abstract - inldigitallibrary.inl.gov vol-23.pdf · abstract about 10 hours after the march 28, 1979...

69
." . .' GEND-INF--023-Vol.3 DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, or implied, or assumes any legal liability or responsi- bility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Refer- ence herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise docs not ncccs'J8rily' constitute or imply its endorsement, recom- mendation, or favoring by the United States Government or any agency thereof. The views and opinions ,f authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof. DE84 004115 DATA INTEGRITY REVIEW OF THREE MILE ISLAND UNIT 2 HYDROGEN BURN DATA Jim K. Jacoby Ralph A. Nel son Charles L. Nalezny Ron H. Averill Published September 1983 EG&G Idaho, Inc. Idaho Falls, Idaho 83415 Prepared for the U. S. Department of E.nergy . Three Mile Island Operatlon Offlce Under DOE Contract No. DE-AC07-76ID01570 H'\ I U OF TillS OOCI:H?t:ift IS Urlt.lMI It !lIS 1 HlflUI,9r, 2

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Page 1: ABSTRACT - inldigitallibrary.inl.gov VOL-23.pdf · ABSTRACT About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen

." .

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GEND-INF--023-Vol.3

DISCLAIMER

This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, exprcs.~ or implied, or assumes any legal liability or responsi­bility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Refer­ence herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise docs not ncccs'J8rily' constitute or imply its endorsement, recom­mendation, or favoring by the United States Government or any agency thereof. The views and opinions ,f authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

DE84 004115

DATA INTEGRITY REVIEW OF THREE MILE ISLAND UNIT 2 ~ HYDROGEN BURN DATA

Jim K. Jacoby Ralph A. Nel son

Charles L. Nalezny Ron H. Averill

Published September 1983

EG&G Idaho, Inc. Idaho Falls, Idaho 83415

Prepared for the U. S. Department of E.nergy .

Three Mile Island Operatlon Offlce Under DOE Contract No. DE-AC07-76ID01570

H'\ ~ I U OF TillS OOCI:H?t:ift IS Urlt.lMI It !lIS 1 HlflUI,9r,

2

Page 2: ABSTRACT - inldigitallibrary.inl.gov VOL-23.pdf · ABSTRACT About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen

ABSTRACT

About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen burn occurred inside the Reactor Building. This report reviews and presents data from 16 channels of resistance temperature detectors (RTDs), 2 steam generator pressure transmitters, 16 Reactor Building pressure switches, 2 channels of Reactor Building pressure measurements, and measurements of Reactor Building hydro~ gen, oxygen, and nitrogen concentrations with regard to their usefulness for determining the extent of the burn and the resulting pressure and temperature excursions inside the building.

i i

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FOREWORD

At the request of the TMI-2 Technical Integration Office, a review was conducted by the EG&G Idaho Loss-of-Fluid Test (LOFT) Data Integrity Section

of selected TMI-2 hydrogen burn data. The LOFT Data Integrity Section is

responsible for qualification of LOFT data following each LOFT experiment.

Although other physical evidence is available related to the extent of burn and overpressure damage, estimation of the peak temperature reached during the burn from physical damage effects is difficult because of the apparent short duration of the high-temperature transient. Consequently, intepretation of Reactor Building temperature, pressure, and gaseous com­

position data is an important element in understanding what actually hap­pened. It is important to know what peak spatial average temperature was

reached so that the amount of hydrogen produced from zirconium-water reac­

tion during the accident can be estimated.

; ; i

Page 4: ABSTRACT - inldigitallibrary.inl.gov VOL-23.pdf · ABSTRACT About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen

,'-- "

ACKNOWL(DGMENTS

We would like to thank the following EG&G Idaho employees. James W. Mock provided tabulated data for 16 Reactor Building resistance temperature detectors (RTDs). B. Mack Galusha and J. Bruce Marlow were instrumental in entering the RTD data onto the Idaho National Engineering Laboratory'Cyber computer. Douglas L. Reeder and Lorenzo D. Goodrich provided many helpful comments.

i v

Page 5: ABSTRACT - inldigitallibrary.inl.gov VOL-23.pdf · ABSTRACT About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen

CONTENTS

ABSTRACT •••••••• ".................................................... i·i

FOREWORD ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• iii

ACKNOWLEOQJIENTS ••••••••• ., •••••••••••••••••••••••••••••••••••••••••••• iv

I NTRODUCT I ON ••••••••••••••••••••••••••••••••••••••••••••••••••••••••.

PRESENTATION OF DATA •••••••••••••••••••••••••••••••••.••••••••••••••. 3

PERTINENT OBSERVATIONS •••••••••••••••••••••••.••••.••••••••••••.••••• 4

Temperature •••• ~ .•••••.•••••••••.••••••.••••..•.....•.•• " . . . . • . . 4

CREDIBILITY OF DATA •••••••••••••••••••••••••••••••••.••.••••••••••••• 5

Temperature ••••••••••..•••••.• c.................................. 5

Pressure ........................................................ , 5

CONTAINMENT BUILDING HYDROGEN AND OXYGEN DATA •••••••. ;................ 7

CONCLUSIONS •••••••••••••••••••••••••••••••••••••••.•••••••••••••••••• 8

REFERENCES ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 8

APPENDIX A--RTD AND OTSG PRESSURE INDICATIONS DURING THE TMI-2 HYDROGEN BURN ••••••••••••••••••••••••••••••••••••••••••••••••••• 9

APPENDIX B--TMI-2 OTSG PRESSURES {DIGITAL} 13~44:30 TO 14:00:03, 28 MARCH 1979 .•..•••••.•.•...•..•••••••............••. 29

APPENDIX' C--STRIP CHART RECORDS •••••••••• 'v.......................... 39

APPENDIX D--TMI-2 ALARM PRINTER PRINTOUT SEQUENCE FOR 4 PSIG REACTOR BUILDING PRESSURE CHANNELS AND 28 PSIG ENGINEERED SAFEGUARDS BUILDING SPRAY ACTUATION PRESSURE SWITCHES ••••••.•..• 43

APPENDIX E--REACTOR BUILDING ATMOSPHERE HYDROGEN, OXYGEN, AND NITROGEN DATA •••••••••••••••••••••••••••••••••••••• 'l •••• tl. to..... 47

APPENDIX F--INVESTIGATION OF THE TMI HYDROGEN PHENOM~NA OF MARCH 28, 1979 ••.•••••••.••••.••.....•••. 1................... 51

APPENDIX G--INVESTIGATION OF HIE TM! HYDROGEN PHENOMENA OF MARCH 28, 1979 ••••••••••••••••••••.•.•...••••.•.••.•...•..•.••••. 59

APPENDIX H--REACTIMETER ZERO OFFSET SHIFTS •••••••..•••••••.•••••••..• 63

v

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DATA INTEGRITY REVIEW OF THREE MILE ISLAND UNIT 2 HYDROGEN BURN DATA

I NTRODUCTI ON

All 16 resistance temperature detectors (RTDs) located inside the Three Mile Island Unit 2 (TMI-2) Reactor Building indicated a peak temperature following the hydrogen burn of less than 200°F. Using the equation of state for air, and the peak pressure (28 psig) shown by strip chart recorders dur­ing the burn, a peak Reactor Building spatial average temperature of about l200°F may be calculated. In addition, physical damage to organic materials

lnside the Reactor Building indicates that temperatures greater than 450°F

were reached. Calculations of the amount of hydrogen burned from oxygen depletion data in the containment atmosphere are not entirely consistent with any of the temperature or pressure data. The purpose of this investi­gation, therefore, is to determine which measurements are reliable indi­cators of what actually happened in the TMI-2 Reactor Building during and immediately following the hydrogen burn. A list of measurements reviewed is given in Table 1.

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TABLE 1. LIST OF DATA REVIEWED,

Resistance Temperature Detectors

AH-TE-50l7, No. 1 Primary Shield AH-TE-50l8, No. 2 Primary Shield AH-TE-50l6, No.3 Primary Shield AH-TE-50l9, No.4 Primary Shield AH-TE-50l5, No. 1 Supply Air AH-TE-5027, No.2 Supply Air AH-TE-50l3, Ambient--Impingement Barrier AH-TE-5010, Ambient--Sump area AH-TE-50ll, Ambient--let down cooler area AH-TE~5012, Ambient--drain tank area AH-TE-5020, Ambient--353-ft elevation AH-TE-502l, Ambient--353-ft elevation AH-TE-5023, Ambient--330-ft elevation AH-TE-5022, Ambient--330-ft elevation AH-TE-50l4, Amoient--310-ft elevation AH-TE-5088, Ambient--3l0-ft elevation

Once Through Steam Generators Pressures

OTSG Loop A steam pressures SP-6A-PTl or SP-6A-PT2 OTSG Loop B steam pressures SP-6B-PTl or SP-6B-PT2

Reactor Building Pressures (Strip Chart Records)

BS-PT-4388-1 BS-PT-4388-2

Reactor Building Pressure Switches (4 psig)

BS-PS-3570 BS-PS-3571 BS-PS-3572 BS-PS-3S73

Emer~ency Suppression Building Spray Switches (28 psig)

BS-PS-3253 BS-PS-3254 BS-PS-3255 BS-PS-3256 BS-PS-32S7 BS-PS-3258

Reactor Building Atmospheric Hydrog€!n and Oxygen Measurements

2

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PRESENTATION OF DATA

Data from 16 Reactor Building RTUs and 2 once through steam generators

(OTS6) pressure transducers listed in Table 1 have been entered into the INEL Cyber computer system under the file ndme TMIDATA, IO=BM6. Plots of these data are contained in Appendix A. Note that the OTS6 pressure _lots are designated as "qualified" data and the Reactor Building RTD data are designated "trend" data. The qualified designation indicates that the data are considered reliable indicators of the phenomena measured within the stated accuracy. The trend designation indicates that the data are ndt always reliable indicators of the phenomena measured and are useful only

for discerning trends during some interval of the measurement.

Time sequenced data from the OT5G pressure transducers are given in

Appendix B, and Appendix C contains strip chart records of the Reactor Building pressure as indicated by BS-PT-4388-l and -2. Appendix D contains a record of the actuation and reset times for the Engineered Safety Features Reactor Building Pressure Switches, and Appendix E gives a compilation of Reactor Building atmosphere hydrogen, oxygen, and nitrogen analyses. Appendix F is a memorandum concerning the hydrogen phenomena, Appendix 6 is

an interpretation of OTSG pressure data, and Appendix H is a report on the

reactimeter zero offset shifts.

3

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PERTINENT OBSERVATIONS

~erature

Scorched paper indicated that Reactor Building gas temperatures had reached at least 450°F. 1 Polymers and numerous other objects were found that indicated temperatures of 480°F and 1~5 to 500°F respectively. The wide variation in indicated material temperatures reported in Reference 1 is probably due to variations in thermal diffusivities, surface area to volume ratios and heat capacities, and moisture content or moisture film thick­nesses which existed on the samples just prior to the burn. Also, there is evidence, as reported in Appendix F, that the containment air circulation system was operating continuously during the accident. Since the Reactor Building atmosphere turnover time (free volume divided by the volumetric

flow rate) was about nine minutes, it is unlikely that there could have been high local concentrations of hydrogen to account for the variations in mate­

rial temperatures observed in Reference 1. In addition, Reactor Building pressure data indicate that the average Reactor Building gas temperature had decreased to between 220 and 240°F within two minutes of burn initia­tion and to between 190 and 210°F within four minutes. All these ob~erva­tions point to a maximum temperature during the transient of higher than 450 to 500°F.

4

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...

CREDIBILITY OF DATA

Temperature

During the hydrogen burn transient, the Reactor Building RTD data plotted in Appendix A are only worthwhile for estimating trends. The data

. points were too far apart in time (6 min) to give a detailed understanding of the rapid heatup and coo1down transients during the burn. The RTO data are worthwhile for substantiating that a burn did occur, for indicating relative effects in various parts of the Reactor Building, and for studying more gradual temperature changes during the accident sequence.

Pressure

The OTS6 steam pressure data when interpreted as suggested in Appendix 6 are reliable within the specified accuracy of the instruments

(±2.7 psi for the sum of deadband, repeatability, hysteresis, and drift) for estimating the change in containment pressure during the period from

burn initiation, 13:49:12, reactimeter time to 13:51:00 reactimeter time.

Since the response time of the pressure transducers (1.17 s) is somewhat slow, and also since the sampling rate (1 point every 3 s) is low, the peak value of containment pressure was missed. A test is now underway to con­firm that the peak indicated value is within the instrument error band (±2.7 psi) of the actual peak pressure. Back extrapolating the pressure decrease curve to its intersection with the linear pressure rise curve cer­tainly provides a conservative estimate of the peak containment pressure. 2

As explained in Appendix F" three out of the four OTS6 pressure trans­

ducers were not affected by buildup of water on the containment floor and the general agreement of the OTS6 pressure transducers indicates a high degree of confidence. The time shift between transducers could be partly due to one transducer being subR~rged. (See Appendix B).

The trip and reset pressures indicated for 28 ps;g and 4 psig engi­neered safety features pressure switches in Appendix 0 are accurate .within

5

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±l.O psig for the 28 pSig switches and ±O.2 psig for the 4 pSig switches. This accuracy is attributable to the accuracy of the Heise gauges used for calibration.

Additional credibility is lent to all the pressure data including the strip chart recorders BS-PT-4388-l and -2, because of the general agreement of peak indicated pressures. However. since timely calibration data and operating characteristics of BS-PT-4388-l and -2 and their associated strip chart recorder are not available, it is not possible to put numerical limits on the uncertainty in the chart recorder prp,ssure data.

6

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CONTAINMENT BUILDING HYDROGEN AND OXYGEN DATA

The data reported in Appendil< E are not reliable for determining the amount of hydrogen burned because (a) the accuracy of the analytical tech­niques is unknown, (b) the representativeness of the samples is unknown,

(c) the amount of oxygen and hydrogen produced by radiolysis of th~ Reactor Building sump water is unknown, and (d) the amount of oxygen consumed and

hydrogen produced by corrosion of Reactor Building components is unknown.

7

,1 ,I

-.", j

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CONCLUS IONS

Based on instrument specification data and agreement between multiple redundant measurements, the OTSG steam pressure data, when interpreted as described in Appendix G, and 16 engineered safeguards pressure switches provide a reliable indication of Reactor Building pressure during the hydrogen burn.

Due to the low sampling rate, the RTD data are suitable only for esti­mating temperature trends at different locations in the building during the hydrogen burn. The RTD data should not be used as actual values for the temperatures that ~ere present during the burn.

The containment atmosphere gas composition data shown in Appendix E are not reliable for determining the amount of hydrogen burned.

1.

REFERENCES

H. W. Schutz, P. K. Nagata, Estimated Temperatures in the TMI-2 Con­tainment Building during the 1979 Accident, GEND-INF-023, Vol. 2, August 1982.

2. J. O. Henrie, A. K. Postma, ~na1ysis of the Three Mile Island LTMI-2) Hydrogen Burn, GEND-INF-023 Vol. IV. March 1983.

8

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APPENDIX A RTD AND OTSG PRESSURE INDICATIONS DURING THE

TMI-2 HYDROGEN BURN

Page 15: ABSTRACT - inldigitallibrary.inl.gov VOL-23.pdf · ABSTRACT About 10 hours after the March 28, 1979 loss-of-coo1ant accident began at Three Mile Island Unit 2 (TMI-2), a hydrogen

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Figure A-2. OTSG-8 steam pressure (qualified).

11

1000 INEL 3 3639

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12

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13

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14

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Figure A-10. West stairwell ambient air temp 330 R-5 (long term trend).

15

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16

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Figure A-14. Top ceiling ambient air temp 353 R-15 (long term trend).

17

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OO¢ " ¢OOO

50 100 150

Time (min) after 13:24:0028 March 79

200 INEL33641

Figure A-15. Reactor coolant drain tank ambient air temp 282 (short term trend) •

LL 0

Q) '-~ -CG ..... Q) a. E Q) I-

175

150

125

100

75 o

AH-TE-5012

~ \

~ "-. .. ~-

1000 " 2000

Time (min) after 15:44:0028 March 79

3000

INEL33625

Figure A-16. Reactor coolant drain tank ambient air temp 202 (long term trend) •

18

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..

130 AH-TE-5011

120 u:-o

Q) ... ::J -f!'! Q) a. E Q)

~ 110

100 o

()

<>

<> ¢

¢ ¢

<> Q

IO¢ ¢

¢ <>

<> ¢ ¢

~~ ~

¢ ¢¢O

¢ ¢<;: <>¢

50 100 150

Time (min) after 13:24:00 28 March 79

<>O¢ 0<>

200

INEL 3 3632

Figur2 A-17. Letdown cooler ambient air temp 282 (short term trend).

140~--------------r---------------~------------~ AH-TE-5011

u:- 120 0

Q) ... ::J -t13 .... Q) a. E Q) ~

100

80~------------~--------------~--------------~ o 1000 2000 3000

Time (min) after 15:44:0028 March 79 INEL 3 3634

Figure A-lB. Letdown cooler ambient air temp 2B2 (long term trend).

19

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ii:" 0

CD ~

~ -as ~

CD Q.

E CD ~

140 AH-TE-5010

130

120

110 lA

100 o

<i>

<i>

<> <i> 0

<> <>

It\

<> ()

0 <i> <> ()

O~ ~ O<i>¢A

VO<>( O<>O<i><i>O<i>

50 100 150

Time (min) after 13:24:0028 March 79

200

INEL33646

Figure A-19. Sump pump ambient air temp 282 pump room (short term trend).

140 AH-TE-5010

ii:" 120 0

CD ... ::l -as "-CD Q.

E CD ~

100

-80

o

"

~ ~.

v v I~

1000 2000

Time (min) after 15:44:0028 March 79

3000 INEL33622

Figure A-20. Sump pump ambi mt air temp 282 pump room (long term trend).

20

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101

~

.,

u:-0

CD ~

::l -to ~

CD a. E CD ~

160 AH-TE-5013

140

120 V"o

100 o

<)

<>

<>¢

0

-, ~"

..;,

~ <>

<> <> <> <)

~ 0< ¢'6,.

~v<>

O()~ 0<>00

50 100 150

Time (min) after 13:24:00 28 March 79

<> :.. -0

200

INEL 3 3627

Figure A-21. Impinge bar ambient air temp 282 (short term trend).

175 AH-TE-5013

150

LL 0

CD ..... ::l

125 -to A

..... CD a. E CD ~

100 ~ ~-... ~

75 o 1000 2000 3000

Time (min) after 15:44:0028 March 79 INEL 3 3526

Figure A-22. Impinge bar ambient temp 282 (long term trend).

21

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--\------------------------------------------------------------- -----

I

(L 0

CD ~

::l -I1S ~

CD a. E CD I-

140

120

100

80

eo o

AH-TE-!5027

()

()

<>

¢ ¢ .:> A

~

() ~

()

.. ~ <>()

()<>o ..... ...... >

0

<> Q

¢ ()<>¢ . <:

O() -OOOO¢

50 100 150

Time (min) after 13:24:0028 March 79

200

INEl3 3637

Figure A-23. Ail'cooler plenum outlet temp 305 R-OI (short term trend).

150

_CD .... ::::J

a; 100 ~

CD a. E CD I-

50

AH-TE-5027

~

o

" IA

~

\~ ~

10100 2000

Tim€: (min) after 15:44:00 28 March 79

3000 r;NEL 3 3631

Figure A-24. Aircoo1er plenum outlet temp 305 R-Ol (long term trend).

22

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.,

~.

u: 0 -CD .... ::J ... CIS .... CD a. E CD t-

140 AH-TE·5015

120

100

~ 80

60 o

0

00 0

0 "'0

p 0

0 0

50

,-

0.6. QI)

< 0

<> 0

6 0 00

0'0 . 00 0000

100 150 200

Time (min) after 13:24:0028 March 79 INEL 3 3638

Figure A-25. Aircooler plenum outlet temp 319 (lung term trend).

LL 0

CD .... ::J -CIS .... CD a. E Q)

t-

150 ~

AH-TE-5015

125

100

~

75

50 o

~

IAi\

I \~

I ~ 1000 2000 3000

Time (min) atfter 15:44:00 28 March 79 INEL 3 3633

Figure A-26. Aircooler plenum outlet temp 319 (long term trend).

23

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G:' 0

Q) ~

::J -as ~

Q) c. E Q) ~

107.0 AH-TE-5019

106.5

106.0

~ 105.5 o

0

..

00

0 00

... --~" .. - .-.--... - .- ... - .. ~.- -.," .

0 O()()() ()

0

0 0 0 O(

~ <> 00

0 0 0

50 100 150

Time (min) after 13:24:0028 March 79

00

0

0

00

200

INEL 3 3629

Figure A-27. Primary shield ambient air temp 282 (short term trend).

G:' 0

Q) .... ::J -as '--Q) c. E Q) ~

115 AH-TE-5019

110

105

100 L-_______ "--__ ,

o 1000 2000

Time (min) after 15:44:00 28 March 79

3000

INEL 3 3624

Figure A-28. Primary shield ambient air temp 282 (long term trend).

24

..

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"'

~.

<.

101.5 AH-TE-5016

LL 107.0 0

a> ... ~ .... ns L-

a> a. E a> ~

106.5

¢¢ ¢¢ ¢¢

106.0 o

0

0 ¢¢ ¢ ¢ ¢

<> ¢ ¢ ¢ ¢ <:

AA

¢¢

¢¢ ~

50 100 150

Time (min) after 13:24:00 28 March 79

¢

000

<> 0

200 INEL 3 3642

Figure A-29. Primary shield ambient air temp 282 (short term trend).

115 AH-TE-5016

LL 110 0

a> ... ~ ... ns ... a> a. E G.l ~

105

100~--------------~--------------~------------~ o 1000 2000 3000

Time (min) after 15:44:00 28 March 79 INEL 3 3618

Figure A-30. Primary shield ambient air temp 282 (long term trend).

25

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u:-0

Q) ~

:l -as ... Q) a. E Q) t-

111.5 AH·TE"5017

111.0

110.5

00 pO 0 110.0

109.5 o

Q Q

0

".' .. ;~. '.

()

0 Q IQ QQQQ

~ 0 0 0 000 0 (l

~I>

50 100 150

Time (min) after 13:24:0028 March 79

<>

0

()

0 00

()o

200

INEL 3 3644

Figure A-31. Primary shield ambient air temp 282 (short term trend).

120 AH.TE.5017

iL 115

0

Q) ... :J -co ... Q) a. E Q) t-

110

105L---------------~--,----------------~--------------~

o 1000 2000 3000

Time (min) after 15:44:00 28 March 79 INEL 3 3628

Figure A-32. Primary shield ambient air temp 282 (long term trend).

26

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.,.

. ~.

110.0 AH-TE-5018

<> ~ <>

<> <>

~ 109.5 .'. .'

0

<> Q) ... ::J <><> <> <> ... as ... <><><> <><> <> Q) Q. () ) <> ()( () E Q) I-

109.0 vvv

108.5 o

<> <> v

0 O()O

50 100 150

Time (min) after 13:24:00 28 March 79

I 200

INEL33647

Figure A-33. Primary shield ambient shield air temp 2B2 (short term trend),

115r-------------~--------------~--------------~ AH·TE·5018

~ o .

Q) .... ::J ~ 110~----------------------------~--------~~~~~~------------------------~ .... Q) Q.

E Q) I-

105~------------~------------~------------~ o 1000 2000

Time (min) after 15:44:00 28 March 79

3000 INEL 3 3623

Figure A-34. Primary shield ambient air temp 2B2 (long term trend).

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APPENDIX B TMI UNIT 2

OTSG PRESSURES (DIGITAL) 13:44:30 to 14:00:03, 28 March 1979

29(30

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APPENDIX B TMI UNIT 2

OTSG PRESSURES (DIGITAL) " 13:44:30 to 14:00:03, 28 March 1979

OTSG-A OTSG-B Pressure Pressure

Time (ps ig) {Qsig~

13:44:30 1.06274 267.037 13:44:33 1. 24927 267.219 13:44:36 1.24927 267.219 13:44:39 1.34253 267.037 13:44:42 1.24927 267.037

13:44:45 1. 24927 267.037 13:44:48 1.24927 267.037 13:44:51 1.34253 266.854 13 :44: 54 1.43535 266.671 13:44:57 1.62207 266.671

13:45:00 1. 71533 266.671 13:45:03 1.43555 266.671

~ 13:45:06 1. 52881 266.671 13:45:09 1.43555 266.854 13:45:12 1.43555 267.037

13:45:15 1.24927 266~334 13 :45: 18 1.15601 267.037 13:45:21 1. 06274 267.037 13:45:24 1. 15601 267.037 13:45:27 1.06274 266.854

13:45:30 1.06274 266.671 13:45:33 0.87622 266.671 13:45:36 0.87622 266.489 13 :45: 39 0.87622 266.489 13:45:42 0.87622 266.489

13:45:45 0.87622 266.213 13:45:48 0.78296 266.123 13:45:51 0.78296 266.123 13:45:54 0.87622 266.123 13:45:57 0.78296 265.941

13:46:00 0.87622 265.941 13:46:03 0.68970 265.941 13 :46: 06 0.68970 265.941 13:46:09 0.87622 265.941 13 :46: 12 0.87622 266.123

31

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OTSG-A OTSG-8 Pressu~e Pressure

Time {Qsig} (psig)

13 :46: 15 0.87622 266.123 13 :46: 18 0.87622 266. 123 13:46:21 0.87622 266. 123 13:46:24 0.87622 265.941 13:46:27 0.87622 265.941

13:46:30 0.78296 . 265.941 13:46: 33 0.87622 265.941 13:46: 36 0.68970 265.941 13:46: 39 0.87622 265.941 13:46:42 0.87622 266.123

13:46:45 0.87622 265.941 13:46:48 0.87622 266.123 13:46:51 0.87622 265.941 13:46:54 0.87622 265.941 13:46: 57 . 0.87622 265.941

13:47:00 0.87622 265.941 13 :47: 03 0.87622 265.941 13:47:06 0.876 265.941 13 :47: 09 0.876 265.941

13:47:12 0.876 265.941 13:47:15 1.063 266. 123 13:47:18 0.876 266.123 13:47:21 0.969 265.941 13:47:24 0.876 266.123

13:47:27 0.969 266. 123 13:47:30 0.969 266. 123 13:47:33 1.063 266. 123 13:47:36 1. 156 266.306 13: 47: 39 0.969 266.215

13:47:42 1.063 266.305 13:47:45 1.249 266.489 13:47:48 1.436 266.489 13:47:51 1.249 266.489 13:47:54 1.063 266.489

13:47:57 1.136 266.489 13:48:00 1.249 266.489 13:48:03 1.249 266.489 13:48:06 1. 2,~9 266.489 1.3:48:09 1.249 266.306

.;

32

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OTSG-A OTSG-8 Pressure Pressure

Time (esig) {~si9)

~ 13 :48: 12 1.249 266.489 13:48:15 1.249 266.489 13 :48: 18 1.249 266.489 -13:48:21 1.249 266.489 13:48: 24 1.249 266.306

13:48:27 1.249 266.306 13:48: 30 1.249 266. 123 13:48:33 1.436 266.123 13 :48: 36 1.436 266. 123 13:48:39 1.529 266.123

13:48:42 1.529 265.941 13:48:45 1.436 265.941 13:48:48 1.529 265.941 13:48:51 1.529 265.849 13 :48: 54 1.622 265.758

13 :48: 57 1.715 265.758 13:49:00 1.715 265.758 13:49:03 1.809 265.575 13 :49: 06 1.995 265.575 13:49:09 1.995- 265.758

13:49:12 1.809 265.375 13:49:15 1.063 2650393 13:49:18 -6.396 264.388 13:49:21 -21.874 256.441 13:49:24 -22.247 241.4-60

13:49:27 -20. 102 243. 105 13:49:30 -18.983 244.383 13:49:33 -17.678 245.845 13:49:36 -16.652 247.306 13:49:39 -15.813 246.576

13:49:42 -14.850 249. 133 13:49:45 -13.855 250.047 13:49:48 -13.109 250.778 13:49:51 -12.083 251. 600 13:49:54 -10.778 232.970

13:49:57 -9.472 234.249 13: 50: 00 -8.2610 25-5.345 13:50:03 -7.2354 236.238 13:50:06 -6. 1165 257.354 13:50:09 -5.3706 258.268

33

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OTSG-A OTSG-B Pressure Pressure

Time (psig) (psig)

13: 50: 12 -4.8113 258.907 13:50:15 -3.9722 259.547 13: 50: 18 -3.4126 260.095 13:50:21 -2.8533 260.643 13:50:24 -2.2937 261.1S1

13:50:27 -1.9208 261.191 13: 50: 30 -1.4546 261.922 13:50:33 -1.1750 261.922 13: 50: 36 -0.9885 261.922 13:50:39 -0.7087 262. 104

13: 50: 42 -0.5225 262.287 13:50:45 -0.3359 262.469 13: 50: 48 -0.0562 262.469 13:50:51 0.1384 262.652 13: 50: 54 0.3169 262.652

13: 50: 57 C.5034 262.,635 13:51:00 0.6897 262.835 13:51:03 8. 1487 270. 145 13: 51: 06 9.0311 271.491 13:51:09 8.8945 271.239

13:51:12 9. 1743 271.421 13:51:15 9.6406 271.787 13:51:18 9.4539 271.421 13:51 :21 9.2676 271.421 13:51:24 9.4539 271.421

13:51 :27 9.6406 271.604 13: 51: 30 9.9202 271.604 13:51 :33 10.9658 272.883 13: 51: 36 11.5984 273.248 13:51 :39 12.1580 273.522

13: 51: 42 11.3849 273.065 13: 51 : 45 10.3865 271.604 13: 51: 48 9.8271 270.873 13:51 :51 8.8945 269.777 13: 51: 54 8. 1487 269.046

13:51 :57 8.1487 268.864 13: 52: 00 7.81591 268.498 13:52:03 7.61326 268.133 13:52:06 7.6826 268.950 13:52:09 7.61326 267.768

34

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OTSG-A OTSG"B Pressure Pressure

Time (ps i9) (Qsig)

"'. 13: 52: 12 7.5894 267.585 13: 52: 15 7.5894 267.219 13: 52: 18 7 .40283 267.219 13:52:21 7.30957 266.854 13:52:24 7.30957 266.854

13:52:27 7.12305 266.489 13:52:30 7.02979 266.123 13:52:33 6.75000 266.123 13:52: 36 7.02979 265.941 13:52:39 6.93652 265.758

1-3:52:42 6.75000 265.573 13:52:45 6.65698 265.393 13:52:48 6.56372 265.210 13:52:51 6.63698 265.210 13:52:54 6.56372 264.844

13:52:57 6.56372 264.862 13: 53:00 6.37720 264.479 13:53:03 6.47046 264.479 13:53:06 6.28394 264.297 13:53:09 6.56372 264.297

13:53:12 6.56372 264.114 13:53:15 6.65698 264.297 13:53: 18 6.47046 264. 114 13:53:21 6.37720 264.114 13:53:24 6.47046 263.931

13:53:27 9.45386 266.854 13:53:30 9.08105 266.306 13:53:33 9.64063 266.854 13:53:36 9.45386 266.489 13:53:39 8.70801 265.941

13:53:42 8.33521 265.210 13: 53 :45 7.49609 264.753 13:53:48 7.12305 264.291 13:53:51 7.12305 264. 114 13: 53: 54 6.93652 263.931

13:53:57 6.56372 263.566 13:54:00 6.37720 263.200

o!:' 13:54:03 6.28394 263.018 13:54:06 5.81787 262.835 13:54:09 5.91113 262.835

35

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OTSG-A OTS6-8 Pressure Pressure

Time (psig) (psig)

13:54:12 5.72461 262.469 "':<. 13:54:15 5.53809 262.287

13: 54: 18 5.44482 262.104 13:54:21 5.33156 262. 104 13: 54:24 5.81787 262.267

13:54:27 5.53809 262. 104 13: 54: 30 5.53809 262.104 13:54:33 5.55156 261.922 13:54:36 5.25830 261.922 13:54:39 5.25830 261.556

13: 54:42 5. 16528 261.373 13:54:45 5.07202 261.008 13: 54: 48 4.97876 261.191 13: 54: 51 6.7~JOO 262.335 13:54:54 6.37720 262.652

13:54:57 6. 19067 262.469 13:55:00 5.91113 262.287 13:55:03 5.91113 262. 104 13: 55:06 5.91113 262. 104 13:55:09 5.72461 261.922

13: 55: 12 5.91113 261.922 13: 55: 15 7.40283 263.200 13: 55: 18 6.65698 262.632 13:55:21 6.47048 262.287 13:55:24 6.28394 262. 104

13: 55 :27 6.09741 261.922 13:55:30 6.09741 261e922 13:55:33 6.00415 261.. 922 13: 55: 36 6.00415 261.465 13:55:39 5.91113 261.373

13:55:42 5.91113 261.373 13:55:45 5.91113 261.373 13: 55: 48 5.91113 261.373 13:55:51 5.91113 261.556 13:55:54 6.00415 261.922

13:55:57 6.,1]046 262.287 13: 56: 00 6.65698 262.469 13:56:03 6.84326 262.652

36

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OTSG-A OTSG-B Pressure Pressure

Time (psig) (psig)

" 13:56:06 7.12305 262.835 13:56:09 7.21631 262.469 13: 56: 12 7.40283 262.652 13: 56: 1 S 7.40283 262.652 ,. 13:56:18 7.68262 262.835

13:56:21 7.58936 262.652 13:56:24 7.58936 262.469 13:56:27 7.21631 262.469 13: 56: 30 7.58936 262.469 13:56:33 7.58936 262.287

13: 56: 36 7.58936 262.469 13:56:39 7.4960S 262.469 13:56: 42 7.68262 262.469 13:56:45 7.58936 262.469 13: 56: 48 7.68262 262.469

13:56:51 7.58936 262.469 13: 56: 54 7.77588 262.469 13:56:57 7.77588 262.652 13: 57 :00 -:'.77588 262.287 13:57:03 7.77588 262.287

13: 57: 06 7.77588 262.469 .. 13:57:09 7.96216 262.104

13:57:12 7.86914 262.10~

13:57:15 8.05542 262. 104 13:57:18 8. 14868 261.922

13:57:21 9.64063 263.270 13:57:24 9. 17432 262.835 13:57:27 9.08105 262.469 13: 57: 30 9. 17432 262.469 13:57:33 9.08105 262.287

13:57:36 9. 17432 262.287 13:57:39 8.98779 262.104 13:57:42 8.98779 261. 922 13:57:45 8.70801 261.556

13: 57: 48 8.52173 261.373 13:57:51 8.33521 261.191 13:57:54 8.24194 261. 008 13:57:57 8.33521 261.008 13:58:00 8.24194 260.825

"

37

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OTSG-A OT5G-6 Pressure Pressure

Time (psig) -.Jpsig) -

13: 58:0:3 8.24194 261.005 13:58:06 8.24194 261.008 13:58:09 8.70801 261.191 13:58:12 8.52173 261.008 13: 58: 15 8.24194 260.825

13: 58: 18 8.33571 260.73'J 13:58:21 8.33571 260.225 13:58:24 8.24144 260.643 13:58:27 8.33521 260.734 13:58:30 8. 14868 260.369

13:58:33 8. 14868 260.367 13:58:36 7.77588 260.277 13: 58: 39 7.77588 259.912 13:58:42 7.58936 259.912 13: 58: 45 7.40203 259.547

13:58:48 7.21631 259.364 13: 58: 51 7.02979 259. 181 13:58:54 6.75000 258.999 13:58:57 6.65698 258.907 13:59:00 6.47046 258.033

13: 59: 03 6. 19067 258.430 13:59:06 5.91113 258.268 13: 59: 09 5.91113 258.268 13:59:12 5.81707 258.085 13:59:15 5.72451 257.902

13: 59: 18 5.53809 257.902 13:59:21 5.53809 257.537 13:59:24 5.35156 257.720 13:59:27 5.44482 257.446 13:59:30 . 5.23830 257.446

13: 59: 33 5.25830 257.446 13:59:36 5. 16528 257.354 13:59:39 5.25830 257.446 13:59:42 5.25830 257.354 13:59:45 5. 16528 257. 171

13:59:48 5. 16528 256.989 13: 59: 51 5.07202 256.989 13:59:54 4.97876 256.989 13: 59: 57 4.69897 256.806 14:00:00 4.60371 256.806 14:00:03 4.69897 256.989

38

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APPENDIX C STRIP CHART RECORDS

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10 BS-PT-4388-1

8 '8i U) 6 a. -Q) 4 .... ::J If) en 2 Q) .... Q.

0

~ 10AM

'8i 50 I

en 40 f-BS-PT-4388-2 c. Q) 30 r .... ::J

20 ·en f-en Q)

10 .... I-Q.

0 10 AM

APPEr-tJIX C STRIP CHART RECORDS

12 N 2 PM

Time

I I

28 psi ~

12 N 2 PM

Time

Figure C-l. Reactor Building pressure stripchart

41

4 PM 6 PM

I

..:..

---

4 PM 6 PM

INEL 3 3651

records (28 Marc h 1979).

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::~ 180

170

160

--------- ...,.,--(L 150 o

140 ~ ~ -'" ....

---~ ....-------­

Elevation 330 (14)*

Elevation 353 (12)

'I \ : ~ElevatiOn I I~ 330 (13)

~V' I ~ .... , ....... ------ \' I \ -- V

Q)

0. 130 E -~ ... -.....

~ ... ~ ---- .... ----Q) I-

(11) .--... J.:~:' (6) •• ::;....~/ (5)~ ,~"~ ," ~.,~ :~

100 ~':~~' /'" ". /: " ------ ~ .. , \

90 ~~' Block valve opened ' :

120

110 Air supply ducts (after fans)

80 *Number in parenthesis is the stripchart record

70~----------~----------~------------~----------~ 2 PM 1 PM

INEL33650 5 PM 4 PM 3 PM

Time

Figure C-2. Reactor Building resistance temperature detector readouts.

42

______________________ ............... &ml .... ... 2 It

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APPENDIX D TMI-2 ALARM PRINTER PRINTOUT SEQUENCE FOR 4 PSIG REACTOR BUILDING

PRESSURE CHANNELS AND 28 PSIG ENGINEERED SAFEGUARDS BUILDING SPRAY ACTUATION PRESSURE SWITCHES

431J-{~

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APPENDIX D TMI~2 ALARM PRINTER PRINTOUT SEQUENCE FOR 4 PSIG REACTOR BUILDING

PRESSURE CHANNELS AND 28 PSIG ENGINEERED SAFEGUARDS BUILDING SPRAY ACTUATION PRESSURE SWITCHES

.;.:.

Input Set Point Time Number Channel Designation Action (psig)

13: 50:21 3167 4 PSI RB Pressure Red Ch Trip High 3.6 13:50:21 2833 4 PSI RB Pressure Red Ch Trip High 3.6 13:50:21 3278 4 PSI RB Pressure Red Ch Trip High 3.6 13:50:21 3168 4 PSI RB Pressure Grn Ch Trip High 3.6

13:50:21 2834 4 PSI RB Pressure Grn Ch Trip High 3.6 13:50:21 3279 4 PSI RB Pressure Grn Ch Trip High 3.6 13: 50: 21 3169 4 PSI RB Pressure Vel Ch Trip High 3.6 13:50:21 2835 4 PSI RB Pressure Vel Ch Trip High 3.6

13:50:21 3280 4 PSI RB Pressure Vel Ch Trip High 3.6 13:50:22 3170 4 PSI RB Pressure Blue Ch Trip High 3.6 13:50~26 3264 ES Bldg Spray Sw Act B Ch 2 Trip Trip 26.6 13:50:27 2836 ES Bldg Spray Sw Act A Ch 1 Trip Spray 27.05

13:50:27 2837 ES Bldg Spray Sw Act A Ch 2 Trip Spray 27.30 13:50:27 2838 ES Bldg Spray Sw Act A Ch 3 Trip Spray 27.75 13:50:27 3265 ES Bldg Spray Sw Act B Ch 3 Trip Trip 27.35 13:50:27 3281 ES Bldg Spray Sw Act B Ch 1 Trip Trip 27.85

13: 50: 31 3265 ES Bldg Spray Sw Act B Ch 3 Trip Norm 26.20 13:50:31 3281 ES Bldg Spray Sw Act B Ch 1 Trip Norm 26.75 13:50:32 3264 ES Bldg Spray Sw Act B Ch 2 Trip Norm 25.40 13:50:32 2836 ES Bldg Spray Sw Act A Ch 1 Trip Norm 25.80

13: 50: 32 2837 ES Bldg Spray Sw Act A Ch 2 Trip Norm 26.30 13:50:32 2838 ES Bldg Spray Sw Act A Ch 3 Trip Norm 25.80 13: 52: 53 3170 4 psi RB Pressure Blue Ch Trip Norm 3.2 13: 53: 14 3167 4 psi RB Pressure Red Ch Trip Norm 3.2

13: 53: 32 3280 4 psi RB Pressure Vel Ch Trip Norm 3.4 13:53:37 2833 4 psi RB Pressure Red Ch Trip Norm 3.4 13:53:49 3169 4 psi RB Pressure Ye1 Ch Trip Norm 3. 1 13: 54:01 2834 4 psi RB Pressure Grn Ch Trip Norm 3.3

13: 54: 03 3279 4 psi RB Pressure Grn Ch Trip Norm 3.3 13:55:15 3278 4 psi RB Pressure Red Ch Trip Norm 2.9 13:59:15 2835 4 psi RB Pressure Vel Ch Trip Norm 3.3 14:01:44 3168 4 psi RB Pressure Grn Ch Trip Norm 3.0

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APPENDIX E REACTOR BUILDING ATMOSPHERE

HYDROGEN, OXYGEN, AND NITROGEN ANALYSIS DATA

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Date

3/31/79 3/31/79 3/31/79 3/31/79 3/31/79

4/1/79 4/1/79 4/1/79 4/1/7Cj 4/1/79

,. 4/1/79 4/1/79 4/1/79 4/1/79 4/1/79

4/1/79 4/2/79 4/2/79 4/2/79 4/2/79

4/3/79 4/3/79 4/3/79 4/4/79 4/6/79

4/6/79 4/7 /79 4/7/79 4/8/79 4/8/79

APPENDIX E REACTOR BUILDING ATMOSPHERE

HYDROGEN, OXYGEN, AND NITROGEN ANALYSIS DATA

Sampl ing % H2 % O2 % N2 Time Method ---

06:00 Ua 1.7 15.7 82.6 06:00 U 1.7 16.5 81.8 21:00 GC 2.0 22:00 G 1.7 23:30 G 2.3

07:00 G 1.9 19.2 78.9 09:30 Ae 2.4 12:00 G 2. 1 19. 1 78.8 12: 25 A 2.0 13:30 G 2. 1 18.9 79.0

13:30 A 2. 1 15 :00 G 2.0 18.7 79.3 15:00 A 2.0 18:30 G 2.0 21. 8 76.2 19:00 A 2.0

23:00 G 2.3 18.9 78.9 06:00 G 2.4 17.6 79.9 10: 30 G 2. 1 18.4 79.5 23:36 A 2. 1 23:42 A 2. 1

10: 1 0 A 1. 95 10: 21 A 2.0 23:00 G 2.3 17.7 80. 1 16: 1 0 A 1.5 20:00 Rf 1.65

22:45 A 1.8 06:00 R 1. 59 14:00 A ~ • 65 02:30 A 1.65 13:45 A 1. 74

49

Reference

NSAC-lb NSAC-l GPUd GPU GPU

GPU GPU GPU GPU GPU

GPU GPU GPU GPU GPU

GPU GPU GPU GPU GPU

GPU GPU GPU GPU GPU

GPU GPU GPU GPU GPU

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Date

4/9/79 4/9/79 6/1/79 8/2/79

a. Unknown.

lime

04:30 04:40

Sampling Method

A A

% H2

1.95 1.2 0.6 0.6

14.5 14. 1

Reference

GPU GPU NSAC-l NSAC-l

b. Nuclear Safety Analysis Center (EPRI), Analysis of Three Mile Island Unit~_Accident, NSAC-80-1, March, 1980.

c. Grab sample analyzed by a gas partitioner.

d. GPU/TMI-2 secondary chemistry log books.

e. On-line gas chromatograph.

f. Calculations based on recombiner inlet and outlet gas temperature.

50

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APPENDIX F INVESTIGATION OF THE TMI HYDROGEN PHENOMENA

OF MARCH 28, 1979

51

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Date

Subject

To

Inter-OHlce .emorandum

MARCH 26, 1982

INVESTIGATION OF THE TMI HYDROGEN PHENOMINA OF MARCH 28, 1979

G. R. EIDEM

I!fi[I Nuclear 7132-82-167

location THREE MILE ISLAND

The following information is provided to assist in the investigation of the TMI Hydrogen Phenomina of March 28, 1979.

1. Reactor Building Ventilation and Purge System

a. Fan cooler units Four fan cooler units are oper~ted under normal conditions. four fan coller units are also operated under LoeA conditions. Ref. 1MI Unit 2 FSAR Section 6.2.2.2.2.1 through 6.2.2.2.8 (see page 6.2-2Sb AMS9 10-7-77) and 9.4.1S.1. The system description and FSAR Sections 1.2.3.1.4 AM48 11-1S-76 and 7.3.1.1.3 AMS9 10-7-77 incorrectly state three fans operating under normal conditions anf five under LOeA conditions.

b. LOeA Dampers, 0-5127 A&B

The LOeA dampers are designed to ope~ on reactor building isolation when ES actuation secures instrument air to the LOeA dampers by closing AH-V-72 (ES actuation A) and AH-V-7l (ES actuation B). This event occurred at 07:56 on March 28, 1979.

NOTE: ES actuation A at 07:56:23 and ES actuation B at 07:56:13.

Reactor building pressure remained above the 3.S8 PSI ES actuation setpoint until about 09:30 a.m. Therefore the LOCA ducts would have remained open during this period. This would be a major flow path f()r reactor building ventilation; fan coolers through the open LOeA dampers, up the LOeA ducts and exiting the gravity dampers (which are welded open) at the 416 1 8" level. The du(:ts are directed toward the reactor building dome (see B&RDwg. 2041 and GPU Vendor Dwg. 63-01-0088). Moreover, it is likely that the dampers remained open durinq the entire accident. [)amper position is indirectly indicated by the position of vahes AH-V-71, AH-V-72 & AH-V-74, if any of these valves are clt,sed, instrument air to the dampers is secured and the dampers open. After an ES signal the valves close and must be manucilly repositioned by handswitch (Ref. FSAR section 7.3.2.1 P AMS9 10-7-77). There are no records of these valves bei ng ,'epos i t i oned fo 11 ow; ng the 07: 56 RB isolation. It is un1U:e1y that they were repositioned pr10r to the hydrogen phenom1lna. It 1s therefore possible for a

, ' \ ,

AOOOOMI

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. . .... . ~~. _:"r-'-.-, _~---::_ .. ____ ~ __ ~.~._~~_~ _____ . ________ '_ -

G. R. EIDEM 1132 .. 82-167

PAGE 2 MARCH 26, 1982

. .

relatively high concentration bf hydrogen to have accumulated in the vicinity of the reactor building dome prior to the con­flagration. NOTE: Specific times given in the abuve discussion were

obtained from computer alarm summary printout. 2. a. Main Steam Pressure Transmitters

There are four main steam pressure transmitters. Two per steam generator. These devices measure differential pressure (main steam outlet pressure / R. B. pressure) and transmit indication to the IeS computer and B&W supplied mini computer (reactimeter) through a manual selector switch (one per steam generator). The position of the selector switches at the time of pressure spike is not known therefore, which two of the four pressure transmitters were logged on the reactimeter's magnetic tape 1s also unknown. At the time of the hydrogen burn the water level in the reactor building would have submerged one transmitter and three would be above water.

Presented below are some parameters of interest in this discussion:

Transmitter

SP-6A-PT1 SP-6A-PT2 SP-6B-PT1 SP-6B-PT2

Rack

426 424 MTG R13 428

Elevation

288.0' 288.5' 284.0' 288.5'

Penatration Elevation

292.0' 292.0' 342.0' 292.0'

b. Calculation of Water level in the Reactor Building Basement at the Time of the Hydrogen Burn.

Although it is not possible to calculate the exact water level in the building at the time in question, it is possible to calculate an upper bound water level based on avaHable data. The two primary sources of water were the reactor building coolers, operating by use of the river water as a cooling medium, this accounts for 1251 gallons, and the borated water storage tank accounting for an addition 231,702 gallons by 17:20 on 3/28/79. Combining these figures gives a water depth in the basementof 2.83 ft., water had reached the 285.33' 1 eve 1 •

Data

Inventory released to the r(!actor buHding floor via the BWST is based on level indications taken from shift supervisor and CRO logs and the TMI-2 tank log.

~1

54.7 ft.

26.5 ft.

Date

3/27/79

3/28/79 @ 17:20

Data Sov:-'ce

TMI-2 Tank log DRMG File Tl-0001.04 Shift Supervisor log and eRO Log

54

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, I I !

,,- -... _- - "~----- '--- -. ~--'------------'--.----~--.---,.,-.. --.- .. ~----..,~~~~---

G, ~, EIDEN 7132-82":167

... ~....,..,..- ----------_ .. _------" ----~-~----- - .. _ ... _-- . __ ... ,.-.... ----------~

PAGE 3 MARCH 26, 1982

The volume calculation must be done in two parts 1: 54.7 ft to 51.0 ft. and 2: 51.0 ft. to 26.5 ft. This method accounts for the oblate hemispherical tank top .. (Ga11ans per ft. varies from 7375 ga1/ft to 8261 ga1/ft). Combining both parts of the calculation, a total of 231,702 gallons were released from the BWST. .,

Water released to the reactor building by the river wdter cooling system is calculated to be 180,000 gallons based on recovery engineering calculation #75 as referenced in recovery engineering letter Sept. 10, 1981, 5530-81-095 from R. H. Greenwood to D. K. Croneburger titled "Reactor Building Floording Following the TMI-2 Accitent. II

To arrive at a water level in the reactor building at the time of the hydrogen phenomina one must back this calculation 59 days.

NOTE: The calculation concludes that about 180,000 gallons were added to the building between 3/28/79 and 5/27/79.

59 days = 84,960 minutes

180,000 gallons/84,960 minutes = 2.12 gpm

or 2.12 gallons per minute were being added to the building via the reactor building coolers using river water as a cooling med1a.

Assuming this leak rate was constant and projecting forward to the time of the detonation (3/28/79, 13:50) one obtains 1251 gallons added to the reactor building basement by this mechanism.

990 minutes x 2.12 gallons per min~te = 1250.8 gallons

The total water in the TMI-2 basement at the time of the hydrogen phenomina is then:

231,702 gal. 1,251 gal.

-2,500 gal. -7,240 gal.

-12,400 ga 1.

210,813 gals.

BWST Injection River water Leakage Sump Volume RC Drain Tank Volume Sump Pump Transfer

Total in Bldg.

Assuming 6,200 gallons/in from RB water level memmo TMI-II-R-2352, February 14, 1980.

then: 210,813 gal/6,2DO Gal/In = 34.0" or 2.83 ft. of water had accumulat • .:d or water had reached the 285.33' level.

S5

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G. R. EIDEM 7132 .. 82-167

PAGE 4 MARCH 26, 1982

3.

NOTE: The 12,400 gal. figure used in calculation 675 is probably incorrect .. Reactor building sump pump acceptance tests. REF: TMI-2 Startup Test TP 235/1, would indicate a value of 8,400 gallons transferred. This value would increase level by 0.65 inches.

Reactor Building Temperature

Revfew of previously published reports indicates that there is ~ome question as to location of reactor building temperature elemen~s. The table presented below will, hopefully, clear up these uncertainties. The Points refer to PEN numbers of multipoint recorder AH-YMTR-5017.

Point location TemE. E1 ement B&R Dwg. *TemQ of

1 2 3

4

5 6 7 8 9

10 11

12 13 14 15 16

11 Primary Shield AH-TE-5017 2227 bllO 12 Primary Shield AH-TE-50l8 2227 b109 13 Primary Shiel d AH-TE-5016 2227 b106 14 Primary Shield AH-TE-50l9 2227 b106 #1 Air Supply AH-TE-5015 2229 123 12 Afr Supply AH-TE-5027 2229 122 Ambient Imp. Barrier AH-TE-50l3 2227 156 Ambient Sump Area AH- TE-50l 0 2227 132 Ambient letdown Cooler AH-TE-50ll 2227 128 Ambient Drain Tank AH-TE-5012 2227 152 ,,"bi ent E1 ev . 353-1 AH-TE-5020 2227 ~103

kltbi ent El ev . 353-2 AH-TE-S021 2227 180 Ambient Elev. 330-1 AH-TE-S023 2228 170 Ambient Elev. 330-2 AH-TE-5022 2228 182 Ambient E1ev. 310-1 AH-TE-5014 2228 151 Imbf ent E1 ev . 310-2 AH-TE-5088 2228 151

NOTE: These points print on a 6 min"te interval so that peak temperatures must be extrapolated from the stripchart. * Maximum (unextrapolated) temperature at the approximate time of detonation. a. Point 11 decreased by about 220 F at this time. b. Points 1,2.3 & 4 remained relat1v@ly constant through

the transient.

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G, R, EIDEM 7132-82-167

PAGE 5 MARCH 26. 1982

The attached ffgure is a copy of the AH-VHTR-5017 stripchart during the period of fnterest. Curves were drawn by this reports author. .

JEF:dg Attachm~nt

cc: H. M. Burton F. l. Mel tzer CARIRS

--/}

~ ~E-?£. ~~James E. Flaherty

Technical Information Coor~ator

(wfth attachment) "

(w/o attachment)

51/58

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- ".-"---

,.

" ..

APPENDIX G

INVESTIGATION OF THE TMI HYDROGEN PHENOMENA OF MARCH 28, 1979

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APPENDIX G INVESTIGATION OF THE TMI HYDROGEN PHENOMENA

OF MARCH 28s 1979

The TMI-2 OTSG steam pressure transmitters indicate the ,difference

between steam generator pressure and Reactor Building pressure t as Reactor Building pressure acts on one side of a pressure sensing bellows and steam pressure acts on the other side. Bellows movement is transmitted by a mechanical linkage to a mechanical/electrical transducer in the conventional manner. If it is assumed that steam pressure was constant (or nearly sa) during the hydrogen burn period 13:49:12 to 13:51:00 h, then the indicated decrease in steam generator A and steam generator B pressure during this

period can be interpreted as an increase in Reactor Building pressure, i.e.,

Reactor Building pressure = P - p(t) + P b o r

where

= indicated steam pressure at 13:49:12

p(t) = indicated steam pressure at time 13:49:12 ~ t < 13:51:00

= Reactor Building pressure at 13:49:12.

For measuring a change in pressure such as that which occurred during

the hydrogen burn period, 13:49:12 to 13:51:00 h, the sum of deadband, repeatability, hysteresis, and drift is judged to be the most applicable for stating data accuracy. This is specified by the manufacturer to be ±0.15% of the 180 psig instrument span or ±2.7 psi.

61

'.;

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OTS6 Pressure Transducer Data

Manufacturer Model Accuracy Span

Deadband Repeatability Hysteresis Drift

Temperature Sensitivity

Time Response

Foxboro Ell GM SAEl ±0.5% of span 200 to 2000 psi

±0.15% of span

±l.O%/lOO°F below 250°F body temperature ±2.0%/100°F above 250°F body temperature

1. 17 s

62

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APPENDIX H REACTIMETER ZERO OFFSET SHIFTS

Lorenzo D. Goodrich

James Adams

Jim K. Jacoby

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I,

APPENDIX H REACTIMETER ZERO OFFSET SHIFTS

Introduction

J. O. Henrie and A. K. Postma have performed an investigation of

selected TMI-2 Reactimeter Data which is reported in Reference H-l. This

appendix reports a computer analysis of that data intended to determine the probability and frequency of nearly equal simultaneous voltage changes on multiple data channels.

It is suggested that the reader refer to References H-l and H-2 for background prior to using the material presented in this Appendix.

Method

During examination of the iOTSG data reported in Reference ~-l, it was ,

noticed that pressure in the st~am generator took a sudden jump of about

7.5 psi at 13:51:00 reactimeter time. Similar jumps of smaller magnitude

occurred at 13:53:24, 13:54:48, 13:55:12, and 13:57:18. Plots of the

reactimeter data during this time period are shown on Figures H-l thru H-l1 with the sudden jumps indicated. The reactimeter patch schedule is given on Table H-l. Using the voltage/engineering unit conversions shown on Table H-2 to convert the engineering unit uata changes at 13:53:24 to volt­age changes, it was found that the voltage change on several of the channels

was almost the same. This indicates an overall simultaneous zero offset

calibration shift of these channels on the reactimeter, since a real physi­

cal event would not be expected to result i~ the nearly the same voltage

change on so many data channels. In addition, a change in indicated turbine header pressure (MUX Channel 15) from 496.6 to 500.2 psig, which occurred at 13:51 :00 reactimeter time, apparently does not represent a real change in pressure because the turbine header pressure transducer is a 600 to

1200 psi range instrument and the actual pressure in the turbine header at

this time was near atmospheric as indicated by OTSG "A" steam pressure. Consequently, a test was performed in~situ on the turbine header pressure transducer. It was found that the pressure transducer would not respond to

65

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148r-------~------_r--~--~-------~--------~------~ Sudden

-~----jump

CL 146 o -<C Q. o o

...J

-0 (5 o ....

z-Q. Q.

~

« Q. 0 0

....J

~-0

-c: ns (5 0 0 .... 0 -0 ns Q)

a:

144 ----.-----

142~------~------~----~~----~~----~~----~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

Time, March 28, 1979 INEL33610

Figure H-l. Cold temperature of Loop A.

0.3

I .. ~udden I

0.2 ----J- r-~-

\ ~

0.1 . - - -.-.------- ------

0

-0.1 13:44:35 13:46:15

___ l _______ ---------I

Y \

1\ I

13:47:55 13:49:35 13:51:15

Time, March 28, 1979

jump

13:52:55

Figure H-2. Reactor coolant flow, Loop A.

66

13:54:35

INEL 3 3612

.\

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'.'

-c: -Q) > Q)

~ c: cu ... a. :::J Q) ~ cu ~

:c-o. a. ~ -a. o o

...J

i o ;: ... c: cu (5

8Or-------~------~~----r_------r_--~_,._----_,

75 -- ---- ------- ----- ------ ------+-~---+_----_t

70 -----\----+----- ---.--++

65~----~~----~~----~~----~~----~~----~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15

Time, March 28, 1979

Figure H-3. Makeup tank level.

13:52:55 13:54:35 INEL 3 3605

0.4~------~------~--------~------~--------r-------~

0.2

-04 ___ --

I

: -----i-----\--+-

! i

, ,

Sudden jump

8 0 ~_...A_J:-+ '-o ... u cu Q)

a:

-0.2~------~------~------~------~------~------~ 13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

TimEt, March 28, 1979 INEL 3 3611

Figure H-4. Reactor coolant flow, Loop B.

67

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c; ·en Co -4(

Co 0 0 .J

cP .... ::J II) II) Q) .... Co .... Q) "C IG Q) .c Q) c:: :0 .... ::J .....

z Co Co ~

Co o o .J

504 Sudden .. jump

502

500 ------_ .. -

498

496L-------~------~------~------~------~------~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

Time, March 28, 1979 INEL33609

Figure H-S. Turbine header pressure, Loop A.

0.40,....----,....-----,-----,,-------..,r-------..,r---·---

.... Sudden jump

;i 0.38 --.- .--.. -.-- -----.... --o .... Q) -IG :: "C Q) Q) u..

0.36 1....-___ "'--___ "'--____ "'--____ '--____ '--__ ........

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55

Time" March 28, 1979

Figure H-6. Feedwater flow, Loop A.

68

13:54:35 INEL3 3608

".

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=c­o. a.

0.46 r-----.-----r-------,r-------,.-------,.------, Sudden

-.. ---- jump

::. m 0.44-------v-t-a. o o ..J

~ o

I ;0= ~

CI) -~ 0.42 "0 CI) CI) lL

Ci (/) a. -CI) ~

:::J (/) (/) CI) ~

a. E (\j CI) -(/)

0.40 '---__ "'--___ ...I--___ ...J.-___ -L-___ ~ ___ ~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

Time, March 28, 1979 INEL 3 3607

Figure H-7. Feedwater flow, Loop B.

20~------~------~------~--------r-------~------~

o I

i I

Sudden -... oe--- jump

« - 20 - ------­ ------f-------+-----f-------f C!) fF) I-o

-40'------"'-----~----~-----L----~------..J 13:44:35 ';3:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

Time, Mar:::h 28, 1979 fNEL 3 3614

Figure H-8. OTSG A steam pressure.

69

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Ci o C. -Q) ~

::J o o ~

280.------.-------r------.---~--r_----~------~ Sudden

-~------ jump

~260 - -- -- --ns Q) ..­o m (!} en t­O

-::§?. o

240~------~------~------~----~~----~~----~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15 13:52:55 13:54:35

Time, March 28, 1979 INEL 3 3615

Figure H-9. OTSG B steam pressure.

62~------~------~------,-------~------_r------_, Sudden ,-.. _--

~ 61---Q)

Cl c::: ..-ns Q) c. o m (!} 60 - - ---- -------­en

------ ------I-------+------t

t-O

59L-------L-------~-------~------~------~----~

13:44:35 13:46:15 13:47:55 13:49:35 13:51 :15 13:52:55 13:54:35

Time, March 28, 1979 INEL 3 3616

Figure H-10. OTSG B operating level.

70

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....

"

-r:::: -Q) > Q)

a. ~ ... .... CIS ... r/)

(!) (J) t-O

I

246 Sudden - jump

244

I

242 ---r~--

240 ------

238 ~ ______ ~ _______ ~ ______ ~ ________ L-______ ~ ______ ~

13:44:35 13:46:15 13:47:55 13:49:35 13:51:15

Time, March 28, 1979

Figure H-ll. OTSG startup level.

13:52:55 13:54:35

INEL 3 3613

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TABLE H-l. REACTIMETER PATCH-SCHEDULE

Logged Variable Mux Patchboard Logged Measurement Range if Different

Channel Number DELOG Variance 10. Than DASEY Range

1 14 - 012~; + 0125 NI-5 Power Range 0/+10V 0/125% 2 28 + 0520 + 0620 T HOT LP A NR TEl - 4A -10/+10V 520/620 oF 3 29 + 0520 + 0620 T HOT LP B NR TEl - 4B -10/+10V 520/620°F 4 31 + 0050 + 0650 T COLD LP A WR TE2 - 5A -10/+10V 50/650°F 5 34 + 0050 + 0650 T COLD LP B WR TE2 - 5B -10/+10V 50/650°F 6 45 + JOOO ,. 0090 RC FLOW LP A TEMP COMP RC-14A-DPT-1 -10/+10V 0/90 MPPH 7 22 - 0400 + 0000 PZR LVL TEMP. COMPo RC-LT1-10RCTEl-2 +lO/-lOV 0/400 IN 8 96 + 0000 + 0100 MUT LVL MU-14-L Tl -10/+10V 0/100 IN 9

,,... - 9990 + 9999 PZR SPRAY VLV POSe RC-V2 CLOSED CC 1::1 ""-.J 10 65 - 0250 + 0250 DRAIN TANK PRESS. WDL-1202-PT O/+lOV 0/250 PSIG N

11 27 + 0900 + 2500 RC PRESS. LP 8 NR RC-3D-PT2 0/+ lOV 1700/2500 PSIG 12 1 - 9999 + 9999 REACTOR TRIP TRIP - CC 13 47 + 0000 + 0090 RC FLOW LP 8 TEMP COMP RC-38-DPT-l -10/+10V 0/90 MPPH 14 57 - 0500 + 0000 FEEDWATER TEMP. SP-5A-TE-1 +lO/-lOV 01500°F 15 110 - 0305 + 1203 TURBINE HDR. PRESS. LP A SP-10A-PT1 +2/+10 600/1200 PSIG 16 49 + 0000 + 0100 OTSG A OP LVL TEMP COMP SP-1A-LT2 -10/+l0V 0/100% 17 50 + 0000 + 0250 OTSG A SU LVL SP-1A-LT4 -10/+10V 0/250 IN. ,X,

18 62 + 0000 + 6500 FEEDWATER FLOW LP A FE-8A FW-8A-FE -10/+10V 0/6500 KPPH .' :i

19 63 + 0000 + 6500 FEEDWATER FLOW LP B FE-88 FW-8B-FE -10/+10V 0/6500 KPPH 20 85 - 9999 + 9999 TURBINE TRIP TRIP - CC 21 112 - 1833 + 1222 OTSG A STM. PRESS. SP-6A-PTl +2/+10V 0/1200 PSI 22 113 - 1796 + 1197 OTSG 8 STM. PRESS. SP-6B-PTl +2/+l0V 0/1200 PSI 23 51 + 0000 + 0100 OTSG B OP LVL TEMP COMP SP-1B-LT2 -lO/+lOV 0/100% 24 52 + 0000 + 0250 OTSG B SU LVL SP-1B-LT4 -lO/+lOV 0/250 IN.

!>- 4. iii> ..

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TABLE H-2. MUX VOLTAGE/ENGINEERING UNIT CONVERSIONS

1 2 3 4 5 6 7 8 9

iO 11 12

13 14 15 16 17 18 lS 20

21 22 23 24

Patchboard Number

14 28 29 31 34 45 22 96 19

65 27 1

47 57

110 49 50 62 63 8S

112 113

51 52

Equations

Mux 1 = 12.5* (Voltl) Mux 2 = 570.0 + (5.0* Volt 2) Mux 3 = 570.0 + (5.0* Volt 3) Mux 4 = 350.0 + (30.0* Volt 4) Mux 5 = 350.0 + (30.0* Volt 5) Mux 6 = 45.0 + (4.5* Volt 6) Mux 7 = 200.0 - (20.0* Volt 7) Mux 8 = 50.0 + (5.0* Volt 8) Mux 9 = Volt 9 (If [(Volt 9.GE.9.0) and (Volt 9.LE.10.0)] then Mux 9 = 10.0 If [(Volt 9.GE-1.0) and (Volt 9.LE.l.0)] then Mux 9 = 0.0 Mux 10 = 25.0* (Volt 10) Mux 11 = 1700.0 + (80.0* VoltJ 11) Mux 12 = Volt 12 If [(Volt 12.GE.9.0) and (Volt 12.LE.10.0)J then Mux 12 = 10.0 If [(Volt 12.GE.-l.0) and (Volt 12.LE.l.0)J the Mux 12 = 0.0 Mux 13 = 45.0 + (4.5* Volt 13) Mux 14 = 250.0 - (25.0* Volt 14) Mux 15 = 600.0 + (75.4* Volt 15) - (2.0* 75.4) Mux 16 = 50.0 + (5.0* Volt 16) Mux 17 = 125.0 + (12.5* Volt 17) Mux 18 = 3.?5 + (325* Volt 18) Mux 19 = 3.25 = (325* Volt 19) Mux 20 = Volt 20 If [(Volt 20.GE.9.0) and (Volt 20 o LE.l0.0)J then Mux 20 = 10.0 If [(Volt 20.GE.-1.0) and (Volt 20.LE.1.0)] then Mux 20 = 0.0 Mux 21 = 152.75* Volt 21 - (2.0* 152.75) Mux 22 = 149.65* Volt 22 - (2.0* 149.65) Mux 23 = 50.0 + (5.0* Volt 23) Mux 24 = 125.0 + (12.5* Volt 24)

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I

I ( I

input pressure changes if the absolute pressure was below 500 psig. This is another strong indication that the reactimeter data spikes in' question were not real.

A statistical analysis of the voltage changes that occurred was per­formed to determine if the sudden jumps, with nearly equal voltage cilanges, were improbable events.

The coefficient of variation was analyzed for 116 events from the NSAC-1 H-2 Sequence of Events table at the event initiation time listed in Reference H-2. No events were found which had a coefficient of variatior. less than 1.0 out of the 116 times examined. In addition, for 27,168 data

points examined on the reactimeter data tape out to 81,156 s total elapsed time, only 28 data points were fOllnd which had a coefficient of variation

H-3 of less than 1.0.

Eight out of these 28 correspond to sudden jumps illustrated on Figure H-1, and the sudden jump a~ 01,125 s has the lowest coefficient of variation found. On this basis, it was concluded that the probability of

nearly equal voltage changes on several channels as a result of a real

physical event is so low that the sudden voltage changes must have been due to a shift in the zero offset calibration of the data channels in question.

Although it could not be confirmed, the calibration shifts were most probably due to the reactimeter power supply being on a different grounding system than the instrument data channels. In that case, any ground f au lts in either system could be expected to result in a zero offset calibration. Numerous grounc Caults could have occurred as d result of the combined effects of the. ,t high humidity conditions, Reactor Building spray actua­tion which contained a conductive solution of NaOH, and the high temperature

damage of electrical insulation caused by the hydrogen burn.

It was found that some data channels did not exhibit sudden jumps. Although it is beyond the scope of this document to explain why, it is

74

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"

. '

related either to (a) the fact that the particular data channel was over­ranged at the time, or (b) the channel was on/off (i.e. reactor trip), or (c) th~ channel was a zero-to-ten volt output channel. The channel voltage outputs are shown on Table H-2.

The statisti~~l analysis also indicated that after the hydrogen burn,

zero calibration shifting was occurring so frequently, that the reactimeter

data were rendered very unreliable. Any use of this data would have to be done with extreme caution unless a way was found to determine and apply a suitable zero calibration shift correction.

References

H-l. J. O. Henrie, A. K. Postma, ~alysis of TMI-2 Transients, GEND-Inf-023, Vol V, to be published. Also published as SO-WM-TI-067 by Rockwell Hanford nperations May 1983

H-2. J. O. Henrie, A. K. Postma, Anal~is of the TMI-2 Hydrogen Burn, GEND-Inf-023, Vol. IV, March 1983.

H-3. Nuc lear Safety Anal ys'i s Center, Ana~s of Three Mi 1 e Is 1 and-Unit 2 Accident, NSAC-80-l, Mar~h 1980 •

75