regulatury #ormation distribution sys10 (rids) …a e /ient page 1 of 2 secmtel 9 mrwk wu infoaster...
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REGULATURY #ORMATION DISTRIBUTION SYS10 (RIDS)
ACCESSION N4R:;8404050020 DUC.DATE: 84/04/02 NOTARIZED: NO DOCKET # FACIL:50-, 61 San Unofre Nuclear Station, Unit 2, Southern Californ 05000361
50-362 San Onofre Nuclear Station, Unit 3, Southern Californ 05000362 AUTHNAME AUTHOR AFFILIATION MEDFORDM,0, Southern California Edison Co. RECIP.NAME RECIPIENT AFFILIATION KNIGHTUNG.W. Licensing Branch 3
SUBJECT: Responds to NRC 830825 questions stemming from review of 830420 post-LOCA hydrogen monitor environ qualification package.Items include effect of chemical spray on various matis in hydrogen monitors.
DISTRIBUTION CODE: 1001$ COPIES RECEIVED:LTR . ENCL L SIZE.. TITLE: Licensing Submittal: PSAR/FSAR Amdts & Related Correspondence
NOTES:J Hanchett Icy PDR Documents. ELD Chandler icy, 05000361 J Hanchett Icy POR Documents. ELD Chandler Icy. 05000362
RECIPIENT COPIES RECIPIENT COPIES ID CODE/NAME LTTR ENCL ID CODE/NAME LTTR ENCL
NRR/DL/ADL 1 0 NRR LB3 BC 1 0 NRR LB3 LA 1 0 ROODH, 01 1 1.
INTERNAL: ELD/HOS2 1 0 IE FILE 1 1. IE/DEPER/EPB .36 3 3 IE/DEPER/IRb 35 1 1 IE/DQASIP/QAB21 1 . 1 NRR/DE/AEAB .1 0 NRR/DE/CEB 11 1 1 NRR/DE/EHEB 1 1 NRR/DE/EQB 13 2 2 NRR/DE/GB 28 2 2 NRR/DE/MEB 1 1 1 NRR/DE/MTE8 17 1 1 NRR/DE/SA8 24 1 1 NRR/DE/SGEB 25 1 1 NRR/DHFS/HFE640 1 1 NRR/DHFS/LQB 32 1 1 NRR/DHFS/PSR8 1 1 NRR/DL/SSPB 1 0 NRR/DSI/AEB 26 1 1 NRR/DSI/ASB 1 1 NRR/DSI/CPB 10 1 1 NRR/DSI/CSB 09 1 1 NRR/DSI/ICS8 16 1 NRR/DSI/METB 12 1 1 NRR/DSI/PSB 19 . 1 NRR/DI/RAB 22 1 .1 NRR/DSI/RSB 23 1 1 ILE 04 1 1 RGN5 3 3 RM/DDAMI/MIB 1 0
EXTERNAL; ACRS 41 b 6 BNL(AMOTS ONLY) 1 1 DMB/DSS (AMDTS) 1 1 FEMA-REP DIV 39 1 1 LPDR 03 1 1 NRC PDR 02 1 1 NSIC 05 1 NTIS 1 1
NOTES: 2 2
TOTAL NUMBER OF COPIES REOUIRED: LTTR 55 ENCL 48
Southern California Edison Company P. 0. BOX 800
2244 WALNUT GROVE AVENUE
ROSEMEAD. CALIFORNIA 91770
M.O. MEDFORD Ai 1984 TELEPHONE MANAGER, NUCLEAR LICENSING April 2, 1 (213) 572-1749
Director, Office of Nuclear Reactor Regulation Attention: Mr. George W. Knighton, Branch Chief
Licensing Branch No. 3 U.S. Nuclear Regulatory Commission Washington, DC 20555
Gentlemen:
Subject: Environmental Qualification of Post-LOCA Hydrogen Monitors Docket Nos. 50-361 and 50-362 San Onofre Nuclear Generating Station Units 2&3
On August 25, 1983, Mr. Hukam Garg of the NRC Equipment Qualification Branch contacted SCE regarding the post-LOCA hydrogen monitor environmental qualification package submitted on April 20, 1983. Responses were requested to six items resulting from the NRC's review of the package.
The purpose of this letter is to provide responses to the six items identified below. SCE believes that this submittal should satisfy any remaining concerns on the part of the NRC staff regarding post-LOCA hydrogen monitor environmental qualification.
Responses were requested to the following items:
Item 1
How was the hydrogen sensor qualified for chemical spray? Specifically, how does chemical spray affect the various materials in the hydrogen sensor?
Response
The chemical spray parameter is not applicable to the hydrogen sensor assembly. GE evaluated the sensor's material composition and determined that it was immune to the effects of chemical spray (see Attachment 1, telex dated August 22, 1978, from GE to BPC, log XB-21743, item NBR 4). Based on this analysis, caustic spray is not considered an applicable parameter for the sensor assembly.
8404050020 840402 PDR ADOCK 05000361 1 P UPDR
Mr. G. W. Knighton -2- April 2, 1984
Item 2
Provide a copy of the point specific radiation calculation.
Response
See Attachment 2. Note that as the transducer and sensor are located together, this calculation applies to both.
Item 3
Why was the seismic qualification test performed after the LOCA test?
Response
The applicable test report, GE Report 80SDS4244, para. 3.2, responds to this question. It is provided as Attachment 3. Note that such a change to the IEEE 323-1974 test sequence is allowed by section 6.3.2 of the standard which states "the sequence used shall be justified as the most severe for the item being tested."
Item 4
Explain how the post-LOCA qualification was extrapolated from 90 days to 120 days.
Response
See Attachment 4.
Item 5
For aging, how was the activation analysis extrapolated in the arrhenius calculation?
Response
Since the sensor assembly is only qualified for two years, it is considered that it will not age during that brief of a period, therefore, thermal aging was not considered applicable. Attachment 4 describes the post-LOCA aging evaluation.
Item 6
Provide documentation to demonstrate the pressure sensor in the monitor is qualified for 40 years.
Response
Appendix I of GE Report 80SDS4244 (Attachment 5) evaluates the pressure transducer materials of construction, and determined they were not susceptible to age-related degradation. Therefore, the assembly is inherently thermally qualified for 40 years. The transducer was tested to a total integrated dose of 3.2 x 107 rads (Attachment 6) and has only a total integrated dose requirement of 2.55 x 107 rads. The total integrated dose includes both a 40-year normal dose, a LOCA dose, and a 120-day post-LOCA dose. Therefore,
Mr. G. W. Knighton -3- April 2, 1984
the transducer is radiation qualified for 40 years. These two parameters (thermal and radiation aging) are the only two aging criteria applicable to the transducer assembly. Therefore, it is considered qualified for 40 years.
If you have any questions or comments, please contact me.
Sincerely,
Enclosures
cc: Mr. H. Rood, Project Manager Licensing Branch No. 3 Mr. J. B. Martin, Region V Administrator Mr. A. E. Chaffee, Resident Inspector
A e /ient Page 1 of 2
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SECTIONS A AND/ 5 O THE TECHNICAL SUKMARY CONTAIN st EXCEPTIONS.
THESE WERE DATArAXED TO YOU V/3 AS WELL AS SECTION I*
ITEM MBR to
REFER 1/Q St DOCUMENT 775DS434. APPENDIX LU P. -4
SL,.sOR * SCHE 323*1971
IEEE 344-1975
ELECTRONICS * IEEE 3t3-1974/ ISEISfIC ONLY/
IEEE 3t3.1971 ENVIRONMENTS
IEEEPage 2 of 2
ITEM mR 31
TME GE ANALYZERS ARC SUILT TO SPECIFICATION AND HAVE NO COOL
CLASSIFICATION*
ITEM agR as
CHEMICAL SPRAY WAS NOT USED IN THE SENSDR TESTS SINCE NATERI/ALS
USED IN ACTIVE PARTS O THE SENSOR ARE RELATIVELY IMMUNE TO
INORGANIC CHE04ICAL ATTACH.
A COVER OVER THE SENSOR LEADS IS /CURRENTLY Dr ALUMINUM AND IS
USED PRIMARILY FOR MEC14ANICAL PROTECTION O THE NETWORK*
AN ALTERNATE MATERIAL CAN BE SUBSTITUTE/D IF REQUIRED*
ITEM NUR So
SEISMIC TESTING# IF REQUIREDs WILL BE SCHEDULED FOR 4S-* DAYS ARO
AT A COST Or $9,576.
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.1GENERAL
TU primary Containment Hydrogen Monitoring System utilizes a hydrogen partial pressure
sensOr in conjunction with a total pressure sensor and appropriate electronic components to
dcate the percent of hydrogen present in the primary containment atmosphere.
2.2 SENSOR ASSEMBLY
The hydrogen partial pressure sensor is galvanic in nature and consists of a platinum black
electrode and platinum oxide counter electrode within a polysulfone housing. Figure 5
is a schematic of the sensor configuration. The electrolyte providing the ion conductive
path between the two electrodes is separated from the ambient atmosphere by a gas
permeable membrane which is in contact with the sensing electrode. When. the ambient
atmosphere contains hydrogen an electrical current is generated by the sensor which is
directly proportional to the partial pressuj; of the hydrogen in the atmosphere.
L \\I.HOUSING
SENSING ELECTRODE MEMBRANE
-COUNTER ELECTRODE
-EXPANSION BLADDER
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Figure 5. Hydrogen Sensor Schematic
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Test sequence recommended in IEEE 323-74 is:
Pretest Visual Inspection Baseline Functional Test Radiation Exposure Functional Test Aging Functional Test Seismic Qualification Functional Test LOCA Environment
Justifications of variations of the test sequence conducted and those listed above are:
Radiation: Radiation was done in two steps, half before LOCA and half after LOCA followed by a performance test and seismic test. This has three advantages over doing the entire radiation before LOCA simulation:
1. It more accurately simulates the actual condition where the radiation will occur before and after the maximum temperature and pressure extremes.
2. In exposing the sensor to radiation after the stresses of temperature and pressure, any unanticipated synergistic effects of the three stresses are more likely to be identified.
3. By dividing the radiation testing and making a performance measurement after each radiation exposure, any performance degradation trends could be identified. These would be useful in predicting end of life. No degradation due to radiation was detected at after either radiation exposure.
Aging: Because of the limited life of the sensor, aging is not an essential-step in the qualification testing. Appendix K provides further data on sensor aging.
The pressure transducer aging is described in Appendix I.
LOCA Before Seismic: The.H 2 Sensor is a simple device stable in structure and unlikely to be affected by the levels specified for a seismic event. It would be in a most susceptible condition for seismic damage after a LOCA type maximum temperature excursion. Therefore, the seismic testing was conducted post LOCA with subsequent performance testing and inspection.
3-3
.. o... .. ..-
Attachment 7
Page 1 of L/
The equipment has a 120-day post-DBA operability requirement. / :-r +o 4
demonstrates that the first 30 days post-DBA are adequately enveloped by
the first 30 days of the 90-day LOCA simulation/environmental exposure test
sequence. Operability during the remaining 90 days of post-DBA operation
can be demonstrated through use of the Arrhenius equation and taking credit
for the remaining 60 days of test data.
The Arrhenius equation is used to establish a time equivalency between two
data points using the activation energy of the age-susceptible material.
Since the two data points are defined (required operation of 90 days at
120 F, test operation of 60 days at 200 F), solving the Arrhenius equation
yields a required activation energy of only 0.092 ev in order to establish
a time equivalency between the two data points. 0.092 ev is essentially a
negligible requirement since most materials have activation energies from
0.6 to 1.3 ev, therefore, an age equivalency between the two data points
is established.
Attachment " Page -L '-I
As demonstrated pages 3 and"L) the SONGS 2 and 3 temperature
and pressure design envelope curves provide some margin over the actual tem
perature and pressure transients for the worst case LOCA scenario.
On pages I and q of this Attachment, the actual test curve, as described in
is superimposed on both the design envelope and actual transient
curves (for both temperature and pressure) in order to graphically demonstrate
the available margin for these parameters.
Attachment H
DESIGN ENVELOPE CURVE ACTUAL TEMPERATURE TRANSIENT FOR WORST CASE LOCA BASED ON: A. DOUBLE-ENDED SUCTION LINE BREAK (9.82 FT2
B. 2 COOLERS, 1 SPRAY
C. CONTAINMENT NET FREE VOLUME = 2.30 x 106 FT3
0. INITIAL CONTAINMENT TEMP 120 F
Q TEST CURVE
300
200- - - - 90 days
100
100 101 102 103 104 105 103 30 DAYS
TIME, SECONDS
SAN ONOFRE NUCLEAR GENERATING STATION
Units 2 & 3 CONTAINMENT ATMOSPHERE - TEMPERATUR2
VS. TILE LOSS-OF-COOLANT ACC:ENT (LOCA)
Fizure 3-1
Achment ( Page y L
DESIGN ENVELOPE CURVE ACTUAL PRESSURE TRANSIENT FOR WORSE CASE LOCA BASED ON: A. DOUBLE-ENDED SUCTION LINE BREAK (9.82 FT2
B. 2COOLERS,1SPRX 3 C.- CONTAINMENJ41ET FRE VOLUME = 2.30 x 106 FT
TEST C/V
60 PV
50 ,* ***..
40 90,* - -- ----- 9 0 days
** 5
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*CLASS. LTR. QPERATION PROGRAM SEQUENCE NO. REV. LTR.
EllERAL* ELECTRIt - U. 1 B50 CAMS_ 235 SPACE DIVISION Pin No.
nPHnaIA
PROGRAM INFORMATION REQUEST / RELEASE FUSE "C" FOR CLASSIFIED AND "U" FOR Wa ASSIFIED
a Jerry D. Fuller, Project Engineer To E.J. vitsky, Manager
Analyzer Programs Analyzer Programs Room U-3035 - Ext. 2518 Room U-3035 - Ext. 2956
DATE SENT DATE INFO. REQUIRED I PROJECT AND REQ. No. REFERENCE DIR. NO.
10/2/80 2F3 SUWECT
ACCELERATED LIFE TEST REPORT - CEC-1000 PRESSURE TRANSDUCER
INFORMATION REQUESTED/RELEASED
The aging procedure defined in PIR 1B90-CAMS-205 was completed on CEC Pressure Transducer
Part Number 1000-173, S/N 4240.
RESULTS
* Overall worse case change in performance occurred at 350*F and was a zero shift
of -. 413% of Full Scale. * Unit aging is unnecessary since pressure transducer contains
no age sensitive materials.
* Aging test served to increase confidence in component reliability.
SPECIMEN
The specimen included CEC Transducer S/N 4240, (see Attachment 1) mating connector P/N 170200
and -50 feet of cable fabricated from Raychem Spec. 44 twisted shielded pair.
DISCUSSION
Log of key test activity is summarized in Table 1 and followed by a brief description of
each.
TABLE 1
TEST LOG
ACTIVITY LOCATION DATE
Acceptance Test Procedure CEC 4/9/79
Dated 7/7/77
Accelerated Life Environment GE-SD 8/ 2/79 to 8/17/79
Radiation Exposure Isomedix, Inc. 9/79
Seismic .Event 'Acton, Acton, Mass. 10/79
Acceptance Test Procedure CEC 3/2/80
Dated 7/7/77
L, Heverly J. Murphyo _*_** *
F. DiSanto J. Fuller QOP19. Q ... E. Savltsky E. Wong (CEC) *-- 0 *as.
J. Ashly (CEC) 1OP ** 6 w""e gol etSTRO O
- - I-1
PIR 1B50-235 PAGE 2
0 0 Pre and Post Performance Tests
Both tests were performed at CEC to the 1000-04 (173) Acceptance Test Procedure dated 7/7/77 modified to include the linearity and hysteresis run at 250*F. Results were excellent with maximum deviation occurring at 350*F as a zero shift of -.413% of full range relative to the 4/9/79 test. The CEC calibration data summary is included with this report as Attachment 2.
Accelerated Life Environment, PIR 1B90-CAMS-205
To verify the long term operation requirements, the pressure transducer was subjected to the procedure presented in Attachment 3. The aging of the pressure transducer was performed by using present state-of-the-art aging technology. This technology allows acceleration of the time/temperature aging effects artificially by increasing the temperature. The pressure transducer contains both metallic and non-metallic components. The deterioration due to aging effects on the metallic components is judged to be insignificant. The aging of the pressure transducer was therefore based on its non-metallic materials only.
It is known for many non-metallic materials, that the degradation process can be defined by a single temperature-dependent reaction that follows the Arrhenius equation:
Ea - kBT
k = Ae (1)
where,
k = reaction rate
A = frequency factor
Ea = activation energy
kB = Boltzmann's Constant (8.617 x 10-5 eV/*K)
T = absolute temperature
1-2
PIR 1B50-CAMS-235 PAGE 3
It is further noted that, for many reactions, the activation energy can be considered to be constant over the applicable temperature range. Equation (1) can be transformed into a form which yields an acceleration factor to define a given amount of thermal degradation. The form is:
T (T T2 (2) *tl/t2 * e
where,
t1 accelerated aging time at temperature T1
t2 - normal service time at temperature T2
Ti - accelerated temperature T1 (OK)
T2 = normal service temperature T2 (oK)
Equation (2) can be used to derive the accelerated aging times for materials with known activation energies.
Normal operating temperature for the transducer is 1200F. The transducer was operated for 14 days at 300*F as presented in Table 2. From equation (2), this would age to greater than 40 years any material with an activation energy less than .81 eV. This would include most organic materials.
Aging Analysis
Table 3 describes the non-metallics in the pressure transducer. Both materials are included in the following list of materials that are considered to not have significant aging characteristics:
Silicon semi-conductors, resistors; tantalum dry electrolytic capacitors; ceramic capacitors; dry paper and plastic film capacitors; mica capacitors; glass capacitors; integrated micro-electronic devices; hybrid micro-circuits; steel, aluminum, copper, epoxy fiberglass GI1, Gl, or equivalent; brass, ceramic, and glass-filled diallylphthalate.
Since there are no age sensitive materials in the transducer, no aging prior to seismic is required. The temperature aging test serves as a confidence test in the pressure transducer reliability. A detailed "aging" test log is presented in Table 2.
No detectable change observed in unit performance or visual appearance.
S023 -508-17-18-0 1-3
N 0 0 PIR 1B50-CAMS-235 PAGE 4
TABLE 2
AGING TEST LOG
DATE ACTIVITY COMMENTS
7/19/79 Chamber Chamber atmosphere was Installation humidified with 15 ml H20.
7/19 -e8/2/79 Low Temperature 145*F with chamber total Operation pressure variation of
15.8 to 17.6 PSIA.
8/2/79 Initiate Aging Chamber was cooled to Environment ambient and opened to allow
transducer inspection. Atmosphere preparation included 1/2 atmosphere of 2% H2/N2 and water vapor (15 ml of water). Chamber was sealed and temperature set for 3000F.
Temperature Pressure Vo (OF) (PSIA) (my)
8-3 Aging Environment 302 53.5 18.739 8-6 "o 302 55.3 19.241 8-7 " 302 53.5 18.804 8-8 " 302 49.4 17.464 8-9 302 49.3 17.364 8-10 302 49.4 17.282 8-13 302 47.2 16.79 8-14 308 49.7 17.574 8-15 305 49.5 17.525 8-17 (8:30) 305 48.6 17.259 8-17 (15:00) 305 48.4 17.151 8-17 (15:10) Terminate Aging Set heat for 125*F
Environment 8-20 (11:45) 129 26.2 7.839
(11:50) Terminate Test Shut off heat, open the chamber and remove the specimen
1-4
PIR 1B50-CAMS-235 - -PAGE 5
TABLE 3
PRESSURE TRANSDUCER - NON-METALLICS
COMPONENT MATERIAL COMMENTS
Bridge Substrate Silicon Oxide S102 Thin coating to which resistors are mounted.
Resistors "Ceramicite" (CEC) Resistors are wire wound, Ceramic nickel coated with Ceramicite
which contains Al, Pb. Glass.
Radiation Exposure
The Transducer,connector and cable assembly was delivered to Isomedix for a radiation exposure of 1.2 x 106 Rads/hr. for a total integrated dose of 3.2 x 10/ Rads. Dose certification is included with this report as Attachment 4. No detectable change in unit performance or visual appearance was observed during post exposure evaluation.
Simulated Siesmic Event
The specimen was subjected to the environment described in GE-SD Procedure 250852 as part of H2 Analyzer P/N 47E240609 System Seismic Test. Test details are presented in the '609 system Qual Test Report.
,erry D. Fuller, Project Engineer Edward4. Savits Analyzer Programs Analyter Progra s Room U-3035 - Ext. 2518 Room U-3035 - Ext. 2956
/mes
S023 -50 8 -17-18 -0
1-5
CEC' 100(Y4 Sputtered Th fFilm Higfi Temperature
Pressure Transducer
* .0ng-Te17 Stab Providing long-term stability and reliability, CEC Sputtered Gage Pressure Transducers are the most accurate thin film transducers available. Performance stability is =0.1% for extended operation at any combination of constant pressure
* H ly Reloble and temperature within the operating range. The CEC 1000-04 has a compensated temperature range of 75'1 to -. 00*F, and an operable temperature range of -650F to +450*F. The thermal errorband performance is typically better than o High Performo nce 0.5% within any 500F temperature band.
Advanced techniques of sputtered film deposition create sensing elements with a maximum combined error for non
Ad nced Sensor Design linearity, hysteresis, and non-repeatability of =0.25% of the full range output
Available in many standard ranges from 15 to 10,000 psi, the CEC 1000 Series also feature an innovative double-case
* Rugged Dual COse Isolation isolation. The basic sputtered sensor is electron beam welded to the pressure chamber/adapter which also provides a high degree of mechanical isolation from mounting torque effects. The sputtered sensor is well isolated from external case effects since the case is welded to the pressure chamber/adapter and not in contact with any portion of the sensor.
CEC Sputtered Gage Pressure Transducers are manufactured in accordance with the program quality requirements of MIL*Q-9858A.
For further information about this pressure transducer, or special application designs, contact the nearest Bell & Howell/CEC Division Sales Office or factory in Pasadena. California.
. . CEC DIS10
BELL s HOWELL 1-6 ATTACHiENT I
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. . @ BELLsHOWELL ATTACUMENIT 1
.I BELLsHOWELL CEC DIViSIDn 0 360 S "OftA MADE VILLA. PASADENA. CA esU TLEPHONE (23)M76938 TELEX. 87.5415
CALIBRATION DATA SUMMARY
CEC 1000-0173 S/N 4240
0-100 PSIA
77*F +ZSOF 350'F 77*F Temperature *B *A ** *A *3 *A *B *A
Full Scale (MV) 33.389 33.504 34.100 34.260 34.1749 34.188 33.368 33.486
Zero (MV) 0.262 0.353 0.855 0.924 0.732 0.594 0.253 0.350
Sens. (MV) 33.127 33.151 33.245 33.336 33.417 33.594 33.115 33.136
Insulation Resistance 10KMD 10MG 10KMm 10a 51Q42 51Mf 53M 10140
AZero (MV) +C.091 .0.069 -0.138 +0.097
ASens. (MV) *0.024 *0.091 *0.17; +0.021
AZero (%ER) . +0.275 +0.208 -0.413 *0.293
ASens.(%FR) +0.072 *0.274 +0.530 +0.063
LINEARITY AND HYSTERESIS RUN AT +2500F
VS 0 20 40 60 80 100 80 60 140 20 *3 0.855 7.473 14.115 20.769 27.430 34.099 27.438 20.776 14.12217.482 0
*A I0.9247.58 114.223 20.896 127.579 134.268127.586120.903 14.22917.568 0 *B is before radiation 4/09/79 *A is after radiation 3/20/80.
, bE. -ong Sr. ProductSpecialist
1-8 ATTACHMENT 2
E ENERAL ELECTI *s. ow n mosAw aSEsso. .gv sPAI omn . U 1B90 CAMS 205
PROGRAM INFORMATION REQUEST /REASE *as *c Lo UsswIFe Mo **tr* Iran uncussan FROM TO
J.- D. Fuller, Project Engineer F. P. Rudek, Manager - Analyzer Systems
DATE SNT DATE INFO. REQUIRD PROECT AD REQ. NO. RERUCE DIR. no.
7-25-79 Auadc=
CEC-1000-04(173) Pressure Transducer Aging Procedure INFORMATION REQUESTED/RELEASED
The purpose of this test is to subject the transducer proposed for current configuration H2 Analyzers to a combination of environmental conditions simulating long term operation-of the transducer.
1. Initial Conditions:
a. Place 30 al H20 in the chamber prior to closing.
b. Pressurize the chamber to 15 PSIG with 2% HZ/N2 then vent to ambient pressure. Close inlet and outlet valves.
c. Set the temperature for 135oF + 50F.
d. Record the following data for stabilized sensor performance.
- Temperature Pressure Transducer Output
- Time (Date and Time of Day)
2. Accelerated Life Temperature, Pressure Conditions: 4100 a. Set temperature controller to achieve a chamber temperature of 3000
b. Upon achieving a chamber temperature of 3000F, record the time and date. Vent the chamber as required to maintain a chamber pressure c 65 PSIG.
c. Maintain the conditions established in the preceding step for 14 days and record the following information daily:
- Temperature - Pressure * Sensor Output - Time
cc: J. 0. Fuller J. E. Murphy PAnn s maa.n N e urn..vy
L. R. Heverly F. F. Rudek cop0ms O. I _._._spoll
J asWes. t 3 awes. IOP Wses. se es.
m ATTACHMENT 3 1F=__0=_W__ "0
-2
d. Decrease the temperature setting to achieve a chamber temperature of 125 + 50f and maintain for 2 .days. Daily record the data noted in step 2.c.
e. Shut off the heat, open the test chamber and remove the transducer for visual inspection.
3. Radiation Exposure:
a. Subject the transducer to a total integrated dose of 3.2 x 107 Rads at a rate of 1.2 megarads/hour.
b. Perform CEC ATP.
.0Fuller, Project Engineer Analyzer Systems Room #U-3035, VFSCExtension -2518
h
I-10 ATTACHMENT 3
ISQMEDIX
Sept. 13, 1979
J. J. Collexy General Electric Company Space Systems P.O. Box 8555 Philadelphia, Pa. 19101
Dear Mr. Collery:
This will summarize parameters pertinent to the irradiation of CEC XDUCER, calibration cap and cylinder, as per your purchase order A28-A10311, dated August 28, 1979.
The specimens were exposed for 37 hours at-an average dose rate of 1.0 Megarads per hour, yielding a dose of 37 Megarads. The. specimens were over-irradiated to account for the t3% accuracy of the the dosimetry system; the reported dose is 32.Megarads.
Halfway through the exposure, the specimens were rotated 1:800 to give a more uniform dose distribution.
Dosimetry was performed using Harwell Red 4034 Perspex dosimeters, utilizing a Bausch and Lomb Model .710 spectrophotometer as the readout instrument. This system is calibrated directly with NBS, with the last. calibration being May 30, 1979.. A copy of the dosimetry correlation report is available upon request.
Irradiation was conducted in air at ambient temperature and pressure. Radiant heat from the source heated the samples somewhat, but the temperature did not exceed 1300F, as indicated by previous measurements on an oil solution in the same relative position.
Irradiation.was initiated on August 31, 1979, and was completed on September 2, 1979.
. Sincerely yours,
ISOMEDIX, INC.
David P. Constantine Production Manager
DPC:vt . CC: G. Deit:
Isamedix Is. * 25 Eastmans Road. Parsippany, New Jersey 0704 * (201) 87-2566 ATTACHMENT 4
Chemical spray was not included in the LOCA testing because the exposed materials are the same as those used in Oxygen Sensors which contains a much stronger basic solution of 50% KOH.
3.3 SUPPLEMENTARY TESTS
1. Top Assembly Seismic Test - This test was performed to demonstrate the H2 Containment Atmosphere Monitoring System ability to withstand simulated seismic vibration. Note that all analyzer components described in Paragraph 1.3.4 were included. Detailed test results are presented in Appendix F.
2. Pressure Transducer Tests - The pressure transducer underwent an aging test to demonstrate long term operation. The environment included elevated temperature of 300*F and a radiation exposure of 3.2 x 107 Rads TID. Detailed description of the test and results are presented in Appendix I.
The transducer was not subjected to a separate LOCA pressure and temperature profile. The CEC predelivery test environment, Appendix G, exceeds the maximum predicted LOCA conditions for temperature and pressure. The testing in Appendix I includes 14 days of continuous operation above 300*F and 48 PSIA. In addition, the acceptance test on the pressure transducer (Appendix G) includes short term testing at 400*F and two times rated pressure (200 PSI). These combined conditions stress the pressure transducer far beyond the conditions of the SONG 2 and 3 LOCA profile.
3-4