Positions,(Steps) l RCS TemPe ature (*T): S Y Y. / Test l l Pouer Level (% T.P.): 0 7-Conditions 1 3DA: 220 SDB: 228 CA: 22B ! Other (Specify): * (Actual) i CB 220 CC: 226 CD 228 1 Below Nuclear Heating I I l ""Qi'#;si"'lin =7#6 l l l _. l Mens Parameter i IV l (Description) l (4 * )Ago Iso Temp Coeff - 120 l l I I Test i Mansured Value I ( c 55 )uo =
- 3. 40pcmp (Cc = lyys)
Results l l l Design Value ! l (Actual Cond) ! (*Cf )w = '[, y 2 O. Ogmh( C h * /Y'/ E ) 1 I l I Design Value (Design Cond) Il ( -(?* )% = - 4.42 + 3.0 pcm/*T (Cg = 1445 ppm) i I l Reference ! VEP-TP.D-HTE 209 I l-1 I V l TSAR / Tech Spec l ec.i.s c 5 0.44 pcm/*r .r.f = -2.06 pcm/*r Acceptancel l Criteria l l I Reference l TS 3'. 1 , VEP-TED-HTE 209 I I I I Design Tolerance is met /YES HO VI l Acceptance Critaria is met /YES _HO I Comttents l " Uncertainty on " N o =.0.5 pcm/*r (Refe:ence: memorandum I from C. T. Snou to E. J. Lonito dated June 27, 1989). I I _ Completed By: / - lN ONL Evaluated By: - N
~ 'T'e s t Engin' r Recommended for Approval By 8 I ff /- "*'
HTO Engineer A.3
.!UI. s g m SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP Pi!?OICO TEST RESULTO AMD EVALUATION OMEET I l Test Description. M/D Tlux Map - HZP, ARO Reference l Proc Ho / Coction: PT28.2, OP-57 Sequence Step Ho: q II I Bank Positions (Steps) i ECS Temperature ('T) Tggp r1 Test I l Power Level (% T.P.) -0 Conditionsi SDA: 228 3D3: 228 CA: 228 l Other (specify)
(Dasign) l CB : 228 CC 223 CD: 228 i Must have 2 40 thimbles l I III I Bank Positions (Steps) ! RC,5 Temperature ('T): F y 7 sg Test l l Power Level (% T.P.): _fg Conditionsi :DA: 22D SDB a d a 6 CA 220 l Other (Specify): (Actual) l CB JJ6 CC 228 CD s a.2. 3 I l l 4'7tk.Ases l Date/ Time Test l l Performed g 'L / 30 /S I OACA I I I l l MAX. REL l NUC EXTHALITOTAL HEAT! QUADRANT IV l Mens Pernmeter! AS3Y PWR I RISE HOT -l TLUX HOT IPOUER TILT I (Description) I % DITT l CHAM TACT lCHAN TACT l RATIC I I (M-P)/P 1 T-dH(N) ! T-9(T) l 2PTR I I l i I I Iw c, f ' ' "21 I I a Test l Mensured Value1 i I,486 1 d . 3. 6 0 i f,0 iG $ Results i 17 '? /* 8 * * # 'd ! I I I Design Value 'l ste: r., e ~, . , I I I I ( Design Conds ) I '"* '" y * ;') l'k 2 2 55(2* 2(2-r))lrl(2) * '. 36 = 'tt:ll
< 1.02 I I I I I l lWCAP-7905 l l l WCAP-7905 l Reference ! REV. 1 l XONE I NOME I REV. 1 I I I I I I I I -
1 I V l TSAR / Tech Spec l NONE l HA l MA' l NA Acceptancel l l l 1 Criteria i i l I i l Reference l MOME I T.O. 3.12 1 T.S. 3.121 T.S. 3.12 I I I I I I l_ l 1 1. I I Design Tolerance is met : ! !ES N0 l Acceptance Criteria is met
- 7 YES NO VI l . . .
. Comments I l
i I
~
, Completed By> - Ill MIA Evaluated By: V fest EnginLjr j) Recommended for Approval By C- - A HTO En g :.ne e r
. A.4 .
JUL 311920 SURRY POWER ST?. TION UNIT 2 CYCLE 6 STARTUP Pl!YSICS TEST F.E::ULTS AHD EVALUATION SHEET I l Test Descriptions.Cntl Ennk B Morth Mens.-Rod Susp Red Bank Reference l Proc Mo /Section: PT23.11/ APP. E Sequence Step Mos 10 II l Bank Positions (Steps) l RCS Temperature ('T): 547 Test l I Pouer Level ( *: T.P.): O Conditions! SDA: 220 SDB 223 CA: 228 l Other (specify): (Design) l CB: Moving CC: 228 CD: 228 l Below Huclear Heating i i III l Bank Positions *(Steps) l RCS Temperatura ('T): 516.o Test l l Pouer Level (?. T.P.): 0% Conditionsl SD A i 2 25 SDB: 22d CA 228 i Other (Specify): (Actual) l CB noviay CC 228 CD: 226 i Belou nuclear nenting i i l Date/ Time Test Performed: l I l l2/30/91 0530 I I l Measured Parameter l I"g ; Integral Worth of Cntl Bank B, I (Description) l All other Rods Out IV i 1 I I Test Results i Measured Value i I$tF =
/37/ pcm l l t Design.value i I (Actual conditions) ! I%'" = /355 ? / 3 6 p c m l I l Design Value l l (Design Conditions) l I$EF = 1355 2 136 pen I l l Reference ! VEP-TRD-MTE-209 1 l l l If Design Toleran=e is exceeded, SNSCC l l shall evaluate impact of test result i TSAR / Tech Spec ! on safety analysis. SMSOC may specify V 1 l that additional testing be performed.
Acceptance! ! Criteria l I i Reference ! VEP-TRD-36A I I l Design Tolerance is met /YES MO VI I Acceptance Critoria is met VYES NO
, Comments !
I i 1 Completed By r- - [ld /hiOA Evaluated By: . MA . Yest Engin 'r Recommended for Approval By : C - C MTO Engineer A.5
01 G80 SURRY PO'JEn STATION UNIT 2 CYCLE 6 STARTUP Pl!YSICS TE::7 RESULTS AHD EVALUATION SHEET . I l Test' Description Critical Boron Concentration - B In PT20.11/ APP. C Sequence Stop Ho: g Reference i Proc Ho /Section Bank Positions (Stcps) 1 RCS Temperature ('T). 547 II I Test l l Pouer Lovel (*C T.P.): O SDB: 228 CA: 228 l Other (specify): Conditionsi SDA: 228 i Belou Huclear Heating (Design) l CB: 0 CC: 228 CD: 223
'l l l RCS Temperature (
- r ) : 545' S III Bank Positions (Steps)
Test l i I Pouer Level (:( T.P.): O& SDA 226 SDB 2.26 CA: 218 1 Other (Specify): Conditionsi (Actual) I C38 O CC: 229 CD: 228 1 3 ,/,, nucfe,,. g, gp i Date/ Time Test Performed: l ll . / a/30/8 / / / 37- //'/S l l l Mens Parameter I IV l (Description) l (CO) ; Crit Boron Conc - 3 Bank In I I I I i Measured Value I (Cg @ = /277 m Test ! l Results ! I I Design value 1 (Actual Cond) 1 Cg = /2 73 f [7 pgg I Design Value ! I (Design Cond) 1 Cg = 1236 + A C 2(10 + 135. 5/14.c l ) ppm i I I Reference l VEP-FRD-HTE-209 I I I I V l FSAR/ Tech Spec l d Cg x Ca f 15,115 pcm Acceptancel 1 Criteria l Reference l FSAR Section 14.2.5 l l l Design Tolerance is met VYES _ NO l Acceptance Critoria is met : VYES NO I VI I ' Comments I dC g = -8.44 yem/ ppm for preliminary analysis I lAc" a
= (Cg)E - 1445
' act3 = -7.83 pc~/ ppm he R* / a"*/y*
U l DIO Evaluated By: bMA Completed By: dest Eligin er Recommended for Approval By b- C NFO Engineer A.6
M J ? Ga0 SUR2Y POL!ER STATION UNIT 2 CYCLE 6 STARTUP Pl!YSICS TEST RESULTS AHD EVALUATICH S!!EET I I Test Descriptions Isothermal Temperature Coefficient-D In Reference i Proc Ho / Sections PT20.11/ APP. D Sequence Step Hos 32. II I Ban!: positions (Steps) i RCS Temperature ('T): 547 Test i I Pouer Level ( *: T.P.)r 0 Conditionsl SDA: 228 SDE: 22C CA: 228 l Other (specify): (Design) l CB O CC: 228 CDs 228 i Belou Huclear Heating i I III I Bank Positions.(Steps) l RCS Temperature Cs7): gyg-Test I > I Power Level (: T.P.): 0% conditionsI SDA:?28 SDB: 238 C A r27.5 l Other (Specify): (Actual) l C3 21 CC: 228 CD 228 l Belou Huclear Heating I l l Date/ Time Test Performed: 1 i
/2/30/8/ l2 0s i l Mens Parameter i IV i (Description) 1 (-Ch" 2 3 Iso Temp Coeff - B Bank In i I I I Test i Measured Value 1 (.c.J" )g = - 6,30 gap Results ! l 7 ( C g = /gg6 )
I Design Value i I (Actual Cond) l (*f0 3 6 * 'b bf]OfhC U B */2O6 )
! I I Design value I ( =(.? )g = - 6.78 3.0 pcm/*T l (Design cond) 1 (C g = 1286 ppm) i I l Reference ! VEP-TRD-HTE 209 I I 1 I 4 V l TSAR / Tech Spec I M$ 0.44 pcm/'T gpP = -2.06 pcm/*T Acceptancel l Criteria l l l Reference ! TS 3 ' 1, VEP-TED-NTE 209 I I i
i Design Tolerance is met VYES HO VI l Acceptance Criteria is met _k'Y E S HQ I Comments 17 Uncertainty on %og = 0.5 pcm/*r (
Reference:
memorandum
. I from C. T. Snou to E. J. Lomito dated June 27, 1980 ).
1 Completed By: - . L1 f448 Evaluated By: 4 Yest E'ngideer h Recommended for Approval By a b HTO Engineer A.7
s jut. 3 1 '8350 SURRY POWER OTATIOH' UNIT 2 CTCLE 6 STARTUP PHYSICO TEST RESULTG AMD EVALUATION SHET.T I I Test Descriptions.HZP Doron Worth Coefficient Proc Ho /Section: P;28.11/ APP. E Sequence Step Mo s AJ/4 Reference l Dank Positions (Steps) l RCS Temperature ('T): 547 II I Test i ! Pouer Level (% T.P.): 0 DA: 223 CDB 223 CA: 223 I Other (specify): Conditions! CDs 22C l Below Muclear Heating (Design) i CB Moving CC: 228 '
~
I I Bank Positions (steps) i KCS Temperature (*T): 5 43 III I
. Test I
! Power Level (% T.P.): C "/-
SDA 226 SDB: 228 CA: 228 i Other (Specify): Conditionsi (Actual) 1 CB I7ov/ny CC: 22,8 CD 228 l l l Selow Oucltae Nesb/ny l Date/ Time Test Performed: 1 I I l?,/2 9/ 6/ /030 I Measured Parameter ! IV l (Description) 1 "Ca , Boron Worth Coefficient i I I I I Measured Value ! "C8 = -7. 8 3 gem /f3Om Test ! I Results ! l I Design Value I
~
l (Actual Conditions) I dcg=-8,VyIO,8V pcm/ ppm i I I Design Value i I (Design Conditions) I dca = -8. 94 2 0.84 pcm / ppm i 1 l Reference l VEP-FRD-HTE 209 I I I I I TSAR / Tech Spec 1"Cg x Cg 5 15.115 pcm V I I Acceptancel l Criteria i Reference i FSAR Section 14.2.5 I I I l Design Tolerance is met : /YES HO VI l Acceptance Criteria is met [YES Ho Comments I
.. g i
i - 1 N I M lWM Evaluated By: (} &&C Completed By> U Test Eng eer Recommended for Approval Dy C- - M[C Hr0 Engineer A,8 -
l
~
NL g I 'Se SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PHYOICO TEST RESULTS AND EVALUATION CHEET I I Test Description.: M/D Tlux Map -HZP, 3-Bank In R3forence l Proc Ho / Gection PT28.2, OP-57 Sequence Step Hot 13 II I Bank Positions (Steps) l RC3 Temperature ( ' T ) T u,3 11 Yest l I Power Level (% T.P.):=0 Conditionsi DA 228 GDB: 228 CA: 228 I Other (specify) (Dasign) ! CB : 0 CC 228 CD: 228 l Must have 2 40 thimbles I l III l Bank Positions'(Steps) l RCS Temperarure('T): ^+47'F Test l l Power Level (% T.P.): ~t 7. Conditions l CDA: 223 3DB: 227 CA: 229 l Other (Specify) (Actual) l CB -2. 3 CC : 22g CD 22F I g 4, y l Date/ Time Tests l l Performed
- 12[30[fl 14 24- 1 I l I l MAX. REL l NUC ENTHALITOTAL HEATl SUADRAMT IV l Maas Parameterl ASSY PWR l RISE HOT l TLUX HOT l PC'*ER TILT l (Description) l % DITT l CHAM TACT lCHAX TACT l RATIC l l (M-P)/P l T-dH(H) l T-S(T) l SPTR I l l l !
I I12.~[d f Pc~g*uil I I Test l Measured Valuel P l l,799 I "o *64 { l j,C /e/ 9 Raoults W N* l I a 4 *cd l l l Design Value I .ier e., r . . , I I I I ( De sign C ond s ) I {.,','g, ,';,h I HA 1 NA i $ 1.02 I I I l i I lWCAP-7905 l l l WCAP-7905 l Reference l REV. 1 1 NOME l HOME l REV.1 l l I l I I I I I I V l TSAR / Tech Spect NOME I MA l NA I MA Acceptancel l l l 1 - Criteria i i l I I l Reference l HONE I T.S. 3.12 1 T.S. 3.121 T.S. 3.12 l l ! l l 1 l_ l i I I l Design Tolerance is met : YES /MO l Acceptance Criteria is met a /YES HO VI l
- Ccznents I 1
- Oa'$, 4o k m m+ r.d , b:1 % vt <=s.dh cue aq-t A y C1w .
I 1. b y few St.rtim D.dich P,y N o : 62- 82-20 Coupleted By; b_t UDYL Evaluated By 9 4?_O 8 j 'fest En g s.Ne c t
. Recommended for Approval By : I # e8 NTO Engineer .
. A.9
JUL 3 ' 88) SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I l Test
Description:
Cntl Bank D Morth Measurement-Rod Suap Reference l Proc No /Section *PT28.11/ APP. T Sequence Step No: g4 II l Bank Positions (Steps) l RCS Temperature ('T): 547 Test .I l Pouer Level (% T.P.): 0 Conditions! ODA: 228 OD3: 228 CA: 228 l Other (specify): (Design) l CB Moving CC: 228 CD Moving l Delou Nuclear Heating i ! III l Dank Positions (Steps) ~ l RCS Temperature (*T): 516./ Test I l Pouer Level (% T.P.): O Conditionsi SDA 3.16 SD3 : J.d6 CArdQ8 l Other (Specify): (Actual) 1 CB S f,,3 C C.8 2 3 9 Belou Nuclear Heating CD :pjoj;g l Date/ Time Test Performed: I I g #2/30/61 - 2 A CO l l Mens Parameter i I (Descript.on) 1 If ; Int Morth of Cnti 3ank D-Rod Suap l l IV I I (Adj. Meas. Crit. Red Bank Test l Measured value i If = lil5 pcm Position =159 steps) Results ! I l Design value I (Adj. Meas. Crit. Ref 3ank l(Actual cond) l Igs = 115s 3 873 pcmPosition = l59 steps) i I I I l Design Value l(Design Cond) l If = l 1155 1 173 pcm (Critical Red Bank Position = 132 steps) I I I I l Reference l VEP-TRD-NTE-209. VEP-TED-36A, NTO-TI-2.2A 1 I l l If Design Tolerance is exceeded. SNSOC 1 i shall evaluate impact of test result on V I TSAR / Tech Spec l safety analysis. SNSOC =ay specify that Acceptance! I additfenal testing be performed. Criteria l 1._ l Reference l VEP-TRD-36A I l_ l Design Tolerance is met _$_YES NO VI I Acceptance Criteria is met _ImYES NO Comments ! 1 I l
- III' MJI Evaluated By: M Completed Dy'k/' Test Ingii er Recommended for Approval By : C N' NTO Engineer A.10
JUL 4 1 kg SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PI:Y ICS TEST RESULT AND EVALUATION CHEET I l Test Descriptions.Cnti Bank C Worth Measur: aent-Rod Sunp Reference l Proc No / Sections PT28.11/ APP. T Sequence Step No: g6 II l Bank Positions (Steps) l RCS Temperature ('T): 547 Test l l Pouer Level (% T.P.): O Conditionsi SDA: 220 SDB: 228 CA: 223 ! Other (specify): (Design) I CB: Moving CC* Moving CDs 228 I Belou Nuclear Heating i i III l Bank Positions (Steps) ! RCs Temperature (*T): 5456 Test l I Pouer Level (% T.P.): O Conditions! SDAsd26 SDB 3Jd C A s .12 6 i Other (Specify): (Actual) l CD:Mes,y C C : Mos.y CD s Jd6 i Belou Huclear Heating i 1 l Date/ Time Test Performed: I l l l 11/30/81 - 2243 l l Meas Parameter ! l (Description) l If ; Int Worth of Cntl Bank C-Rod Sunp l l IV i I (Adj. Meas. Cri . Ref Bank Test l Measured Value l I 7 = 7 3 3 P6'" Position =lic steps) Results l l l Design Valun 1 (Add. Maas. Crit. Red Bank l(Actual Cond) l If = 6 3 fc 125 f'" Position = Ilc steps) 1 I I I I Design Value l(Design Cond)
! If =
l 829 1 124 pcm (Crrtical Red Bank Position = 134 steps) l I I I l Reference l VEP-TRD-NTE-209, VIP-TED-36), NTO-TI-2.2A l 1 - l l If Design Tolerance is e x ce. - de d . SNSOC l I shall evaluate impact of test result on V I TSAR / Tech Spec l safety analysis. SMSOC may speci'v that Acceptancel I additional testing be performed , Criteria I I , l I Reference l VEP-TRD-36A l l 1 Design Tolerance is met : X YES hc VI I Acceptance Criteria is met X YES NO . Comments l l l _ l _ Completed By - 1 \\- (I ll f 4l M onJ Evaluated By: [- <S - d Ms Test Engi cer Recommended for Approval By : I ,g u<J NTO Engineer A.ll o
Me I I Un SURRY POWER OTATIOH UNIT 2 CYCLE 6 STARTUP PHYSICC TEST RESULTS AMD EVALUATION SHEET I I Test Descriptions Cntl. Bank A Worth Measurement-Rod Sunp Reference l Proc'Ho /Coction: PT28.11/ APP. F Sequence Step No: gg II I Bank Positions (Steps) l RC Temperature (*F): 547 Test l l Pouer Level (% T.P.): 0 Conditions! 3DA: 220 CDB: 220 CA Moving l Other (specify): (Design) l C3 Moving CC: 228 CD 228 l Belou Nuclear Heating i i III l Bank Positions (Steps) l RCS Temperature ('T): 545.7 Test l l Pouer Level (% T.P.): O Conditionsi DA JJS SDB ;238 C A Mo n ng l Other (specify): (Actual) l CB M,y,nj CC 3.a 8 CD 238 I Belos Nuclear Heating i i 1 Date/ Time Test Performed: ! l 9./ 3a /gi - a343 l l Mens Parameter l I (Description) l If ; Int Worth of Cntl Bank A-Rod Swap I l IV l I (Adj. Meas. Crit. Ref Bank Test i Measured Value l I? 515 eca Position = S6 stcPs) Results l l 1 Design Value 1 (Adj. Meas. Crit. Red Banh l(Actual Cond) 'l If = 562 i '00 rc'" Position = $8 steps) l I I I I Design Value l(Design Cond)
! If =
l 582 2 100 pcm (Critical Ref Bank Position = 104 steps) l I I I I Reference l VEP-FRD-NTE-209. VIP-FRD-36A, HTO-TI-2.2A I I I I If Design Tolerance is exceeded, SMSOC l l shall evaluate impact of test result on V l TSAR / Tech Spec 1 safety analysis. SNSOC may specify that Acceptancel I additional testing be performed. Criteria 1 l l Reference l VEP-FRD-36A I I l Design Tolerance is met N YES NO VI l Acceptance Criteria is met % YES HO , Comments l 1 1 I Completed By s' - l[t IA Evaluated By: - k' test Engin r
. Recommended -f or Approval By : CE - uxd NTO Engineer .
A.12
JIIL 3 I W SURRY POMER OTATICH UNIT 2 CYCLE 6 STAnTUP Pl!TSIC TEST RESULTO AND EVALUATIOH CHEE" I l Test
Description:
Shutdoun Bank B Worth Measurement-Rod Guap Referenco l Proc Ho /0ections PT20.11/ APP. T Sequence Otop Hos l7 II l Bank Positions (Steps) i RCs Temperature (*r): 547 Test l I Power Lovel (Z T.P.): O Conditions! CDA: 228 SDB Moving CA: 223 l Other (specify): (Design) l CB Moving CC: 220 CD* 228 l Belou Huclear Heating l l III I Bank Positions (Steps) 1 RCS Temperature (*T): 545 6 Test l l Power Level (% T.P.): O Conditions! SDAs126 S D B 8 sMo/.n y CA8 AJ'd 1 Other'(Specify): (Actual) 1 CD Nev.a3 .CC 229 CDs3J8 1 Belou Huclear Heating i I l Date/ Time Test Performed: l I I i 1 2 / u /8s col 6 l l Mens Parareter i I (Description) l I ; Int Morth of Shutdown Bank 3-Rod Suap I I IV l l (Adj. Meas. Crit. Ref 32nk Test i Measured ValueI l IN = 846 Pce Position = 130 steps) Results i I Design Value 1 (Adj. Meas. Crit. Ref Bank l(Actual Cond) i If8 =963 I Position = llc steps) i I I I 915 1 137 pcm (Critical Ref Bank l Design Value l(Design cond)
!i I$' = Position = 146 steps) i I I I I Reference ! VEP-TRD-HTE-209. VEP-TRD-36A, NTO-TI-2.2A I l l I If Design Tolerance is exceeded, SMSOC i I shall evaluate impact of test result on V l TSAR / Tech Spec l safety analysis. SHSOC may specify that Acceptancel I additional testing be performed.
Criteria i l l Reference l VEP-TRD-36A I I I Design Tolerance is met t 7' Y ES Ho VI I Acceptance Criteria is met
- _p6YES Ho
- Comments l 1 -
1 I Completed By: A A\ N(lM filVf'b Evaluated By: l* 0
~
k ' kost Eng1 eor Recommended for _ g Approval By * - f7 ~ + ~
- NTO Enginocr A.13 e
\ _ - - - - - --
JUl. 31 C40 SURRY Pot!ER STATIO( UltIT 2 CYCLE 6 STARTUP PITSICS TEST RESULTS A:(D EVALUA!!ON S!!EET I l Reference l Test
Description:
Shutdown Bank A Wo=th Measurement-Rod Swap Proc No / Sections'PT23.11/ APP. T Sequence Step No 16 II l Bank Positions (Steps) Test l RCS Temperature ('T): 547 I Conditionsi SDA Moving CD3: 228 _l Poue: Level (:( T.P.): 0 (Design) l CA: 228 i Other (specify): CBaltoving CC: 228 CD: 228 l l Belou Nuclear Heating I III I Bank Positions-CSteps) l RCS Temperature ('T): 515.V . Test i I Poue Level (( T.P.): O Conditions l CD A flavm9 SDB : 32d CA:.2 M I Othe: (Specify): (Actual) i CB N , g,,y CC: 226 l CD: QQS I Belou Huclea: Heating l i Date/ Time Test Performed: 1 l 12/31/81 00Y8 l l Mens Parameter I I (Description) l I5 l
; Int Worth of Shutdown Bank A-Rod Swap l
IV I I Test (Adj. Meas. Crit. Ref Bank l Measured Value ! Ifg = 18 34 rcm Position = 16 3 steps) Results ! l l Design Value I (Adj. Meas. Crit. Red Bank I(Actual Cond) 'l I] =5 105 7.f 159 fcmPosition = 16 3 steps) i I I I l Design '.*alue l(Design Cond) i I$ = 1057 1 2 159 pcm (Critical Red Bank Position = 167 steps) l I I I l Reference ! VEP-TRD-NTE-209, VZp-TRD-36A, NTO-TI-2.2A
'l i I
I If Design Tolerance is exceeded, SNSOC V 1 I shall evaluate impact of test result on Acceptancel l TSAR / Tech Spec I safety analysis. SMSOC may sPecify that Criteria l I additional testing be pe: formed. I Reference ! VEP-TRD-36A l l l Design Tolerance is met : A YES No VI l Acceptance Critoria is met : X YES NO Comments I l 1 1 . Completed By: - II b!N!/2 Evaluated By: [A T'e s t Engi'%er
- Recommended for sj Approval By : Cdv*
NTO Engineer A.14
~
JUL 31280 SURRY POW"n STATION UNIT 2 CYCLE 6 STARTUP PHYSIC TEST RESULTO AND EVALUATION OHEET I I Test Descriptions. Total Rod Worth-Rod Ouap Rafn=ence l Proc No /Gection: PT28.11/ APP. T Sequence Step Not N/A II I Bank Positions (Steps) 1 RCS Temperature ('T): 547 Tost ! I Power Level (% T.P.): 0 conditionsl5DA Moving GDB: Moving'CA Moving! Other (specify): (D3 Sign) l CB Moving CO: Moving CD Moving l Belou Nuclear Heat _ng I I III I Bank Positions (Steps) 1 RCS Temperatu:e (*Y): 515. 'd
. Tost ! I Power Level (% T.P.): O Conditionst 3D A :lhs..y SDD ilic /m) C A M e s-3 l Other (Specify):
(Actual) I CB : pje y,o3 CC : #1ov.43 CD: N y 1 Belou Nuclear Heating I I l Date/ Time Test Performed: I l.2./3 /$n- c5 3o l A / 3; / S g. O 1.21 g I . l Measured Pa:ameter i Q ,; Integral Worth of All Rod Banks-1 (Description) l Rod Suap IV I I I I Test i Measured Value ig= 5656 p c .w Results l !
! Design Value i I (Actual Conditions) l Im = 38 7a d 6 6 7 P C '"
1 I l Design Value l I (Design conditions) ! % g= 5893 2 589 pcm
. 1 I l Reference IVEP-TED-NTE-209,VEP-TRD-36A.NTO-TI-2.2A I I I
I II Design Tolerance is exceeded, SMSOC I i shall evaluate impact of test result I TSAR / Tech Spec l on safety analysis. SMSCC may specify V l l that additional testing ha perforned. Acceptancel l Criteria l l . I Reference ! VEP-TRD-36A I I I Design Tolerance is met : NYES NO VI l Acceptance C:iteria is met : AYES NO
. Csuments l 1
I I Lll MiO Evaluated By: '- completed By -
\ / tost Engi' ec:
) Recommended for Approval By : C.1 & >
MTO Enginoc: A.15 .
Jul. 33 g SURRY POWER ::TATIO!! UNIT 2 CYCLE 6 STARTUP PHTSICS TSST RESULTS AND EVALUATIOH SHEST I l Test Description, M/D Tlux Map - At Power. HI Calib. Reference l Proc Ho / Section: PT28.2, OP-57 Sequence Step Hon g II l Dank Positions (Steps) l RCS Temperature ('T) Tgap ) Test ! I Power Level (% T.P.):^50 Conditionsi SDA: 223 SDB: 22C CA: 228 i Other (specify) (Design) l CB 228 CC 228 CD
- I Must have 1 40 thimbles III I Bank Positions (Staps) l RCS Temperature ('T): Tp,gg :a Test i i Power Level (% T.P.): y 7,3 Conditionsi SDA: Q 26 SDB QaS C A : Md 1 Other (Specify):
(Retual) l CB :226 CC 226 CD: 188/ 1 I I k8 CNn6tes l Date/ Time Test l l Performed f ///$p 0 8/'/8 l 1 1 I l MAX. REL l HUC ENTHALITCTAL HEATl SUADRANT IV i Mens Parameteri ASSY PUR I RISE HOT I TLUX HOT IPONER !!LT l (Description) ! % DITT l CHAN TACT (CHAN TACT I ratio l l (M-P)/P l T-dHCH) l T-2(T) I 2PTR I l I I l F7.3/ArG.,'l.c71 l l Test l Measu..cd Valuel i / . 8/ T 6 i /. N d I /.0067 Results l- If0?O bi #I l ! ! l Design yalue I ster en r, ; .: 1 I i l (Design Conds)I$3 ,'",h ( j3 i NA I HA l 5 1.02 I I I I I I IWCAP-7905 l l 18'; AP-7 9 0 5 l Reference l REV.1 1 NOME I NOME I REV.1 I I I I I I l l 1 i V I TSAR / Tech SpecI HOME li f, t.ssta..rts-rnirjt:): y a stol NA Acceptancel i I l l Criteria i 1 l l l l Reference l HOME I T.S. 3.12 1 T.S. 3.121 T.S. 3.12 I I I l l 1 l i 1 I I l Design Tolerance is met YYES No l Acceptance C::itoria is met VYES HQ VI l
, Comments I
- Above Insertion Limits i
I I Completed By - I l i bMO Evaluated"By: ' l Test Eng[ineer Recommended for A[w ' v Approval By O HTO Engineer - A.16
JUl. 3 ! Ig() SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PHY:;ICS TEST RESULTS AND EVALUATION SHEET I l Test Description 8 M/D Flux Map - At Power. HI Calib. Reference ! Proc Ho / Section: PT28.2, OP-57 Sequence Step No: 4] II l Bank Positions (Steps) ! RCS Temperature (*T) Tftgp 11 Test l l Power Level ( *: T.P.):-60' Conditions! SDA: 220 SDB 228 CA: 228 i Other (sPecify) (Design) I CB : 228 CC 228 CD: x l Must have 2 40 thimbles
! I III I Bank Positions- (Steps ) l RCS Temperature (*T): TAge *:
Test I l' Power Level (:: T.P.): $ 7. 0 2. Conditions l SDA:23F SDB: J. 2 8 CA:a26 l Other (SPecify): (Actual) l CB : .236 CC 's 128 CD : 860/177 I I l '/8 th;m blus l Date/ Time Tes*.: l l Performed: j f j/g g - l109 I I I I l MAX. REL I NUC ENTHALl!OTAL HEAT! EUADRANT IV l Mens Parameterl ASSY PWR l RISE HOT I TLUX HOT IPOMER TILT I (Description) l :: DITT l CHAN TACT !CHAN TACT I RATIC I l (M-P)/P l T-dHCN) l T-9(T) l 2PTR I I _ l i I l l-12 / Ar/' 4 s.so l l l. Test i Measured Valuel f,7c2 1. co M 20.4 I f.'/26 1 l Results i ITR /., P3 s i i l l Design Value Iste::.,p. . . , I I I I (Design Conds ) l {, 'j ((3
,, i NA I NA 1 5 1.02 l I l l I I IWCAP-7905 l 1 IWCAP-7905 l Reference ! REV.1 i NOME I NONE I REV.1 I l l I I
. I I I I I V l TSAR / Tech Spec l NONE Ir", 1.ssct.. (t.r))l jc:) : y xt:)] NA Acceptancel l [ l l Criteria l l l 1 I l Reference i NOME . I T.S. 3.12 1 0.5. 3.121 T.S. 3.12 I I I I I I I I I I I
I Design Tolerance is met : X YES N0 l Acceptance Criteria is met : X YES XO VI I , Comments I
- Above Insertion Limits i
I I completed By: - lL'!Mdd Evaluated By: - j Test Engiiper
) Recommended for Apprcval By : C 2 +/
fr C NTO Sngineer A.17 O
M 3j g SURRY POWER STATICH UNIT 2 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATICH SHEET I l Test Description M/D Tlux Map - At Pouer, HI Calib. kegerence l Proc Ho / Section: PT28.2. OP-57 Sequence Step Hos % II I Bank. Positions (Steps) l RCS Temperature ('T) Tagg al Test l l Power Level (% T.P.) -70 Conditionsl SDA: 228 SDB: 228 CA: 228 I Other (specify) (Design) I CB : 228 CC 228 CD:
- 1 Must have 2 40 thimbles i I ZII l Bank Positions (Steps) l RCS Temperature ('T): Tiv "'
Test i I,Pouer Level (% T.P.): 66 % Conditions l SDA: 226 SDB: 226 CA:220 1 Other (SPecify): (Actual) l CB 8220 CC 3 220 CD IOY l l I 'l8 T*himbler . I Date/ Time Test: l l Performed: I///BA 1807 l l 1 l l MAX. REL l MUC ENTHALITOTAL HEA"! QUADRANT IV I Mens Parameter l ASSY Pt!R l RISE HOT I TLUX HOT lP0"ER TILT l (Description) l % DITT l CHAN TACT ICHAS TACT I RATIO I I (M-P)/P 1 T-dHCH) l T-C(T) 1 SPTR I I I i 1 1 l.6.v--CgwJl l l Test l Measured ValueI
$** l
/- 2 1 /M i /. OO Y8 Results l l d'# I I l l Design Value I sto: ter 7, ; .9 l l l l ( De sign Conds ) l N".'",h (;'3 i NA- I HA l 5 1.02
-1
- I I_ I I l lWCAP-7905 l 1 IWCAP-7905 i Reference i REV. 1 1 MONE I XOME I REV. 1 1 1 I I I I I I I I 18g: 1.ssci..:ct-rnirjt:1 2 21 8 nA V I TSAR / Tech Speei NOME 9.! , ac: 1 Acceptancel l l I I Criteria 1 i l l l l Reference l HONE I T.S. 3.12 IT.S. 3.12 1 T.S. 3.12 I I I I I I I I I I l Design Tolerance is met S MO l Acceptance Criteria is met W ES NO VI l Comments l
- h.ove Insertion Limits l
I . I Completed By
- f--N NY Evaluated'By: ~
/' M Test Eng cer Recommended for M Approval By : C1 M '
HTO Engiace: I
- A.18
b N 3 1 19?) SURRY POWER STATION UNIT 2 CYCLE 6 STARTUP PHYSICS TEST RE::ULTS AND EVALUATION SHEET I l Test Description t M/D Tlux Map - HTP, ARO, Eq. Xe. Map Reference l Proc Ho / Sections PT28.2, OP-57 Sequence Step Hos 44 9 II l Bank Positions (Steps) l RCS Temperature ( ' T ) s T ggg 11 Test ! l Pouer Level (% T.P.): 100 Conditions! SDA: 228 SDB: 228 CA: 228 I Other (specify): Eq. Xe. (Des.qn) d l CB 228 CC 228 CD
- l Must have 2 40 thimbles ~
I I III I Bank Positions -(Steps ) l RCS Temperature ('T) 7ggp f l Test l 1.Pouer Level (% T.P.): loo y, Conditions! SDA 326 SDB8 JdS CA 226 l Other (Specify): (Actual) l CB :226 CC *22S CD 226 1 1 Date/ Time Test l 47 Thimbles l Performeds 3 lso /82 l 3 4'l i I i l l MAX. REL 1 MUC ENTHALITOTAL HEATI SUADRANT IV l Mens Parameterl ASSY PWR I RISE HOT l TLUX HCT IPOW R TILT l (Description) I % DITT l CHAM TACT lCHAN TACT l RATIO l I (M-P)/P l T-dHCM) 1 T-9(T) l 2PTR I I I I I I I m t., t;,; i.o A I I I Test i Monsured valuel /,387 l /,7eg i /,0053 Results ! 8 6 71 4 k-sv,c l l l Design Value i stet ter r .g . , I l l l (Design Conds)l . '" h ,'j3 i NA l NA I $ 1.02 I I I I I l lWCAP-7905 l l lWCAP-7905 l Reference 1 REV. 1 1 NONE l HONE I REV. 1 I I I I I 1 i i i i V 1 TSAR / Tech Spec l NOME fr", 1.sset..*tt-r>>lrjtz) : 1pli . rtz)I NA Acceptancel l i I l Criteria I I i i I l Reference ! NONE . I T.S. 3.12 i T.S. 3.121 T.S. 3.12 I I I I I I I I I I l l Design Tolerance is met
/ YES M0 l Ac ce p tant:c criteria is met V YES NO VI l
+ Comments I r Above Insertion Limits i I I Completed By. - . M1 Evaluated"By: '
'fest Enginch.
l/ Recommended for f Approval By : I w*1 MTO Engincer i A.19
I f , ,
, N 31 %
SURRY PO!!ER STATION UNIT 2 CYCLE 6 STARTUP Pl!Y::ICC TEST RESULTO AND EVALUATION Cl!EET I l Test Descriptions.RC Flou Measurement R3forence l Proc Ho /Section ST-52 sequence step Ho e go II l Bank Positions (Steps) l RC3 Temperature ('T) Tagg Il Test 1 i Power Level (% T.P.):95 +5/-0 Conditions! SDA: 223 SDB: 228 CA: 228 1 Other (specify): (D3 sign) l CB 228 CC: 228 CDs AR l
- l I III I Bank Positions (Steps) l RCS Temperature ('T): f71*F Test ! I Pouer Level (% T.P.): /Co */o Conditionsi SDA: LIB sD3 LI6 CA: E28 I Other (specify):
(Actual) l CB '2;26 CC: 223 CDs g g_ l ger . 20,Jg., mu;(Q l Date/ Time Test Performed 1 ( l i .2 r-a2 / isc i l l Maas Parameter i I'? I (Description) l Trots , Total RCS T1ou Rate I i l i
=
Tost i Mearured value l T773u 3C.6f(06 Spn Rasults l ! l Design value i , I (Actual cond) ! Not Applicable l l l Design Value l l (Design Cond) l Hot Applicable
! I l Reference l Hot Applicable
! I I I ..
I TSAR / Tech Spec l Tgg / 1.02(mens uncerty) 2 255,500. gym V l l A088Ptancel I FSAR Section 4.1.3; 1.etter from J.H. Terguson (*.'epco) to Criteria l Reference l H.R. Denton (:RO) dated April :S. 1981 (Serial !:o. 232); [ l Letter from C.:!. Stallines (Vepco) to I.O. Case (:EC)
; g dated November 16, 1977 (Serial ::o. 516).
I I Design Tolerance is met i 1 YES HO , VI I Acceptance Criteria is met X YES HO I
. Canments !
I I I . Completed By: \* Evaluated By' - NA
" Test tngineer l Recommended for J
Approval By,p
- 1N' N l 4000' Engine ,r A.20 .
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