ML20112J719
| ML20112J719 | |
| Person / Time | |
|---|---|
| Site: | 05000000, Shoreham |
| Issue date: | 02/04/1985 |
| From: | Field D KAMAN INSTRUMENTATION CORP. |
| To: | |
| Shared Package | |
| ML20112J710 | List: |
| References | |
| 460036-002, 460036-002-R-A, 460036-2, 460036-2-R-A, NUDOCS 8504050286 | |
| Download: ML20112J719 (505) | |
Text
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{d ** QUALIFICATION REPORT FOR MODEL KDI-1000 HIGH RANGE I CONTAINMENT AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM 460036-002, REV. A i l KAMAN INSTRUMENTATION CORPORATION P. O. B0X 7463 COLORADO SPRINGS, COLORADO 80933-7463 8504050286 e50402 PDR ADOCK 05000322 S ppg
APPLICATICN REVISIOfeS j N E X T ASS *Y USED ON REV DE SC RIP TION DATE APPROVED 1 A Ordinal Re lease ser Eco 3007.1 G/V/rf hl, QUALIFICATION REPORT FOR MODEL KDI-1000 HIGH RANGE CONTAINMENT AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM 460036-002 Rev. A KAMAN INSTRUMENTATION P.O. BOX 7463 COLORADO SPRINGS, COLORADO 80933 MATER l AL ****" " AllA Maman instrumentation Corporation CHECKED COLORADO SPRINGS. COLORADO FINISH %M'df[/A I/gf/gf
' QUALIFICATION REPORT FOR MODEL KDI-1000 D/7/d , N, /,/ 2/[/r. , HIGH RANGE CONTAlf4 MENT AREA RADIATION DETECTOR UNLE SS OTHE RWISE PROD *
/ AND MINERAL-INSULATED CABLE SYSTEM A ININCHES PROJ CODE IDE NT NO. SIZE DWG. NO. R E V.
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. M M M = 1.010 APPROVE D /TO 2,8 A 460036-002 A CONT R ACT NO. SCALE SPEC SHT OF ANGLE S = 108 3, 1 34 Ki-E NG10 6
CERTIFICATE OF QUALIFICATION for Model KDI-1000 High Range Containment Area Radiation Detector and Mineral-Insulated Cable System Kaman Instrumentation Corporation hereby certifies that the Kaman Model KDI-1000 High Range Containment Area Radiation Detector and Mineral-Insulated Cable System was tested in accordance with Kaman Specification 460036-001. The results of the tests indicate that the Detector and Cable System are suitable for application as Class 1E safety-related instrumentation service within the limitations described here-in.
. l%<1-ko Y Quality As'surancefanager Date k f l90$
Kaman Instrumentetton Corp. En'gineering MaYager ' l ~ Date Z '
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Kaman Instrumentation Corp. e 1 I 2
l l l TABLE OF CONTENTS 4 Page SPECIFICATION COVER SHEET AND REVISION RECORD . . . . . . . . . . . . . . . 1 CERTIFICATE OF QUALIFICATION. . . . . . . . . . . . . . . . . . . . . . . . 2 I TABLE OF. CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
~ LIST OF FIGURES AND PHOTOGRAPHS . . . . . . . . . . . . . . . . . . . . . . 4 LIST OF TABLES ...........................s .. 4 i
LIST OF APPENDICES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 1.0
SUMMARY
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 1
2.0 CONCLUSION
S . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 3.0 GENERAL NOTES AND DEVIATIONS. . . . . . . . . . . . . . . . . . . 5 3.1 Purpose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
; 3.2 . Deviations. . . . . . . . . . . . . . . . . . . . . . . . . . . 11 4.0 TEST ARTICLES . . . . . . . . . . . . . . . . . . . . . . . . . 11 4.1 Detector /Cabl e System 1 . . . . . . . . . . . . . . . . . . . . 13 4.2 Detector / Cable System 2 . . . . . . . . . . . . . . . . . . . . . 13 j 4.3 Penetration Connector System 3. . . . . . . . . . . . . . . . . 13 j 4.4 Penetration Connector System 4. . . . . . . . . . . . . . . . . 14 1 4.5 Reference Cable System 5. . . . . . . . . . . . . . . . . . . . 14 i 4.6 Reference Cabl e System 6. . . . . . . . . . . . . . . . . . . . 14 a
l 5.0 TEST ACTIVITY. . . . . . . . . . . . . . . . . . . . . . . . . . 15 5.1 Mounting Configuration . . . . . . . . . . . . . . . . . . . . . 15 5.2 Detector Calib ration . . . . . . . . . . . . . . . . . . . . . . 15 5.3 Aging Test . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 5.3.1 Aging Tests Performed. . . . . . . . . . . . . . . . . . . . . . 16 5.3.2 Mechanical Aging Test Results. . . . . . . . . . . . . . . . . . 16 t 5.4 I rra di a tion Exposu re Tes t. . . . . . . . . . . . . . . . . . . . 16 5.4.1 Irradiation Tests Performed. . . . . . . . . . . . . . . . . . . 16 . 5.4.2 Irradiation Test Results . . . . . . . . . . . . . . . . . . . . 16 i- 5.5 Seismic Testing. . . . . ... . . . . . . . . . . . . . . . . . . 17
! 5.5.1 Seismic Tests Performed. . . . . . . . . . . . . . . . . . . . . 17 j 5.5.2 Seismic-Test Results . . . . . . . . . . . . . . . . . . . . . . 17-i 5.6 Recove ry Acti vi ty. . . . . . . . . . . . . . . . . . . . . . . . . 17 LOCA Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . , 5.7 18 i 5.7.1 LOCA Tests Performed . . . . . . . . . . . . . . . . . . . . . . 18 4
' 5.7.2 LOCA Test Results. . . . . . . . . . . . . . . . . . . . . . . . 18 i 5.7.2.1- Triax Sheath . . . . . . . . . . . . . . . . . . . . . . . . . . 18 5.7.2.2 . Detector Temperature Coefficient . . . . . . . . . . . . . . . . 19 5.7.2.3 Connector Leakage. . . . . . . . . . . . . . . . . . . . . . . . 19 5.7.2.4 Thermal Transient Behavior . . . . . . . . . . . . . . . . . . . 21 l 5.8 Detector Calibration -(Post-Qual) . . . . . . . . . . . . . . . . 21 ! 6.0 - EVALUATION AND FUNCTIONAL TEST RESULTS . . . . . . . . . . . . . 22 3 i 1
,_ _ , - , - - 4 . _- .. ~ . . _ . _, . . ~ _ _ _ _ . . ,,- . . ~ . .
, LIST OF FIGURES AND PHOTOGRAPHS Page Fig. 1 -
RRS for Vibration Aging . . . . . . . . . . . . . . . 7 Fig. 2 - RRS for OBE Seismic Test. . . . . . . . . . . . . . . 8 Fig. 3 - RRS for SSE Sei smic Test. . . . . . . . . . . . . . . 9 Fig. 4 - L OCA Te s t P ro fi l e . . . . . . . . . . . . . . . . . . 10 Photograph 1 - Test articles as mounted. . . . . .. . . . . . . . . . 12 LIST OF TABLES TABLE I - Summary of Qualified Parts. . . . . . . . . . . . . . 6 TABLE II - Environmental Parameters .............. 6 TABLE III - Summary of Evaluations and Functional Test Data . . . 23 LIST OF APPENDICES APPENDIX A - 460036-001 Rev. A, QUALIFICATION OF MODEL KDI-1000 HIGH RANGE AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM APPENDIX B - DEVIATIONS, ANOMALIES AND FAILURE REPORTS APPENDIX C - DETECTOR CALIBRATION (KNP AND DATA SHEETS) APPENDIX D - MECHANICAL AGING DATA SHEETS APPENDIX E - IRRADIATION TEST DATA APPENDIX F - SEISMIC TEST DATA APPENDIX G - LOCA TEST DATA APPENDIX H - DETECTOR N.T.C. INVESTIGATION APPENDIX I - TORQUE MAINTENANCE INVESTIGATIONS APPENDIX J - EVALUATION AND FUNCTIONAL TEST DATA RECORDS APPENDIX K - THERMAL TRANSIENT INVESTIGATIONS (. 4
l QUALIFICATION REPORT FOR MODEL KDI-1000 HIGH RANGE CONTAINMENT AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM 460036-002 Rev. A 1.0
SUMMARY
A Kaman model KDI-1000 High Range Containment Area Radiation Detector and Mineral Insulated Cable System was subjected to a series of qualification tests including mechanical aging, irradiation exposure, vibration aging and seismic tests, and simulated LOCA tests. The Class lE function of the system is for use in determining the magnitude of the release of radioactive materials and continually assessing such releases. The system provides information display to the operator for this function. The System demonstrated its capability to perform its Class IE function during and after these design basis accident exposures. Based on these tests, the System is qualified and suitable for service in a Safety-Related Instrumentation system to satisfy the Containment Area Radiation
- High Range monitoring requirements stated in USNRC Regulatory Guide 1.97 " Instrumentation for Light-Water-Cooled Nuclear Power Plants to Assess Plant and Environs Conditions During and Following an Accident."
2.0 CONCLUSION
S As evidenced by the results of this qualification test activity, the Kaman model KDI-1000 High Range Containment Area Radiation Detector and Mineral-Insulated Cable system, consisting of the parts listed in Table I, is qualified as Class IE safety-related electrical equipment in environments enveloped by the parameters listed in Table II and shown in Figures 1-4. The qualified life of the detector and cable system is 40 years and is based on mechanical cycling considerations since no organic materials are used. 3.0 GENERAL NOTES AND DEVIATIONS 3.1 Purpose The purpose of this document is to report the qualification activities performed on the Detector and Cable System. The main body of this document presents the test results in summarized and reduced form. Complete and unreduced data are presented in appendices to this document for more detailed examination by the reviewing authority. The controlling document which presents in detail the qualification plan and test procedures that were followed throughout this qualification test activity is Specification No. 460036-001, Rev. A. This dccument is included as Appendix A to this report. l 5
TABLE I
SUMMARY
OF QUALIFIED PARTS Kaman P/N Rev. Level Description 824636-003 B lon chamber detector 450593-001 J Ceramic mount ass'y 952701-001 A Captive mount ass'y. 852562-001 A Female bulkhead connector 852552-001 A Female connector 852553-001 A Hale connector 825284-001 B Mineral-insulated cable 852568-XXX A Male-male cable ass'y 852569-XXX A Male-female cable ass'y. 852570-XXX A Female-female cable ass'y. 813764-001 A Protective plug 813763-001 A Protective cap 825335-013 B Metal 0-ring TABLE II ENVIRONMENTAL PARAMETERS
- Irradiation: 2.2 x 100Rads (air) - gamma, TID Vibration Aging: 30 minutes each axis; biaxial random multiple frequency i input motion - see Figure 1 for RRS.
Seismic: Five 0 30 second duration OBE's plus one @ 30 second duration SSE each axis. Independent biaxial random multiple frequency input motion - see Figure 2 for RRS for OBE's and Figure 3 for SSE's. LOCA: Maximum Temperature - 382 F Maximum Pressure - 70 psig Chemical' Spray - 4400 ppm boric acid buffered by Na0H to pH = 10.5 for 26.5 hrs at 0.15 gpm/ft2 (See DAFR-16) See Figure 4 for LOCA test profile. Life: 90 hand-tight plus 30 full-torque cycles per connection.
- These parameters include margin.
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] 1 2 3 4 5 678910 2 3 4 5 6 789100 200 l Frequency (Hz) FIGURE 1 . a j RRS FOR VIBRATION AGING l i 1 l
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3 - 2.5 6 l 1.5 - { 1 1.5 2 2.5 3 4 5 6 7 8910 15 20 25 30 ,40 50 60 70 80 90 100 Frequency (Hz) ! FIGL)RE 2 RRS FOR OBE SEISMIC TEST 2% DAMPlNG i
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- Add Mergio By Pro. Conditioning The Equipment With The First 2 Hours Of This Profile After initial transs.ent, limit rates of temperature change *
- Temperatures Shown include to<200 F/hr and pressure changes to < 20 pee /hr ,, j$o F. Pres h 12
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W1 0A1 0.1 1.0 to too 1000 10,000 FIGURE 4 LOCA AND POST-ACCIDENT TEST PROFILE
3.2 Deviations Deviations from the general plan and detailed procedures (see Appendix A, Specification 460036-001, Rev. A) were allowed after full evaluation and l approval by the Kaman Qualifications Engineer. Each deviation is noted on l a Deviation, Anomalies, and Failures Report. The following Deviations Anomalies, and Failure Reports were processed and are summarized below (see l Appendix B for completed reports): i DAFR-1 Required photographs to be taken during various phases of the test activity. DAFR-2,5 Added shipping and storage, and operational thermal cycling tests per IEEE-317, to two test articles. DAFR-3,4,6,7,8 Revised or added test article identification and P/N's or S/N's to represent the as-tested components. DAFR-9,10,13 Modified number of torque cycles and torque value to be applied to certain test articles. DAFR-11 Modified TID uniformity during irradiation. DAFR-12 Allowed dose mapping and time rate dosimetry for TID. DAFR-14 Deleted voltage withstand test on signal cables for pre-seismic functional test. DAFR-15 Changed sequence of electrical tests. DAFR-16 Required chemical spray to be applied only during non-superheat conditions. DAFR-17 Controlled activities occurring between seismic and LOCA testing. DAFR-18 Deleted one of two evaluation tests required at 380 F LOCA and modified tests applied to signal cables. DAFR-19 Permitted natural cool-down of autoclave after LOCA. 4.0 TEST ARTICLES The tested items consisted of six (6) principle assemblies mounted on a test platform. These assemblies are described in the paragraphs below. Refer to Photograph 1 for illustration. Note that " SPEC.REF." refers to the reference paragraph in Specification 460036-001, Rev.A(seeAppendixA). 11
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*- 2.5.6 3 Photograph 1 Test Articles as Mounted
4.1 Detector / Cable System 1 Description Part No., Rev. Serial No. Spec. Ref. High Voltage Cable Ass'y 852569-066, Rev. A 76604-02 2.5.1.1 Male Connector 852553-001, Rev. A 2.5.1.1.1 MI Cable 825284-001, Rev. B 2.5.1.1.2 Autoclave Feed-Thru Ass'y (Note 1) 2.5.1.1.3 Female Connector (Note 2) 2.5.1.1.4 Signal Cable Ass'y 852569-127, Rev. A 76602-02 2.5.1.2 Male Connector 852553-001, Rev. A 2.5.1.2.1 MI Cable 825284-001, Rev. B 2.5.1.2.2 Autoclave Feed-Thru Ass'y (Note 1) 2.5.1.2.3 Female Connector (Note 2) 2.5.1.2.4 Detector Ass'y Ion Chamber 824636-003, Rev. B 14624 2.5.1.3.1 HV Female Bulkhead 852562-001, Rev. A 2.5.1.3.1.1 Connector Sig Female Bulkhead 852562-001, Rev. A 2.5.1.3.1.2 Connector Metal 0-Ring (2 ea.) 852335-013, Rev. B Captive Mount Ass'y 952701-001, Rev. A 2.5.2.3.2 4.2 Detector / Cable System 2 Description Part No., Rev. Serial No. Spec. Ref. High Voltage Cable Ass'y 852569-146, Rev. A 76603-02 2.5.2.1 Male Connector 852553-001, Rev. A 2.5.2.1.1 MI Cable 825284-001, Rev. B 2.5.2.1.2 Autocalve Feed-Thru Ass'y (Note 1) 2.5.2.1.3 Female Connector (Note 2) 2.5.2.1.4 Signal Cable Ass'y 852569-127, Rev. A 76602-01 2.5.2.2 Male Connector 852553-001, Rev. A 2.5.2.2.1 MI Cable 825284-001, Rev. B 2.5.2.2.2 Autoclave Feed-Thru Ass'y (Note 1) 2.5.2.2.3 Female Connector (Note 2) 2.5.2.2.4 Detector Ass'y Ion Chamber 824636-003, Rev. B 22710 2.5.2.3.1 HV Female Bulkhead Connector 852562-001, Rev. A 2.5.2.3.1.1 Sig Female Bulkhead Connector 852562-001, Rev. A 2.5.2.3.1.2 Metal 0-Ring (2 ea) 825335-013, Rev. B Ceramic Mount Ass'y 450593-001, Rev. J 2.5.1.3 4.3 Penetration Connector System 3 Description Part No., Rev. Serial No. Spec. Ref. Male Stub (Plugged) 852569-146, Rev. A 76603-01 2.5.3.1 Male Connector 852553-001, Rev. A 2.5.3.1.1 Protective Plug 813764-001, Rev. A Metal 0-Ring 825335-013, Rev. B MI Cable 825284-001, Rev. B 2.5.3.1.2 , Autoclave Feed-Thru Ass'y (Note 1) 2.5.3.1.3 Female Connector (Note 2) 2.5.3.1.4 I i 13 l l
. - . . . . . . . . - -. =_. .- . - - . . -. .- .
i , - FemaleStub(Capped) 852570-072, Rev. A 76606-01 2.5.3.2 Female Connector 852552-001, Rev. A 2.5.3.2.1 !~ Protective Cap 813763-001, Rev. A 4 Metal 0-Ring 825335-013, Rev B MI Cable _ .
-825284-001,-Rev. B 2.5.3.2.2 Autoclave Feed-Thru Ass'y (Note 1)- 2.5.3.2.3 ,
- Female Connector (Note 2) -2.5.3.2.4 I
!~ ! 4.4 Penetration. Connector System 4 i Description _
'Part No., Rev. Serial No. Spec. Ref.
Male / Female Cable Ass'y 852569-066, Rev. A 76604-01 2.5.4.1 Male Connector 852553-001, Rev. A 2.5.4.1.1 i Metal 0-Ring 825335-013, Rev. B MI Cable 825284-001, Rev. B 2.5.4.1.2 Autoclave. Feed-Thru Ass'y (Note 1) 2. 5. 4.1. 3
, Female Connector (Note 2) 2.5.4.1.4 i Female / Female Cable Ass'y 852570-075, Rev._A 76605-01 2.5.4.2 '
Female Connector 852552-001, Rev. A 2.5.4.2.1 MI Cable 825284-001, Rev. B -2.5.4.2.2 Autoclave Feed-Thru Ass'y (Note 1) 2.5.4.2.3-l Female Connector (Note 2) 2.5.4.2.4 l 4.5 Reference Cable System 5 t Description Part No., Rev. Serial No. Spec. Ref.
- Special Cable Ass'y (Note 3) 79903-01 2.5.5.1 i -Autoclave Feed-Thru Ass'y (Note 1) 2.5.5.1.2 MI Cable- 825284-001, Rev. B 2.5.5.1.1 Autoclave Feed-Thru Ass'y (Note 1) 2.5.5.1.3 i
j 4.6 Reference Cable System 6
~
Description Part No., Rev. Serial No. Spec. Ref. Special Cable Ass'y (Note 4) 52A 2.5.6.1 hw'- MI Cable Special Cable Ass'y 825284-001, Rev. B 2.5.6.1.1
- (Note 5) 528 2.5.6.2 ;
j MI' Cable 825284-001, Rev. B 2.5.6.2.1 ! Special Cable Ass'y (Note 6) 2.5.6.3 MI Cable 825284-001, Rev. B I NOTES: l_ 1. Autoclave Feed-Thru Ass'y is special test hardware used for pressure i boundary around MI cable at points where cable' passed through ports in i flange on autoclave. This hardware is not considered to be a test specimen. L 2. These Female Connectors are similar to P/N 852552-001, Rev. A. They 6 ! are called " test-interface" connectors and were used as the connection i point for leads and cables _ from test equipment, such as the megohnuneter, picoammeter, etc. They were not subjected to the simulated LOCA environment. -These connectors are not considered to be test specimens. 14 l
-. , <- n ,.-,-,-,n- , , . . . - , - . . . - , . , , , , - .- . , ~ , , - + . . ,
l j -3. This special cable assembly consisted of a loop of MI cable only with
^
seals and exposed conductors on each end. Both ends of this loop passed through "Autocl 'e Feed-Thru Assemblies" and were located
- outside the autoclave during the LOCA test. The purpose of .this assembly was to measure and verify the characteristics of the cable r alone without the influence of connectors.
l
- 4. This cable assembly consisted of a 60 in. length of cable with a metal cap welded on each end. It was mounted to the outside of a 1" conduit using "ty-wraps" spaced at 12,18, and 24 inches.
- 5. This cable assembly consisted of a 60" length of cable with a metal cap welded on each end and a 10 mil deep by 1 inch long longitudinal defect intentionally scored into - the outer sheath at approximately mid-span. It was mounted to the outside of a 1" conduit using "ty-wraps" spaced at 12,18, and 24 inches.
- 6. This cable assembly consisted of a 66 in. length of cable with a metal cap welded on each end. It was mounted inside a 60 inch long section of 1" conduit and supported by a swage fitting centered in each end of the conduit. (Distance between supports = 60 inches.)
5.0 TEST ACTIVITY 5.1 Mounting Configuration At the start of the test activity, twelve cables and two detectors were mounted on a test platform in accordance with Appendix A, paragraph 3.1.1, to simulate different mounting techniques. One detector was mounted in a ceramic holder, the other in a captive metal mount. Most cables were clamped (using standard single clips McMaster-Carr 5192K12) to the test platform at intervals of 12 inches or less; and 3 cables were mounted to a 1" conduit, one inside and two "ty-wrapped" (Panduit PAN-TY-TEFZEL(C76)) to its outside. One of the Penetration Connector Systems, test articles 76603-01 and 76606-1, was not mated for the qualification tests. Instead, to qualify an installed spare configuration, the male connector was plugged and the female connector was capped. 5.2 Detector Calibration In accordance with Appendix A, paragraph 3.1.2, the detectors were subjected to a gamma calibration per procedure KNP 18-104. The nominal detector efficiency of test article 14624 was 0.91E-11 A/R/hr. The nominal dctector efficiency of test article 22710 was 0.97E-11 A/R/hr. These values are within the tolerance specified for these detectors. Refer to Appendix C for procedure and data sheets on detector calibration. 15
5.3 Aging Test 5.3.1 Aging Tests Performed As there are no organic materials involved in the design of the detectors, connectors, or cables, no thennal aging was performed. In accordance with Appendix A, paragraph 3.1.4, mechanical cycle aging consisting of 90 hand-tighten cycles and 30 torque-cycles was performed on the mating connectors of test articles 76603-02 and 76602-01 with detector 22710, and ten hand-tighten cycles and five torque cycles was performed on the in-line mated connector pair, test articles 76604-01, ana 76605-01. No other connectors were mechanically aged. 5.3.2 Mechanical Aging Test Results A portion of ceramic dielectric material and a spring finger contact (one of four per connector) broke off the female H.V. connector of the ion chamber test article 22710 midway through the mechanical aging test. The aging test was completed and all electrical parameters remained within specification. The damaged connector was mated and torqued "as-is" and subjected to the remainder of the qualification tests. At the conclusion of the mechanical aging tests all connectors were torque-tightened to 25 - 28 ft-lb. Refer to Appendix D for data sheets on mechanical aging. 5.4 Irradiation Exposure Test 5.4.1 Irradiation Tests Performed The irradiation test was performed by International Nutronics, Inc., Irvine, California. In accordance with Appendix A, paragraph 3.1.8, the test platform with all test articles mounted was exposed to a (minimum) total integrated dose of 200 Megarads (air) radiation from a Co-60 source at a dose rate of 1.67 Megarads per hour. One ion chamber and cable system (System No. 2) was operating and monitored throughout the irradiation exposure. The other test articles were not energized nor monitored during the irradiation exposure. Refer to Appendix E for irradiation certification. 5.4.2 Irradiation Test Results Two transients from 1 o 'e . ds/hr to less than 1 rad /hr and from less than 1 rad /hr to _.b) e: grads /hr were performed near the end of the irradiation expcs.ure. Stt'ip chart records of the signal from ion chamber 22710 confirmed the operation of the detector / connector / cable system (test articles 76603-02, 76602-01, and 22710). The response of the detector closely tracked the movement of the source which was approximately 20 seconds from minimum to maximum exposure. 16
, The environment of the Co-60 cell included a large open pool of water directly below the test articles. This, and the high humidity and relatively poor atmospheric conditions (smog) at the facility , continually plagued the gathering of test data. Contamination, i especially by moisture, rapidly degrades the ability of un-terminated connectors to support the high insulation resistances required. Vacuum-drying and/or heat drying the test-interface connectors (not
- the connectors involved in qualification) recovered the caETe l
l assemblies to above their respective minimum specifications. 5.5 Seismic Testing 5.5.1 Seismic Tests Performed The seismic tests were performed by Wyle Laboratories, Norco, California. The test platform with all test articles mounted and both ion chambers operating was attached to an independent biaxial seismic ( simulator. In accordance with Appendix A, paragraph 3.'1.12 , a resonance search, vibration aging test, and 5 OBE and 1 SSE seismic simulations were performed in each axis. See Appendix F for seismic test data. 5.5.2 Seismic Test Results No failures were experienced during any of the vibration tests or seismic simulations, although continued difficulty with moisture contamination prompted return of the test articles to the factory prior to the LOCA test. , l 5.6 Recovery Activity During the pre-seismic difficulties with moisture contamination it was noticed that one of the connectors had loosened to a hand-tight condition. The connector was re-torqued and parallel investigations were begun at the factory to determine the cause. It was initially determined that 25 - 28 ft. - lb. may have been insufficient torque to compress the metal o-ring completely into its seat to allow the mechanical stops of the connector to engage sufficient torque-lock on the threads. It was also suspected that the lack of torque maintenance on all the detector connectors had compromised their hermetic seal and allowed contamination in the form of l moisture to enter the connector body. Upon return of the test articles to the factory prior to LOCA, the four detector (qualification) connectors were unmated and dried using a vacuum bake-out technique. The connectors were re-mated, torqued, and the connectors on Ion Chamber 14624 were locked using jam nuts. Also, all test-interface connectors were vacuum-baked. This activity is reported in detail in DAFR-17; see Appendix B. 17
f 5.7 LOCA Tests 5.7.1 LOCA Tests Performed The simulated LOCA test was performed by Wyle Laboratories , Huntsville,' Alabama. In accordance with Appendix A, paragraph 3.1.16, the -test platfonn.with all test articles mounted and both ion chamber detectors operational was mounted- in a horizontal-axis autoclave and exposed to two cycles of a simulated - loss-of-coolant accident. The-temperature attained was 382 F in thirteen seconds. The pressure attained was 70 psig. The duration of the second transient was four days at 287 F and 40 psig to simulate a post-accident condition. Chemical spray was applied for 261 hours- during the second transient. See Appendix G for LOCA test data. 5.7.2 LOCA Test Results The -triax.. sheath on one . signal cable failed, and one detector exhibited a negative temperature coefficient of the keep-alive signal current. The mated connections of connectors for test articles 76603-01 and 76604-1/76605-01 suffered slight leakage. In addition, the behavior of the cable response to a rapid thermal transient is described. 5.7.2.1 Triax Sheath During the LOCA test the signal cable of test article 76602-01 exhibited a failure of the triax (outer) sheath to coax (inner) sheath insulation resistance. The failure was due to a defect in the triax outer sheath allowing moisture into the sheath-to-sheath dielectric area of the cable. The primary function of the cable is to transmit the ion chamber current to the ratemeter device. This function was not compromised, and the internal coaxial cable maintained insulation resistance within specification and the keep-alive signal was unaffected by the failure. A secondary function of the cable is to separate the chassis and signal grounds. The chassis ground potential is maintained on the triax sheath. Signal ground potential is maintained on the coax sheath. These two ground potentials are normally equal in a reactor installation, as the signal and chassis grounds are tied to a common point on the station ground grid. A minimum of one megohm resistance is normally present to keep circulating ground loop currents to a minimum. The reduction of the insulation resistance due to a triax sheath failure could reduce the capability of the radiation monitor channel to read low levels of radiation in the presence of ground potential differences between the mineral-insulated triax sheath defect and the common-point ground. A circulating current established by, this potential difference may offset the signal ground reference at the ratemeter input. The magnitude and sign of the error offset is entirely dependent on the station ground grid 18 i
f condition. As demonstrated by the LOCA Test, when no ground fault potential difference exists on the station grid, there will L '
-be no effect on the signal. The triaxial design of the system provides an immunity to a triax sheath failure.
To preclude the possibility of similar failure modes on production cables, an acceptance test on all cables has been - added to the cable specification- requirements, Specification No. [ 825284-001, Revs. C and D. The acceptance test assures that
-triax sheath defects, if they exist, are forced to fail prior to cable delivery by subjecting the cable to an autoclave pressure and temperature test.
5.7.2.2 Detector Temperature Coefficient Detector test article 14624 exhibited a negative temperature a coefficient of the keep-alive signal current at the high I ' temperatures attained during both the margin LOCA and the LOCA testing. Detector test article 22710 did not exhibit a similar l characteristic. Post-qualification test evaluations confirmed the N.T.C effect. Both ion chambers were subjected to a calibration source (per KNP 18-104) while exposed to temperatures from ambient to 385*F. The effect of N.T.C. is only apparent on test article 14624 for the keep-alive source-genera ted current. Currents generated in the ion chamber from exposure to the externally mounted gamma source did not exhibit this characteristic. Further investigation by disassembling the ion chamber and comparing it to several production articles determined that the N.T.C effect appears to be isolated to test article 14624 possibly due to a contaminated inner ceramic seal. See Appendix H for investigation findings. The manufacturing process has been - modified to include an N.T.C. screening test prior- to final detector assembly. 5.7.2.3 Connector Leakage The male stub, test article 76603-01, and the in-line mated connector pair, test articles 76604-01/76605-01 exhibited a !
' degraded insulation resistance and increased noise currents
.during or after LOCA conditions. Moisture contamination was determined to be the cause 'of the degraded performance in both Cases.
-5.7.2.3.1 Male Stub
' The male stub was plugged at the beginning of qualification testing to simulate an installed spare cable. The plug was similar to a female connector shell except that the male threads of the stainless steel plug did not have the copper plating typical of the female connectors. As a result, when the plug was torqued into the male stub 19 l _ __ _ __
connector, the stainless steel threads galled and did not allow adequate compression of the metal o-ring into its seat. The margin LOCA pressure was sufficient to allow a small amount of moisture to slowly leak into the connector and cause the I.R. degradation. The plug design has been modified for production to require copper-plated threads, which act as a lubricant to prevent galling. 5.7.2.3.2 In-Line. Connector Pair The in-line mated connector pair was initially torqued to 28 ft-lbs. Between the seismic and LOCA test the torque was checked at 28 ft-lb and then tightened to 30 ft-lb and subsequently to 35 ft-lb prior to LOCA. Jam-lock nuts were not installed. After the LOCA test the torque had relaxed to about 20 f t-lbs. The connector pair was not separated until post-test evaluations were begun at the factory. This connector pair exhibited degraded performance only at the completion of LOCA testing when the mated pair had returned to ambient conditions. After disassembly and drying with heat the I.R. of the connectors recovered. This effect is explained if an extremely small leak is assumed, say, between the o-ring and its seat. At LOCA pressure, a small amount of moisture could be introduced into the connector body which is at essentially atmospheric pressure. The LOCA temperature would cause any moisture in the body of the connector to be vaporized, which, in small enough quantity, would not absorb into the dielectric material to cause degradation. However, as the connector body cooled after the LOCA test, the entrained moisture would condense onto the dielectric surfaces and cause the degradation. Subsequent disassembly and drying would allow recovery of the performance, as indicated. The o-ring manufacturer suggested that the very slow leak may have been caused by a rough surface finish on the o-ring seat. Kaman manufacturing records show that a surface finish on the o-ring seat of the male connector had been specified but that a corresponding surface finish had not been specified on the o-ring seat of the female connector. Production connectors have been re-specified to have a high quality surface finish on the o-ring seats of both the male and female connectors in order to minimize chances of leakage. Post-test evaluations included additional torque studies and vibration testing followed by leak testing. See Appendix I for details. 20
5.7.2.4 Thermal Transient Behavior Chart records of the output current of test article 22710 and its associated cables during the first few minutes of the LOCA transient indicated a response to the rapid increase in temperature. The extrapolated value of the response is estimated to have been approximately 1.5E-10 amps with recovery to the
" keep-alive" specified maximum value (2.04E-11 amps) occurring 5.4 minutes into the LOCA event.
Post-test evaluations determined that this characteristic may be attributable to thermally-induced release of charges trapped in the conduction band of the dielectric materials due to impurities or defects. An algorithm to predict the magnitude of the transient has been empirically determined. The value is dependent on maximum temperature, temperature ramp rate and cable length. The effect of the transient is to add a false signal to the radiation signal. The experiment and methodology applied to determine the magnitude of the error current is provided in Appendix K. Additionally, the appendix describes the cause of the effect and a method to reduce the magnitude. 5.8 Detector Calibration (Post-Qual) The detectors were removed from the test platform at the conclusion of qualification testing, and in accordance with Appendix A, paragraph 3.1.19, subjected to a gamma calibration per procedure KNP 18-104. The nominal detector efficiency of test article 14624 was 0.95E-11 A/R/hr. The nominal detector efficiency of test article 22710 was 0.90E-11 A/R/hr. These values are within the tolerance specified for 9ese detectors. This post-test calibration data is presented in Appendix L. l l 21
~ ~6.0 EVALUATION AND FUNCTIONAL TEST RESULTS I
Evaluation and functional tests were performed in accordance with paragraph 3.3 of the Qualification Plan (Appendix A) at the following steps in the test sequence: o baseline per paragraph 3.1.3 o post mechanical aging per paragraph 3.1.5 o pre-irradiation test per paragraph 3.1.5 o pre-irradiation test per paragraph 3.1.7 o post-irradiation. test per paragraph 3.1.9 o pre-seismic test per paragraph 3.1.11 o post-seismic test per paragraph 3.1.13 o drop-ship at factory C05 #1 per DAFR-17 o drop-ship at factory C0S #2 per DAFR-17 o post-ship to LOCA facility per paragraph 3.1.15 o post-installation in autoclave (per Kaman test engineer discretion) o pre-margin LOCA test per paragraph 3.7.4.7.1 o margin LOCA test per paragraph 3.7.4.7.2 o pre-LOCA test per paragraph 3.7.4.7.3 o LOCA at 380*F per paragraph 3.7.4.7.4 o LOCA at 340 F per paragraph 3.7.4.7.6 o LOCA at 316 F per paragraph 3.7.4.7.7 o LOCA at 291 F paragraph 3.7.4.7.8 o post-LOCA test per paragraph 3.1.17 o post-ship to factory (per Kaman test engineer discretion) o disassembled (per Kaman test engineer discretion) The complete set of data from these tests is contained in Appendix J. Table III is a summary of this raw data. 22
TABLE III
SUMMARY
OF EVALUATI0ft AND FUtiCTIONAL TEST DATA Key to sussarized data tables Tableinds: Table Title Procedure reference 1 KEEP-ALIVEBEFORE para. 3.3.4 2 NOISE I BEFORE para. 3.3.3.3 3 CONTINUITY para. 3.3.3.1 4 I.R. C/S para. 3.3.3.2 5 !.R. C/S para. 3.3.3.2 6 1.R. S/S para. 3.3.3.2 7 !.R. S/S para. 3.3.3.2 8 VOLT N!THSTAND para. 3.3.3.4 ) 9 NOISE V AFTER para. 3.3.3.3 l 10 NOISE I AFTER para. 3.3.3.3 1
!! KEEP-ALIVE AFTER para. 3.3.4 l Test seguence Nase Procedurereference baseline para. 3.1.3 seth aging para. 3.1.5 pre-irrad para. 3.1.7 post irrad para. 3.1.9 pre-seissic para. 3.1.11 post-seisaic para. 3.1.13 drop-ship COSit DAFR-17 drop-ship COS42 DAFR-17 post-ship (All para. 3.1.15 post-install engr's discretion pre-eargin para. 3.7.4.7.1 sargin LOCA para. 3.7.4.7.2 pre-LOCA para. 3.7.4.7.3 LOCA I 380F para. 3.7.4.7.4 LOCA 4 340F para. 3.7.4.7.6 LOCA 4 316F para. 3.7.4.7.7 LOCA 4 291F para. 3.7.4.7.8 post-LOCA para. 3.1.17 post-ship (CO) engr's discretion disasseebled engr's discretion Abbreviation key 1/c lon chasber 1/cs ion chaaber signal electrode 1/ch ion chaeber high voltage electrode es sale stub (plugged) is fosale stub (capped) hv high voltage sg signal lp loep si sale inline (sated to fesale) fi fesale inline (sated to sale)
C/S conductor to (inner coas) shield S/S shield (outer trian) to shield (inner coarl F prefixes an out of tolerance reading 23
Table 1 ~ los chaeber keep-allye readings taken before the application of test voltages. Unite of sessure..... Asps KEEP-ALIVE MFONE 1/c 14624 1/c 22710 annuunun.nu.uu.a.unuun.- specnoeinal 1.52E-!! 1.02E-Il speceln 7.6M-12 5.lM-12 specea 3.04E-!! 2.04E-!! baseline N/A N/A sech aging .N/A N/A pre-irrad N/A N/A post-irrad N/A N/A pre-plosic N/A N/A post-seisaic N/A N/A drop-ship C0881 N/A N/A drop-ship COB 82 N/A N/A post-ship (AL) N/A N/A post-lestall N/A N/A pre-eargin N/A N/A eargio LOCA N/A N/A pre-LOCA N/A N/A LOCA 0 300F F-l.60E-!! 1.!M-!! LOCA 0 340F F-l.0M-Il 1.02E-!! LOCA 0 316F F0.35E-!! 1.40E-l! LOCA 0 291F F-5.0M-!! 1.02E-Il post-LOCA 1.4M-Il 1.0K-il post-ship (CO) 1.5X-11 1.03E-Il disassembled N/A N/A see notes 1,2 1 notes 1 The einismo and easieue tolerances for the keep-alive signal are specified to reflect the allosable systes accuracy. The f acter of two llelt is applied to the keep-alive reading obtained during the ion chaeber calibration. 2 lon chaeber exhibits a negative toeperature coefficient. This characteristic sas due to a contacinated inner cerasic seal in the ton chaeber. Future occurrence of this characteristic mill be olisinated in production detectors by a screening test before final assembly. 24 l
Table 2 Cable noise current taken before the application of test voltages. Unit of esasure.....picoasps NOISE I BEFORE es76403-01 is76606-01 hv76604-02 hv76603-02 e176604-01 fl76405-01 sg76602-02 sg76602-011p79103-01
.................s................................................................................................
specean abs 10.00 abs 10.00 N/A N/A abs 10.00 abs 10.00 abs 10.00 abs 10.00 N/A baseline N/A N/A N/A N/A N/A N/A N/A N/A N/A sech aging N/A N/A N/A N/A N/A N/A N/A N/A N/A pre-irrad N/A N/A N/A N/A N/A N/A N/A N/A N/A post-trrad N/A N/A N/A N/A N/A N/A N/A N/A N/A pre-selseic N/A N/A N/A N/A N/A N/A N/A N/A N/A post-seiselt N/A N/A N/A N/A N/A N/A N/A N/A N/A drop-ship Col 01 N/A N/A N/A N/A N/A N/A N/A N/A N/A drop-ship COST 2 N/A N/A N/A N/A N/A N/A N/A N/A N/A post-ship (All N/A N/A N/A N/A N/A N/A N/A N/A N/A post-install N/A N/A N/A N/A N/A N/A N/A N/A N/A pre-eargin N/A N/A N/A N/A N/A N/A N/A N/A N/A nargin LOCA N/A N/A N/A N/A N/A N/A N/A N/A N/A pre-LOCA N/A N/A N/A N/A N/A N/A N/A N/A N/A LOCA I 380F 4.00 0.70 200.00 DAFR-18 0.60 e F -230.00 DAFR-18 250.00 LOCA 6 340F B.70 0.30 200.00 130.00 1.20 e F -28.00 8.50 -9.00 LOCA 4 316F F 25.50 0.50 160.00 89.00 0.50 * -3,00 9.00 269.00 LOCA 0 291F F 103.00 0.30 150.00 75.00 0.40
- F -40.00 0.60 55.00 post-LOCA F 66.00 0.10 23.00 24.00 F 25.00 e 3.50 0.40 5.00 post-ship (CD) F24000.00 0.10 8.30 9.10 F 82.00 e 1.50 0. 80 1.00 disasseebled N/A N/A N/A N/A N/A N/A N/A N/A N/A see notes 3 4 6 5 notes 3 Galled threads prevented proper torque application to plug, allowing leakage.
4 Suspected solsture condensation ento cerasic surfaces at louer toeperatures. This solsture is believed to have been trapped during the sating operation, or due to lack of sufficient surface finish on o-ring seating surfaces. Production procedures have been revised to include proper surface finish. 5 Due to the NTC of the ion chaeber attached to this cable it is suspected that the pre-aep placed a bias voltage on the ion chamber signal electrode circuit, which induced a charge retention in the dielectric natorial of the ion chaeber. 6 Cables 76604-01 and 76605-01 were connected together during the test and separate readings mere unobtainable. l l i l 25 l l _ _ _ _ _ - _ _ _ _ _ _ _ _ _ _ _
TaDie 3 Condt.ctor Continuity Unit of seasure.....ohes CON 71NUITY es76603-01 is76606-01 hv76604-02 hv76603-02 si76604-01 fi76605-01 sg76602-02 sg76602-01 1p79903-01 588338385833338388333388E833338888333333333338883333333333383333333883333333338388803533333333$8833583333858380888 specea 227.40 227.40 203.60 235.40 240.60 240.60 213.60 245.40 321.60 baseline N/A 0.4 0.44 1.79 0.68 0.21 0.81 0.70 OPEN each aging N/A N/A N/A N/A 1.17 e N/A N/A OPEN pre-irrad 0.3 N/A N/A N/A 0.9B
- N/A N/A OPEN post-irrad N/A N/A N/A N/A 0.9 s N/A N/A OPEN pre-seisaic N/A N/A N/A N/A 0.96
- N/A N/A OPEN post-selseic N/A N/A N/A N/A 0.95 t N/A N/A OPEN drop-ship COS41 N/A N/A N/A N/A 0.96 e N/A N/A OPEN drop-ship C0042 N/A N/A N/A N/A 0.07 e N/A N/A IFEN post-ship (All N/A N/A N/A N/A 0.00 e N/A N/A OPEN post-install N/A N/A N/A N/A 0.96
- N/A N/A OPEN pre-eargin N/A N/A N/A N/A 1.03
- N/A N/A OPEN sarginLOCA N/A N/A N/A N/A 1.38
- N/A N/A OPEN pre-LOCA N/A N/A N/A N/A t.02 e N/A N/A OPEN LOCA I 300F N/A N/A N/A N/A 1.4 i N/A N/A OPEN LOCA I 340F N/A N/A N/A N/A 1.29 e N/A N/A OPEN LOCA I 316F N/A N/A N/A N/A 1.31
- N/A N/A OPEN LOCA 4 291F N/A N/A N/A N/A 1.25 i N/A N/A OPEN post-LOCA N/A N/A N/A N/A 0.91
- N/A N/A OPEN post-ship (CO) N/A N/A N/A N/A 0.89 e N/A N/A OPEN disassembled 0.35 0.42 0.45 1.27 0.54 0.36 0.85 0.80 OPEN see notes 6 7 notes 7 Prior to the start of qual testing this cable nas determined to have a pin-to-sleeve open rircuit due to handling daeage of the vulnerable, esposed seals.
26
TCle4 Insulation resistance, conductor to shield. Linit of esature.....ohes 1.R.CIS
.n==.m....es7M03-01 fs7806-01 hv7M04-02 hv76603-02 si76604-01 (17h05-01 s
.==.uunn.un .n...=un..uun....u.nu..a..u====g7M02-02 og7M02-01 1 p79903-01
== uune.n=== u.a .
i specoln ! baseline 6.00E+09 N/A 6.00E+09 6.00E+09 6.00E+09 6.0M+09 6.00E+09 6.00D09 6.00D09 1.30D11 1.00E+13 )5.00D 12 5.00D12 5.00E+12 1.00D13 >2.5M+12 1.00E+12 N/A sech aging II/A )l.00E+13 >5.0 K +12 1.00E+13 2.50D12 e 1.00D13 IIIA 2.50012 pre-frred 3.70D10 1.00013 1.0M+13 6.00Dit 2.00E+12 e 1.0M+13 1.ME+13 1.MD13 postirrad Fl.30 D09 F4.00E+09 )3.000 09 2.00D09 F)2.5E+09 + F2.0M+09 1.50010 Ft.HDtl pre-seissic 1.HDll F3.50D09 4.00D09 4.00008 5.00E+09 e 1.00E+10 1.0 M+11 F6.5M +07 post-selseic 8.00E+09 F3.50D09 4.00E+10 1.00D10 3.50D09 + 4.00011 8.00D10 F4.5M+08 drop-ship C0001 7.50D11 4.00E+11 1.50E+12 2.50D12 1.2M+11 * >t.00D13 1.50D12 5.00D12 drop-ship C0802 2.50E+12 1.0M+13 1.00D13 5.00D12 6.00011 e 1.00D13 1.0M+13 5.00E+11 ) l post-ship (AL) 2.5K+12 5.00D12 2.50D12 5.00D12 2.20E+11 post-install e 1.00D13 1.00D13 9.00E+11 5.00D12 1.00D13 1.00013 2.50D12 4.00D11 e 1.00D13 1.00D13 6.0M+11 pre-eargin 2.30D10 1.00D13 1.00D13 1.NE+13 1.02E+12
- t.00D13 5.0M412 2.5M+11 eargin LOCA pre-LOCA 1.00Dt! 3.50Dl! 8.00E+10 1.00Dl! 5.00E+10 e 7.00E+10 1.60D10 1.40E+11 F7.00E+07 2.50D12 2.5M+12 2.50D12 2.40D10
- 2.5M+12 2.5M+12 2.5M+12 LOCA 8 300F 3.00E+10 3.00D11 9.00D10 DAFR-18 L.00010 e 8.00E+10 84FR-18 1.50E+11 LOCA 4 340F t.10D10 5.00E+11 4.00D11 1.50D12 1.00E+11 e 4.0M+11 2.50E+12 1.30E+11 LOCA 4 316F F3.5M+09 1.00D12 4.00D11 6.00E+11 1.10E+11
- 4.0M+11 1.50D12 1.30E+11 LOCA post-LOCA 8 291F F6.00E+08 2.50012 8.00D11 1.0M+12 1.5M+11 e 1.0M+12 1.0M+13 2.00Dl!
F2.50008 )l.00E+13 1.00D13 1.00D 13 F4.00D 08 e 5.00D12 )l.00D13 1.00Dt3 post ship (COI F4.00D07 1.00E*!3 1.00D13 1.00E*13 F7.00D 00 e 1.0M+13 1.NE+13 5.HD12 disasseebled F2.00E+09 1.00D13 )l.00D13 5.00D12 1.50012 6.00011 1.00D13 1.00D13 5.0M+1 seenotes 3,8 8 9 9 0,4 6 8,9 9 8 notes 8 Out of tolerance readings at post-irradiation, pre- and post-seisaic are attributable to the test lab location environment (l.a. high hueidity and high air particulates) contasinatingthetestinterfaceconnector. 9 ! Specoln is given for Individual cables. Cables 76604-02and76603-02 were connected to the high voltage connector of an ton chaeber in all but the first and last test and the parallel combination of specein for the cable and the ion chaeber should be applied to the other readings (i.e.1.0M+07). This condition also applies to the signal cables 7802-02 and 76602-01 (2.7D09). Litemise, cables 7804-01 and 76605-01 were connected to each other in all but the first and last tests and the parallel coebination of these (i.e. 3.00D091 should apply. l 27 l t _ - - -
Table 5 Insulation reelstance, conductor to shield, ilnit of asesure.....ohes
!.N. C/8 1/cel4624 1/cs22710 1/chl4424 1/ch22710 specals 5.00E+09 5.00E+09 1.00E+07 1.00E+07 baseline N/A N/A N/A N/A sech aging N/A N/A N/A N/A pre-frred N/A N/A N/A N/A post-irrad N/A N/A N/A N/A pre-selsele N/A N/A N/A N/A post-selsele N/A N/A N/A N/A drop-ship C0001 N/A N/A N/A N/A drop-shipC0802 N/A g N/A N/A N/A post-ship (AL) II/A N/A N/A N/A post-install N/A N/A N/A N/A pre-eargin N/A N/A N/A N/A sarginLOCA N/A N/A N/A N/A pre-LOCA N/A N/A N/A N/A LOCA 4 300F N/A N/A N/A N/A LOCA 4 340F N/A N/A N/A N/A LOCA I 316F N/A N/A N/A N/A LOCA 4 291F N/A N/A N/A N/A post-LOCA N/A N/A N/A N/A post-ship (CO) N/A N/A N/A N/A disassembled 1.00E+13 1.00E+13 1.00E+13 1.00E+13 see notes 9 9 9 9 28
TCle6 l Insulation resistance, shield to shield. Unit of esasure.....ohes 1 i I.R. S/8 es7 M03-01 is766H -01 hv7M04-02 hv7 M03-02 e17 M 04-01 f17 M 05-01 sg7 M 02-02 sg76602-01 1p79903-01 l m.==.m.mu.-===..u=====..===.m=======..=.---.=======..===.. specain 1.00E+M 1.00E+M !.00E+M !.00E+06 1.0M+06 1.00E+M !.0M+M 1.00E+M 1.00006 basellne N/A 1.50E+12 N/A 1.50D 12 )l.00D 13 1.50E+12 2.5M+12 2.50012 N/A sech aging N/A 1.00D13 4.00E+11 2.00D12 2.00E+12 e 1.50E+10 2.50E+12 )l.00D12 pre-irred 2.00E+10 1.60E+11 1.40E+10 1.50D11 1.60Dl! # 1.00E+10 1.7M+11 7.5M+10 post-trred 2.50D00 2.00E+09 1.20E+00 1.20E+00 1.50D09 e 1.00D00 4.00E+10 2.50Dl! pre-selseic 1.30E+10 4.0M+07 2.00D07 6.00DM 2.0M+00 e 2.00D08 1.00E+10 6.00E+M post-seismic 2.00E+09 1.00D08 2.00E+07 5.00E+M 2.00D08 e 2.00E+08 1.60E+10 1.00E+10 drop-ship COO 41 4.50Dl! 9.00E+08 1.90D07 4.00E+08 3.50E+09 e 1.2M+09 3.00010 1.00D09 drop-ship C0002 1.000 12 6.00Dl! 1.50E+12 1.00Dl3 1.70D10 e 1.50D12 1.00D13 1.50E+12 post-ship (AL) 2.70D11 1.80D11 1.50012 1.50D12 1.50E+10 e 1.90E+10 2.50D12 7.00E+10 post-instal! 1.60E+11 1.00Dil 2.5M+12 2.50E+12 0.00E+09 e 1.00D10 2.50D12 2.5K+12 pre-eargia 3.00E+00 1.30Dil 1.00D12 7.0K+11 3.30E+10 e 4.00E*10 7.00D11 4.00E+11
- earginLOCA 3.50E+09 2.30E+10 1.20D10 B.00D09 1.20E+10 e 2.5M+10 1.00E+10 6.0M+10 pre-LOCA F3.70D02 5.50D10 9.00D11 7.00E+11 1.0M+09 e 2.50E+08 4.0M+10 1.00D12 a
LOCA 4 380F 6.00E+00 3.00D10 1.00E+10 DAFR-18 1.30E+10 e 3.00D10 DAFR-18 2.50D10 LOCA 4 340F 2.00000 5.00D10 4.00D10 6.00DM 2.00E*10 e 4.00D 10 F3.50E+02 4.00D11 LOCA 4 316F 1.10E+00 1.00E+11 5.00010 1.10D00 5.00E+10 e 6.00D 10 F7.76E+03 1.50D11 LOCA 0 291F 4.00E+07 1.30bil 1.0M+11 1.6M+10 1.00E+11 e 1.50D 11 Fl.10E+44 1.2M+11 post-LOCA 1.40E+07 2.30D11 )l.00D13 5.00D11 4.50D08 e 1.50D00 Fl.00D03 1.50E+12 post-ship (Col Fl.00E+03 1.HDH 5.00D00 4.50D10 1.IOD07
- 1.0h+07 .1.70 0 % l.0M+12 disassembled 1.40E+07 7.00E+M 2.00E+09 5.00D09 2.00E+49 1.60E+08 6.00D07 1.20D07 1.00E+13 see notes 3 6 10 notes 10 The trias sheath ruptured, allowing solsture to be absorbed in the outer dislectric.
i l 29
._._r.._ __
m - _ _ - . _ . . _ _ . . . _ , . . . - - . - _ _ . _ _ _ . - . - _ _ . - _-
1 1 Table 7 1 Insulation resistance, shield to shield, f
- Unit of seasure.....shes 1
!.R.S/S 1/cel4624 t/cs22710 t/chl4624 1/ch22710 specain 1.00E+06 1.00E+06 1.00E+06 1.00E+06
, baseline N/A N/A N/A N/A aech aging N/A N/A N/A N/A pre-irrad N/A N/A N/A N/A post-irrad N/A N/A N/A- N/A { pre-seisaic N/A N/A N/A N/A post-seismic N/A N/A N/A N/A drop-ship C0641 N/A N/A N/A N/A j drop-ship COS42 N/A N/A N/A N/A i post-shiptAL) N/A N/A N/A N/A post-install N/A N/A N/A N/A pre-eargin N/A N/A N/A N/A earginLOCA N/A N/A N/A N/A pre-LOCA N/A N/A N/A N/A LOCA I 300F N/A N/A N/A N/A LOCA I 340F N/A N/A N/A N/A LOCA I 316F N/A N/A N/A N/A LOCA I 29tF N/A N/A N/A N/A post-LOCA N/A N/A N/A N/A post-ship (CO) N/A N/A N/A N/A disassembled 1.00E+13 1.00E+13 1.00E+13 1.00E+13 l l l l 30
Table B Voltage withstand test ( Unit of seasure.....sitroasps l , VOLT WITHSTANO es76603-01 is76606-01 hv76604-02 hv76603-02 ei76604-01 (176605-01 sg7660242 sg76402-01 Ip79903-01 n o.n u n.n u a u..u n n u..u u n .u n u u u u u.u u u...u...u u u n.n u a..uan.. .u.u u...... specess 1000.00 1000.00 1000.00 1000.00 1000.00 1000.00 1000.00 1000.00 1000.00 l baseline N/A 0.00 0.00 0.00 0.00 0.00 0.00 0.00 N/A t eachaging N/A 0.03 0.00 0.00 0.00 a 0.00 0.00 0.00 pre-trrad 0.06 0.00 0.00 0.00 0.00 e 0.00 0.00 0.00 post-irrad -0.68 -0.33 -0.00 -0.50 -0.60 e 4 .90 0.03 -9.00 i pre-seissic -0.07 -0.65 -0.00 -0.04 -0.40 e BAFR-14 DAFR-14 -8.20 post-seiselt -0.09 -0.36 -0.04 -0.03 -0.46 e -0.01 4.03 -3.48 drop-ship C0001 -0.02 -0.!! 0.00 0.00 -0.02
- 0.00 -0.02 -0.01 drop-ship C0802 0.00 4 .04 0.00 0.00 0.00
- 0.00 0.00 -0.01 post-ship (All 0.00 -0.05 0.C0 0.00 -0.01
- 0.00 0.00 -0.01 post-install -0.02 -0.01 -0.01 0.00 0.00 * -0.01 0.00 0.00 pre-eargin -0.07 -0.01 0.00 0.00 0.01 e 0.00 0.00 -0.04 marginLOCA -0.02 -0.45 -0.03 -0.03 -0.04 e -0.02 -0.09 -0.07 pre-LOCA -38.00 0.00 0.00 0.00 -0.07 e 0.00 0.00 0.00 LOCA 4 300F -0.05 -0.00 -0.03 DAFR-IB -0.04 e -0.03 DAFR-lO -0.08 LOCA 4 340F -0.11 -0.04 -0.01 -0.01 4.02 a 0.00 0.20 -0.03 LOCA 0 316F -0.32 -0.05 4.02 0.00 -0.01 8 0.00 5.00 -0.02 LOCA 4 291F -2.53 -0.24 0.00 0.00 -0.02 8 0.00 1.30 -0.01 post-LOCA -5.00 0.00 0.00 0.00 -0.75 e 0.00 0.70 0.00 post-ship (Col -47.00 0.00 0.00 0.00 -2.30 a 0.00 0.00 0.00 disasseabled -0.01 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 see notes 6 1
l 31 i I
l 7able 9 Cable noise voltage after application of test voltages. Linit of esasure.....elllivelts 1 N0!IE Y AFTER es7M03-01 fe7M06-01 hv7M04-02 hv7M03-02 al7M64-01 fl7M05-01 ag7M02-02 og7M02-011p79903-01 spaceau 30.00 30.00 N/A N/A 30.00 30.00 58.00 50.00 N/A baseline N/A 0.02 0.03 0.04 0.04 0.01 0.M 0.05 N/A sech aging N/A 0.00 0.00 0.00 0.00 e 0.00 0.00 0.00 pre-trred -0.20 -0. M -0.10 -0.09 -0.47 e -0.09 -0.!! -0.07 post-trred 1.26 -0.64 -0.96 -7.74 0.20 e -4.90 -1.43 -0.90 pre-selselc -0.20 -0.86 -0.31 -I.90 -0.35 e -0.24 -2.31 -0.97 post-selselt 4.12 0.47 N/A N/A 0.34 e -0.14 -0.33 -0.16 drop-shipC0001 -0.12 -0. N -0.89 -0.76 -0.16 * -0.15 -4.65 -0.81 drop-ship C0002 0.36 0.20 0.65 0.67 0.60 e 0.40 0.24 5.90
)
post-shiptALI 0.21 0.19 0.48 0.60 0.17 e 0.M 0.12 4.00 post-install 0.63 0.M 0.53 0.47 0.47
- 0.07 0.10 4.61
- pre-eargin 0.05 0.33 0.77 0.17 0.70
- 0.24 0.63 10.50 earginLOCA 0.07 0.52 0.02 1.00 0.31 e 2.50 10.20 15.00 pre-LOCA -23.31 0.25 0.50 0.00 0.20
- 0.45 0.60 0.70 LOCA I 300F 0.07 0.40 1.90 DAFR-lO 0.60 e 3.00 DAFR-II 40.00 LOCA 4 340F 0.30 0.65 2.00 1.60 0.63 e 1.40 2.10 21.80 LOCA4316F 0.44 0.M 2.00 2.50 0.76 e 0.62 15.00 13.00 LOCA I 291F 1.50 0.85 2.40 2.00 0.78 e 2.90 I.50 6.50 post-LOCA -13.00 0.30 0.70 0.75 0.50
- 0.40 0.40 0.30 post-ship (Col F 19.4 0.35 0.41 0.62 3.30 a 0.25 0.30 0.27 disasseebted -0.10 0.04 0.00 0.00 0.C4 -0.03 0.06 0.02 N/A see notes 3 6 .
l i 1 32
( TCle10 Cable noise current taken after the application of test voltages. linit of seasure....piteasps i N0!It I WTER as7H03-01 is7H06-01 hv76604-02 hv7H03-02 ei76604-01 (176605-01 sg76602-02 sg76602-011p79903-01 u n nen.n u n n u n usu.u..n u u n..u.au un..u u n n .u.n u ...u......u ..u u . . u ...n specess abs 10.00 abs 10.00 N/A N/A abs 10.00 abs 10.00 abs 10.00 abs 10.00 N/A baseline N/A 0.50 0.60 3.10 0.40 0.10 0.20 4.30 N/A sech aging N/A 0.50 0.40 1.30 0.30 a 1.30 1.00 N/A pre-irred -I.00 0.20 1.00 0.70 0.30 e -1.30 -1.60 -0.30 post-irrad F 232.00 F -30.10 -57.00 -752.00 F 92.00 e F -475.00 F -69.00 -30.00 l pre-selsele -0.50 F -13.50 N/A N/A -1.00 4 0.50 -6.00 1.20 post-selseic 5.60 F 5.00 N/A N/A F 38.00 e -2.30 F -13.50 2.30 drop-ship C0001 0.70 2.10 24.10 24.50 3.70 e 7.10 F 375.0'r 178.00 drop-ship C0002 2.50 1.60 6.60 4.00 5.00 e 3.50 0.30 16.00 post-ship (ALI 2.30 1.20 1.20 0.60 2.40 e 5.60 1.99 119.00 post-install 6.70 0.00 6.90 7.70 3.50 e 3.10 0.00 90.00 pre-eargin 1.70 2.20 10.00 10.00 5.70 e 5.00 6.50 220.00 eargin LOCA 1.50 7.20 38.70 39.00 5.60 e F -140.00 F 300.00 600.00 pre-LOCA F ??.?? 1.90 10.00 10.00 8.50 e 10.00 10.00 7.00 LOCA I 300F 5.50 8.20 65.00 DMR-1B 7.00 e F -34.00 DWR-lO 250.00 LOCA 4 340F F 15.00 7.00 57.00 44.00 8.50 e F 40.00 F 150.00 590.00 LOCA4316F F 15.00 7.60 75.00 40.00 7.00 e F 41.00 F 470.00 590.00 LOCA 4 291F F 150.00 7.20 50.00 50.00 9.30 e -2.00 F 400.00 230.00 post-LOCA F-2500.00 1.50 20.00 8.00 F -40.00 e 6.00 2.50 2.00 post-ship (CO) F50000.00 1.50 13.00 4.50 F 360.00 e 2.00 3.50 2.00 disassembled 0.10 0.50 0.50 0.30 0.90 0.40 0.50 1.00 0.30 see notes 3,8 0 4,8 6 8,11 I,Il notes 11 The application of high voltages to test the insulation resistance and voltage withstand capability of the systes while at high toeperature induces a charge in the dielectric setorial of the ion chaeber which slouly bloods off through the high insulation resistance. The data presented in Table 2 is sore representative of an appropriate test eethod. l l 33
Tdle !! l I lon chaeber keep-allye reedlege taken after the application of test voltages. Unit of esseurs.....Aspe i KEEP-ALIVE AFTER 1/c 14624 t/c 22710 specneelnal 1.5 1 -11 1.03-11 specoln 7.60E-12 5.lM-12 1 specess 3.0M-11 2.04E-Il i baseline N/A N/A sech aging 1.51E-!! 1.lM-!! pre-trred 1.5M-Il 1.06E-!! post-trred F9.75E-10F!.60E-10 pre-seleelt 1.4M-l! 9.05E-12 post-selselc 1.29E-l! 1.01E-l! drop-shipCale! N/A N/A drop-shipCOB02 1.54E-!! 1.lN-!! post-ship (All 1.5M-!! 1.02EIl post-install 1.55E-11 1.00E-il pre-eargin 1.5M-!! 1.30E-Il eergin LOCA F-l.30E-10F1.40E-10 preLOCA 1.5M-il 1.12E-Il LOCA 4 300F F-1.60E-il 1.lM-!! 1 LOCA I 34# N/A N/A LOCAI31W N/A N/A LOCA 0 291F I.00E-12F!.3M-10 post-LOCA 1.55E !! 1.!N-il post ship (C8) 1.6tt-il 1.lM-Il diessesebled 1.5M-!! l.0M-l! see notes 1,8,11 1,1,11 i I l 34 i
i L l i t i APPENDICES TO QUALIFICATION REPORT [ FOR
'1 1
MODEL KDI-1000 HIGH RANGE CONTAINMENT AREA RADIATION DETECTOR
- AND j MINERAL-INSULATED CABLE SYSTEM
^
460036-002 Rev. A j i ! KAMAN INSTRUMENTATION P.O. BOX 7463 COLORADO SPRINGS, COLORADO 80933 I i 1 .i ( !:i k i I s 4 4
'l LIST OF APPENDICES APPENDIX A - 460036-001 REV. A, QUALIFICATION OF MODEL KDI-1000 HIGH RANGE AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM i APPENDIX B - DEVIATIONS, AN0MALIES AND FAILURE REPORTS l
APPENDIX C - DETECTOR CALIBRATICN (KNP AND DATA SHEETS) APPENDIX D - MECHANICAL AGING DATA SHEETS APPENDIX E - IRRADIATION TEST DATA APPENDIX F - SEISMIC TEST DATA APPENDIX G - LOCA TEST DATA APPENDIX H - DETECTOR N.T.C. INVESTIGATION l APPENDIX I - TORQUE MAINTENANCE INVESTIGATIONS l APPENDIX J - EVALUATION AND FUNCTIONAL TEST DATA RECORDS APPENDIX K - THERMAL-TRANSIENT INVESTIGATIONS These appendices to the Qualification Report for Model KDI-1000 High Range Containment Area Radiation Detector and Mineral-Insulated Cable system 460036-002 present detailed test results and other activities performed during 1 the qualification program. The appendices are provided to support the in-depth , review of the qualification activities and the conclusions of the main body of the report. s i d r
{ [ F L
~ APPENDIX A l
460036-001 Rev. A, Qualification j i of Model KDI-1000 High Range l L Containment Area Detector > and Mineral-Insulated Cable System j 1 I i i f i f l i i l ! I l l I l. 460036-002 Appendix A I l - i
s APPLICATION REVISIONS N E X T AS$'Y USE D ON REV DESCRIPTION D A T,E APPROVE D A Original Issue Eco 29535~ WM TM - s r L ( {
)
{ l MATERIAL ** **" ff) ** Kaman Instrumentation Carpara6on
\
py 7,4 cotoRaco :,.> RINGS. COLORADO FINISH '""Td/pd f/nh QUALIFICATI0fl 0F ft00EL KDI-1000 ll!Gli RAflCE oc/g f.g C0flTAINftENT AREA RADIATIO'l DETECTOR Afl0 ft!!1ERAL-IflSULATED CABLE SYSTEM UNLESS O THE RWagg SPECIF 8ED OtMENSIONS PRODf f pe[ AREININCHES. PROJ
.f CODE #DE NT NO. SIZE DWG. NO. M t V.
* "^~**'
,.3 , APPMovr D 7TO28 A * = -oo' ^
.x x x
- 1.010 CONTR ACT NO. SCALE SPEC SHf ONoLES = to*30' OF gJd)
FC Mi-ENG10 6
QUALIFICATION
)
0F ' MODEL KDI-1000 HIGH RANGE CONTAINMENT AREA RADIATION DETECTOR AND MINERAL-INSULATED CABLE SYSTEM 460036-001 Rev A KAMAN INSTRUMENTATION P.O. 80X 7463 COLORADO SPRINGS, COLORADO 80933 s
~ CERTIFICATE OF QUALIFICATION s ' for - Model KDI-1000 High Rar:ge ' Containment Area Radiation Detector and Mineral-Insulated Cable System L t I L I hereby certify that the Kaman Model KDI-1000 High Range Containment Area ( Radiation Detector and Mineral-Insulated Cable System, as represented by Kaman t Specification 460036-001, was tested and is qualified for the service intended. Date Milt Gigax, Quality Assurance Manager Kaman Instrumentation Corp. Date Harvey D. Bos, Professional Engineer i i
)
i I _ . _ . _ . . . . _ _ _ _ _ _ _ _ _ _ _ _ _ _ . - _ _ _ . - - ~ _ _ _ _ . - - _ . . _ _ _ _ _ . _ _ _
f TA8LE OF CONTENTS h Page SPECIFICATION COVER SHEET AND REVISION RECORD . . . . . . . . . . . . . . . 2 CERTIFICATE OF QUALIFICATION . . . . . . . . . . . . . . . . . . . . . . . 3 TA3LE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 LIST OF FIGURES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 4 J 1.0 QUALIFICATION RESULTS. . . . . . . . . . . . . . . . . . . . . . . . . 6 1.1 S umma ry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 s 1.2 General Notes and Deviations . . . . . . . . . . . . . . . . . . . . . 6 1.3 Detailed Results . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 J 2.0 QUALIFICATION PLAN . . . . . . . . . . . . . . . . . . . . . . . . . . 9 1 2.1 Introduction . . . . . . . . . . . . . . . . . . . . . . 2.2 System Description . . . . . . . . . . . . . . . . . . .
. . . . . . 9 J
..... 9 2.3 Qualification Test Objectives. . . . . . . . . . . . . . . . . . . . . 10 .
2.4 Reference Document List. . . . . . . . . . . . . . . . . . . 2.5 Test Articles Description. . . . . . . . . . . . . . . . . . . . . . 10 11
)
2.6 Qualification Requirements Ana. lysis. . . . . . . . . . . . . . . . . 14 2.7 Environmental Conditions . . . . . . . . . . . . . . . . . . . . . 19 2.8 Acceptance Cri teri a. . . . . . . . . . . . . . . . ......... 24 3.0 SUPPORTING DOCUMENTS . . . . . . . . . . . . . . . . . . . . . . . . .. 3.1 Generalized Preparation and Handling Guide . . . . . . . . . . . . . 26 3.2 Calibration Procedure and Data Record. . . . . . . . . . . . . . . . 26 31 3.3 Evaluation and Functional Test Procedure . . . . . . . . . . . . . . 32
- 3.4 Mechanical Aging Procedure and Data Record . . . . . . . . . . . . . 40 i 3.5 j
Irradiation Test Procedure and Data Record / Certification . . . . . . . 42 3.6 Seismic Test Procedure and Data Record / Certification . . . . . . . . 44 3.7 LOCA Test Procedure and Data Record / Certification. . . . . . . . . . 46 l l i i l l L . _ _ _ _ _ __ _-
t 7 % 5 LIST OF FIGURES I i Reference Fig. 1 - Deviations, Anomalies, and failure Report . . . . . . 1.2.2 f Fig. 2 - RRS for Vibration Aging . . . . . . . . . . . . . . . 2.6.1.5.2 L Fig. 3 - RRS for OBE Seismic Test. . . . . . . . . . . . . . . 2.6.1.5.3 Fig.-4 - RRS for SSE Seismic Test. . . . . . . . . . . . . . . 2.6.1.5.3 Fig. 5 - LOCA Test Profile . . . . . . . . . . . . . . . . . . 2.6.1.6 f Fig. 6 - Test Platform . . . . . . . . . . . . . . . . . . . . 3.1.1 L Fig. 7 - Qualification Data Record Sheet . . . . . . . . . . . 3.1.2 Fig. 8 - IR Measurement Connections. . . . . . . . . . . . . . 3.3.3.2.4 p Fig. 9 - Voltage Withstand Test Connections. . . . . . . . . . 3.3.3.4.3 ( Fig. 10 - Functional Test Connections . . . . . . . . . . . . . 3.3.4.3 e l l l 1 b i i 0
, , . + , . - - - , - , - . , ,.--,..e- ~ . - . - - - - - - - - - ~ , - - - - - - - , - - ---.n. , , - .~. , , , - - - , - , - , - , . . . , --- . . . - ~ . . . , , - . - - - . . , ~ - ,
4
]
1.0 QUALIFICATION RESULTS 1.1 Summary (This section and subsequent sections marked "later" are to be ) completed at the -conclusion of activities described in PARTS 2 & 3) qualification testing and evaluation . 1.2 General Notes and Deviations )s 1.2.1 Purpose s This document describes in detail the Qualification Plan, Procedures, and Results of the Qualification of the Kaman Model KDI-1000 High Range Containment Area Radiation Detector and 1 Mineral-Insulated Cable System. This document is intended to J chronicle the Qualification activities from the initial planning stages (Part 2) through implementation (Part 3) to reporting of results (Part 1), and presents in a single document the complete Qualification Statement for the System. ) Certain sections or parts of this document are initially left incomplete by necessity, and the document is intended to be revised as procedures are completed and results are available.
; 1.2.2 Deviations Deviations from the general plan and detailed procedures are allowed after full evaluation and approval by the Kaman Qualifications Engineer. Each deviation is noted on a Deviation, Anomolies, and i Failures Report. (See figure 1).
(later) 1.3 Detailed Results 1.3.1 Generalized Preparation and Handling (later) l 1.3.2 Calibration (later) l l 1.3.3 Aging Test (later) 1.3.4 Irradiation Test l (later) 1.3.5 Seismic Test (later) J
L .. FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT (- Sequence No.,_ for program 460036-001 [ check one: [ Request for deviation from approved plan or procedure Description of anomalous condition or occurrence Report of failure ( _ List the document or specification reference paragraph and requirement l Describe the Deviation, Anomaly, or Failure Name Date Recommended Disposition Name Date Approved Disposition Approved Date QA Date Qualification Engineer
1 J 1.3.6 LOCA and Post Accident Test - J (later) n J h
]
s 1 l 1 I
' W - --
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2.0 QUALIFICATION PLAN s 2.1 Introduction This part describes the system requirements, components, and objectives of the qualification program, the test sequence and parameters, and the evaluation criteria for the KDI-1000 High Range Containment Area Radiation Detector and Mineral-Insulated Cable System. u
2.2 System Description
2.2.1 Purpose The High Range Containment Area Radiation Monitoring System is - required by USNRC Regulatory Guide 1.97 to monitor the area radiation inside the containment building of a nuclear power reactor throughout the events of a design basis accident. The system is designed to meet the sensitivity, range, and accuracy requirements of the Regulatory Guide over the full range of environmental condition expected for a Loss of Coolant Accident for both BWR and PWR installations. 2.2.2 System Components A complete High Range Containment Area Radiation Monitoring System consists of the detector and mounting assembly, in-containment mineral insulated cable assemblies for signal and high-voltage transmission, containment penetration feed-throughs, ex-containment triaxial cable assemblies, and electronics for high voltage supply and dose rate detennination (current measurement). This test is intended to qualify the in-containment portions of the system. 2.2.3 In-Containment Sub-System Components A typical In-Containment Subsystem consists of a detector, its mounting bracket, and two cable assemblies. 2.2.3.1 Detector The system detector is a Kaman P/N 824636-003 fon chamber approximately 8 in, long and 3 in. diameter. The outermost cylindrical housing is made of stainless steel and provides an hermetic seal for the high voltage and signal anodes insulated with-in. Two female triax bulkhead connectors are provided to connect the HV and signal ports to cables for operation. There are no organic materials in the detector. 2.2.3.2 Mounting Bracket Two styles of mounting brackets are available. A captive mount Kaman P/N 952701-003 or an insulated mount Kaman P/N 450593-001 secure the detector in an assembly suitable for affixing to a flat, preferably vertical, surface. There are no organic materials in the mounting brackets.
10 2.2.3.3 Cables Two identical cables are required for each detector to supply high voltage and to transmit the low-level signal current. The cables are of metal sheathed (stainless steel) mineral-insulated semi-rigid triax construction with hermetically ] designed triax connectors on each end. The cable assemblies are Kaman P/N 852568 (male-male), P/N 852569 (male-female), or P/N 852570 (female-female). There are no organic materials in the cable assemblies. 2.3 Qualification Test Objectives The High Range Containment Area Radiation measurement is classified by Regulatory Guide 1.97 as a type E variable requiring a Category I system. As such, this system is nuclear safety-related and requires full environmental and seismic qualification per Regulatory Guides 1.89 and 1.100. Qualification testing and analysis of this system is achieved by following the procedures and guidance of IEEE STD 323-1974 and IEEE STD 344-1975. The objective of this Qualification Program is to apply these standards to verify the adequacy of the design and manufacture of the High Range Containment Area Detector and Mineral-Insulated Cable System under the most adverse service conditions. 2.4 Reference Document List The following list documents the applicable references, standards, and drawings that apply to this Qualification. 2.4.1 Regulatory Guide 1.97, Revision 3, May,1983. I
" Instrumentation for Light-Water-Cooled Nuclear Power Plants to Assess Plant and Environs Conditions During and Following an Accident.
2.4.2 Regulatory Guide 1.89, November,1974.
" Qualification of Class 1E Equipment for Nuclear Power Plants" 2.4.3 Regulatory Guide 1.100, March,1976
" Seismic Qualification of Electric Equipment for Nuclear Power Plants".
2.4.4 Code of Federal Regulations,10, Energy, Part 50, Appendix B.
" Quality Assurance Criteria for Nuclear Power Plants and Fuel Reprocessing Plants".
- 2.4.5 NUREG-0588 l
i i
" Interim Staff Position on Environmental Qualification of Safety-Related Electrical Equipment".
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E 2.4.6 _IEEE STD 323-1974 "IEEE Standard for Qualifying Class IE Equipment for Nuclear Power Generating Stations". 2.4.7 IEEE STD 344-1975 "IEEE Reconsnended Practices for Seismic Qualification of Class 1E Equipment for Nuclear Power Generating Stations". 2.4.8 Kaman Specification 952837-001 Rev. B
" Ionization Charrber Assy. KDI-1000".
2.4.9 Kaman Specification 450593-001 Rev. K ( " Assembly Ionization Chamber". 2.4.10 Kaman Specification 852569-000 Rev A
" Cable Assy. M-F Mineral Insulated Triaxial".
2.4.11 Kaman Specification 852568-000 Rev. A 1
" Cable Assy. M-M Mineral Insulated Triaxial" 2.4.12 Kaman Specification 852570-000 Rev. A.
" Cable Assy. F-F Mineral Insulated Triaxial".
2.4.13 Kaman Specification 460034-001.Rev. B
" Performance Specification for Cable and Connector Assembly for High Range In-Containnent Area Monitor".
2.4.14 Kaman Specification 460033-001 Rev. A
" Installation Specification for Mineral-Insulated cables for High Range In-Containment Area Monitors".
2.4.15 Kaman Report A-82-70-U-(R)
" Report of Calibration Model KDA-HR High Range Area Monitor Ion Chamber Detector (P/N 824636-001)".
2.4.16 Kaman Calculation PM073184, Pa rt of Design Review File 460036-001. 2.4.17 Kaman Standard Practice Procedure KNP 18-104 Rev. A "KDI-1000 Factory Calibration" 2.5 Test Articles Description The items to be tested consist of six (6) principle assemblies mounted on a test platform.
2.5.1 Detector / Cable System 1 2.5.1.1 HV Cable assy. P/N 852569-000 Rev. A S/N later 2.5.1.1.1 Male mating connector P/N 852553-001 Rev. A 2.5.1.1.2 MI cable P/N 825284-001 Rev. C 2.5.1.1.3 Autoclave feed-through assy. (Special test hardware) 2.5.1.1.4 Female mating connector P/N 852552-001 Rev. A 2.5.1.2 Signal Cable assy. P/N 852569-000 Rev. A S/N later 2.5.1.2.1 Male mating connector P/N 852553-001 Rev. A 2.5.1.2.2 MI cable P/N 825284-001 Rev. C 2.5.1.2.3 Autoclave feed-through assy. (Special test hardware) 2.5.1.2.4 Female mating connector P/N 852552-001 Rev. A 2.5.1.3 Detector assy. P/N 450593-001 Rev /N later 2.5.1.3.1 Ion Chamber P/N 824636-003 Rev. B S/N later 2.5.1.3.1.1 HV female bulkhead connector P/N 852562-001 Rev. A 2.5.1.3.1.2 Signal female bulkhead connector P/N 852562-001 Rev. A 2.5.2 Detector / Cable System 2 2.5.2.1 HV Cable assy. P/N 852.569-000 Rev. A S/N later 1 2.5.2.1.1 Male mating connector P/N 852553-001 Rev. A 2.5.2.1.2 MI cable P/N 825284-001 Rev. C 2.5.2.1.3 Autoclave feed-through assy. (Special test hardware) 2.5.2.1.4 Female mating connector P/N 852552-001 Rev. A 2.5.2.2 Signal Cable assy. P/N 852569-000 Rev. A S/N later 2.5.2.2.1 Male mating connector P/N 852553-001 Rev. A 2.5.2.2.2 MI cable P/N 825284-001 Rev. C 2.5.2.2.3 Autoclave feed-through assy. (Special test hardware) l 2.5.2.2.4 Female mating connector P/N 852552-001 Rev. A 2.5.2.3 Detector assy. P/N 952837-001Rev.[/4Gi)
2.5.2.3.1 Ion Chamber P/N 824636-003 Rev. S S/N later 2.5.2.3.1.1 HV female bulkehead connector P/N 852562-001 Rev. A
=
2.5.2.3.1.2 Signal female bulkhead connector P/N 852562-001 Rev. A 2.5.2.3.2 Captive Detector mount assy. P/N 952701-003 Rev. S/N later 2.5.3 Penetration Connector System 3 2.5.3.1 Male-Female cable assy. P/N 852569-000 Rev. A S/N later 2.5.3.1.1 Male mating connector P/N 852553-001 Rev. A 2.5.3.1.2 MI cable P/N 825284-001 Rev. C 2.5.3.1.3 Autoclave feed-through assy. (Special test hardware) 2.5.3.1.4 Female mating connector P/N 852552-001 Rev. A
) 2.5.3.2 Female-Female cable assy. P/N 852568-000 Rev. A S/N later l
2.5.3.2.1 Female mating connector P/N 852552-001 Rev. A 2.5.3.2.2 MI cable P/N 825284-001 Rev. C 2.5.3.2.3 Autoclave feed-through assy. (Special Test Hardware) 2.5.3.2.4 Female mating connector P/N 852552-001 Rev. A 2.5.4 Penetration Connector System 4 2.5.4.1 Male-Female cable assy. P/N 852569-000 Rev. A S/N later 2.5.4.1.1 Male mating connector P/N 852553-001 Rev. A 2.5.4.1.2 MI cable P/N 825284-001 Rev. C 2.5.4.1.3 Autoclave feed-through assy. (Special Test Hardware) 2.5.4.1.4 Female mating connector P/N 852552-001 Rev. A 2.5.4.2 Female-Female cable assy. P/N 852568-000 Rev. A S/N later 2.5.4.2.1 Female mating cJnnector P/N 852552-001 Rev. A 2.5.4.2.2 MI cable P/N 825284-001 Rev. C 2.5.4.2.3 Autoclave feed-through assy. (Special test hardware)
j n 2.5.4.2.4 Female mating connector P/N 852552-001 Rev. A 2.5.5 Reference Cable System 5 2.5.5.1 Special cable assy.
, 2.5.5.1.1 MI cable P/N 825284-001 Rev. C S/N later 2.5.5.1.2 Autoclave feed-through assy. (Special test hardware) 2.5.5.1.3 Autoclave feed-through assy. (Special test hardware) 2.5.6 Reference Cable System 6 2.5.6.1 Special cable assy. s J
2.5.6.1.1 MI cable P/N 825284-001 Rev. C S/N later 2.5.6.2 Special cable assy. 2.5.6.2.1 MI cable P/N 825284-001 Rev. C S/N later ~ 2.5.6.3 Special cable assy. (as determined by Kaman Test ' Engineer). 2.6 Qualification Requirements Analysis The System is qualified by test. The following analysis justifies the { tests run, the envelope of environmental parameters, and the sequence of 4 testing.
]
2.6.1 Test Sequence The following test sequence is to be followed: Detector Calibration and Keep-alive Source characterization, Baseline evaluation and functional tests, aging test, evaluation and functional tests, irradiation test, evaluation and functional test, seismic test, evaluation and functional tests, LOCA Test, evaluation and functional . tests, and finally a detector calibration check. These tests are l detailed by procedures in PART 3 and are furtiler described below. 1 1 2.6.1.1 Detector Calibration and Keep-Alive Source Characterization The system is required to perform a measurement of 1 containment area . radiation fror.1 IE0 to IE7 Rads /hr within an I accurac A report of calibration (Ref. l 2.4.15)yon of a factor of two (2). an identical detector with different connectors i established the capability of the detector to generate accurate high range dose rate measurements. It is required that each installed system be calibrated -in the first three decades of measurement. This test is performed by Kaman, using procedure KNP 18-104 "KDI-1000 Factory Calibr 4n" (see paragraph 3.2). l In order to monitor the <fetector's abili ty to accurately measure j area radiation throughout those qualifir.1 tion tests where it is l (
s [ l l impractical to expose a large radioactive source, the keep-alive source is utilized. Kaman provides an installed radioactive " Keep-alive" source in radiation monitor ion chamber detectors. This source is a [ small radioactive nuclide that is sealed inside the ion chamber. This source provides two functions for the user: a continuous check on system integrity and an indication of electronic calibration. The system's integrity is assured by a microcomputer or / ratemeter limit check on the detector output. The " keep-alive" ( source has been designed -to - produce a current level of 10-50 picoamperes. If the. detector output falls below a predetermined threshold (approximately 5 picoamperes) due to a disconnected or { damaged cable, loss of internal gas pressure in the ion chamber, or failure of the preamplifier or high voltage electronics, the microcomputer or ratemeter will declare a detector failure and steps to remedy the cause can be initiated by the operator. i The electronic calibration can be monitored by comparing the observed output " keep-alive" level to the " keep-alive" level determined nominal for the detector during factory calibration (ambient radiation levels must be well below the detector's minimum detectable level). Any subsequent " keep-alive" level that compares favorably with the nominal " keep-alive" level is indicative of adequate electronic calibration. Long term (one
! hour or one day) average " keep-alive" levels that are consistently different from the nominal level by a factor of greater than two are indicative of the need for electronic calibration. If the long term average remains out of tolerance f after electronic calibration, there may be a problem with the detector (or its cable) and a detector radioactive calibration or replacement should be considered.
2.6.1.2 Baseline (and subsequent) Evaluation and Functional Tests After the test articles have been mounted on the test platform (Ref. procedure 3.1) the Baseline Evaluation and Functional Tests are performed. The same tests are performed before and after each subsequent test in the test sequence. The evaluation and functional test acceptance criteria are presented in paragraph 2.8. 2.6.1.2.1 Evaluation Tests Evaluation Tests are electrical tests run on de-energized test articles to determine continuity, voltage withstano capability, insulation resistance, and dielectric integrity of all test article components. This test procedure and data is listed in paragraph 3.3. t
2.6.1.2.2 Functional Tests ; Functional Tests are system tests run on Test Articles 2.5.1 and 2.5.2 to determine the ability of the system to accurately indicate the keep-alive radioactive source current. This test is also utilized during the irradiation, seismic, and LOCA tests to continuously monitor system performance. See the test procedure and data record in paragraph 3.3. 2.6.1.3 Aging Tests
' The system is designed for a 40 year qualified and installed life. The system components are entirely of metallic, mineral, and inert gaseous material, and have no known age-related failure modes or synergisms that could be simulated by accelerated thermal techniques. The possible aging mechanisms for this i equipment are by material state changes due to irradiation, fatigue-cycling by plant-induced or seismic vibrations, or by mechanical failure due to connect / disconnect cycles. The former two mechanisms are tested separately (Ref. para. 2.6.1.4 and 2.6.1.5), and the latter mechanism, mechanical cycling, is tested per the procedure listed.in paragraph 3.4.
Since the detector may be removed for periodic calibration at a remote facility, the purpose of this test is to simulate the stress history in.the cable and connector that would be caused by the number of connect / disconnect cycles that may reasonably be expected to occur during the 40 yr. life of the equipment. These tests will be performed by Kaman after Baseline Functional Tests at Kaman facilities. In actual service, Kaman requires replacing the 0-ring P/N 825335-013, in the connector each time the cable is reconnected to the ion chamber (such as when the ion chamber is reinstalled after a periodic calibration test). Thus, the 0-ring itself is not subject to mechanical cycling. 2.6.1.4 Irradiation Tests in order to place the equipment in a condition which simulates its end-of-qualified life plus accident condition, the equipment shall be exposed to a Total Integrated Dose (TID) of 2.2E8 Rads from a Cobalt 60 source. This dose represents the maximum specified background TID for the equipment over a 40-year service life plus the accident-level irradiation dose plus 10% ma rgin. The rate of exposure shall not exceed IE7 Rads /hr. Care 1 should be taken to ensure that the specimen receives a uniform exposure. The Total Integrated Dose shall be determined by NBS traceable oosimetry techniques. An irradiation report including certification of radiation dose shall be supplied by the irradiation facility. See the test procedure and data record in paragraph 3.5. l
L At least one of test article 2.5.1 or 2.5.2 may be energized k.- and functional during the radiation exposure as a check on the system operation. This test does not constitute a calibration of - the system. H 2.6.1.5 Seismic Tests See the detailed test procedure and data record in paragraph 3.6. 2.6.1.5.1 Resonance Frequency Search A low level resonance search shall be conducted on the equipment as mounted in the test fixture. The resonance search y shall be conducted in each of the three orthogonal directions [ following the guidelines of Paragraph 6.6.2.5 of IEEE 344-1975. A sufficient number of accelerometers shall be mounted on the equipment, including cables, and monitored to identify sources of resonant vibration and the corresponding amplificaticn factor. A sinusoidal input not exceeding 0.2g shall be applied in the range from 1 to 200 Hz and from 200 to 1 Hz at a sweep rate not to exceed 2 octaves per minute. For each resonance that is found, the test laboratory shall record the frequency, amplification factor, and source. 2.6.1.5.2 Vibration Aging The purpose of this test is to subject the equipment to vibrations similar to those that will be encountered during its service life. The equipment shall be monitored visually for evidence of any mechanical damage or deterioration. The equipment shall be subjected to a biaxial or triaxial vibration consisting of random multiple frequency input motion. The input motion shall be adjusted such that the test response spectrum (TRS) envelopes the vibration aging required response spectra (RRS) shown in Figure 2 over the entire frequency range. Note that the upper frequency value for this motion is 200 Hz. The duration of this test shall be 30 minutes for each axis. It is not necessary that the test be continuous; however, the total of all time increments must equal 30 mirates for.each axis. The SRV aging test may be accomplished by the use of 10 second to 30 second duration pulses at the maximum SRV level, with a pause in between. The waveform shall be amplitude controlled in at least 1/3 octave steps from 1 to 200 Hz. The TRS shall be analyzed in at least 1/6 octave intervals at both 2% and 4% damping factor from 1 to 200 Hz. The table shall be equalized to the RRS prior to performing this series of tests, i i
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'The equipment, as mounted on the test fixture, shall be
, subjected to five OBE and one SSE excitations in each orthogonal direction. The input motion for these excitations shall be of random motion multifrequency wavefoms. The waveform shall be amplitude controlled in at least 1/3 octave steps form 1 to 100 Hz. Each excitation shall be of 30 seconds duration. The ( Required Response Spectrum (RRS) for the OBE excitation is shown in Figure 3, while Figure 4 shows the RRS for the SSE excitation.
- The table shall be equalized to the appropriate RRS prior to this f test. A Test Response Spectrum (TRS) analyzed at a 2% damping L factor for the OBE excitation and at a 2% damping factor for the SSE excitation in at least 1/6 octave intervals from 1 to 100 Hz e shall be supplied. Besides the control accelerometers, triaxial
[ accelerometers shall also be placed at one location on each fon chamber and at a minimum of 3 locations on the cable assembly as deemed appropriate by all personnel and KI Engineering. The equipment shall also be visually monitored for evidence of any mechanical degradation or failures, and functionally monitored for integrity of signal. In the event tiie TRS fails to envelope the RRS, the test facility shall provide justification for the adequacy of the TRS. 2.6.1.6 LOCA Test The Loss of Coolant Accident (LOCA) test is designed to demonstrate that the equipment can perform its Class 1E function during a LOCA event. The profile to be simulated is shown in Figure 5. The equipment will be monitored continuously by Kaman personnel at the start of the test, then periodic readings will be taken. The main parameters to be monitored are the
" keep-alive" signal currents. Insulation resistance (IR) tests will also be performed at certain intervals and are required to be performed at least once at every stabilized temperature.
2.6.1.7 Detector Calibration Check The test of para. 2.6.1.1 is repeated as assurance that the measurement accuracy has not degraded. 2.7 Environmental Conditions 2.7.1 Storage, Handling and Installation Conditions The detector and cable assemblies shall be protected from environmental conditions during transport, storage, and pre-test handling operations. The test articles shall be mounted on a test platfo a suitable for transport and mounting / demounting in all required test environments without undue exposure to mechanical damage.
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The temperature extremes shall not exceed 0 F to 150 F during storage or transport. Avoid rapid ( 20 F/hr.) temperature changes. are Relativedirect Avoid humidityexposure conditions to of 0-100% (non-condensing)(snow, condensing moisture allowed. rain, condensation). Shock and vibration shall be minimized during transport and handling. Self-recording shock indicators (3 axes) shall be mounted on the test platform and periodically monitored for status. General cleaning of test articles and test platform, if needed, should be accomplished using a brush, vacuum cleaner, and/or dry cotton rag. The cable connectors and end preparations shall be capped f or bagged with a dessicant to keep the test connections dry and clean. Prior to connection to test instrumentation appa ratus, connectors shall be cleansed with a cotton swab moistened with de-natured alcohol or de-ionized water, then thoroughly dried with a heat gun (350*F max). 2.7.2 Conditions of Normal Service
, During periods of monitored tests the laboratory environment / test cell shall be maintained at 50*F - 104*F,10-g5% RH (non-condensing) conditions, except for specific test requirements.
2.7.3 Test Environments 2.7.3.1 Baseline (and Subsequent) Evaluation and Functional Tests Per conditions of normal service (para. 2.7.2) except relative humidity should not exceed 50% RH (non-condensing). 2.7.3.2 Aging tests Per conditions of Normal Service (para. 2.7.2). 2.7.3.3 Irradiation Tests 2.7.3.3.1 Temperature and humidity shall be as listed in conditions for nonnal service (para. 2.7.2). 2.7.3.3.2 Exposure: 2.2 E8 Fads Co-60 at a rate nct to exceed IE7 Rads /hr (Instrument range limit). 2.7.3.4 Seismic tests 2.7.3.4.1 Temperature and humidity shall be as listed in conditions for normal service (para. 2.7.2) except during periods of evaluation and functional test recording when the relative humidity conditions shall be as listed in paragraph 2.7.3.1. 2.7.3.4.2 Resonance Search Sine-wave input motion excitation not to exceed 0.2g from 1 to 200 to 1 Hz in each of three orthogonal directions.
J 2.7.3.4.3 Vibration Aging Biaxial or triaxial random multi-frequency input motion per figure 2 and paragraph 2.6.1.5.2. 2.7.3.4.4 Seismic Tests Biaxial or triaxial random multi-frequency input motion per figures 3 and 4 and paragraph 2.6.1.5.3. 2.7.3.5 LOCA Test 2.7.3.5.1 The temperature, pressure, and spray conditions of figure 5 and paragraph 2.6.1.6 shall be maintained. 1 2.7.3.5.2 Conditions external to the LOCA test apparatus shall be as listed in conditions for normal service (para. 2.7.2) except during periods of evaluation and functional test recording when the relative humidity conditions shall be as listed in para.
- 2.7.3.1.
2.7.4 Margin The environmental parameters include margin insofar as these generic parameters have been derived by reviewing a large number of power plant specific requirements, and designing the equipment to meet or exceed the maximal envelope of these requirements. The envelope of e generic test parameters therefore tests the equipment to the design level, providing an indication of the maximum environment that the l equipment is capable of surviving. . t In general, the curves represented in this document include the following minimum margins for most specific applications, and no additional margin should be added by the test facility: Mechanical Aging +10% connect / disconnect cycles Irradiation +10% total integrated dose Seismic vibration +10% acceleration < LOCA temperature +15'F l LOCA pressure +10% gauge i LOCA transient applied twice 2.8 Acceptance Criteria The following parameter limits are to be maintained for all evaluation and functional tests (Ref. document 2.4.16). l l l
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I v 2.8.1 Evaluation Tests 2.8.1.1 Conductor Continuity article 2.5.1.1 < 203.6 ohms , article 2.5.1.2 2 213.6 ohms article 2.5.2.1 2~235.4 ohms article 2.5.2.2 2 245.4 ohms , [$ ' article 2.5.3 article 2.5.4 2 227.4 ohms 2 240.6 ohms article 2.5.5 -5321.6 ohms 2.8.1.2 Insulation Resistance conductor o guard guard to s feld article 2.5.1.1 > 1.0 x 10 ohms > 1.0 x 10 ohms article 2.5.1.2 s 2.7 x 10 ohms s 1.0 x 10 ghms article 2.5.2.1 s 1.0 x 10 ohms' s 1.0 x 10 ohms f article 2.5.2.2 s 2.7 x 10 ohms s 1.0 x 10 ohms article 2.5.3 s 3.0 x 10 ohms s 1.0 x'10 ohms article 2.5.4 s 3.0 x 10 ohms I s 1.0 x.10 ohms article 2.5.5 E1.3x10 ohms E1.0x10 ohms 2.8.1.3 Noise Measurements millivolts picoamps article 2.5.1.2 < 58.0 < 10 article 2.5.2.2 2 58.0 2 10 article 2.5.3 2 30.0 2 10 article 2.5.4 s 30.0 ' 2 10 article 2.5.5 51300.0 i10 2.8.1.4 Voltage Withstand Each cable must not breakdown when a d.c. potential 1000V is applied center conductor to guard. Breakdown is defined as current in excess of 1 milliampere. 2.8.2 Functional Tests , i j Articles 2.5.1 and 2.5.2 will be checked for actual function initially (baseline) and before and af ter each test in the sequence, and during irradiation, seismic testing, and LOCA testing, except during the periodic evaluation tests. A record shall be made of the l keep-alive current measurement (at 800 80 Vdc High voltage) that congitutes proof of function. The current shall be_ greater than 1 x 10 amperes. i i I i . 2
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3.0 SUPPORTING DOCUMENTS 3.1 Generalized Preparation and Handling Guide This sectio provides guidance and reference for activities necessary , to qualify the equipment. I QA shall perfonn surveillance on a timely basis. As a minimum, and ' unless otherwise specified, a QA representative will witness testing one time during a qualification test sequence (seismic, LOCA, etc.) If Kaman QA is not available, the testing services vendor shall provide a Quality representative for this function. The data sheet of the testing witnessed will be marked " witnessed", signed, and dated by the Quality representative. 3.1.1 Preparation of Test Platfonn Figure 6 indicates the layout of the test articles on the test platform. The mineral-insulated cable shall be attached to the ' platform using the procedure of reference 2.4.14 as guidance for mounting the equipment. 3.1.2 Calibration of Detectors Prior to installation of the KDI-1000 detectors on the test platform, calibrate them per the procedure listed in paragraph 3.2. Record data on a Qualification Data Record (QDR) Sheet. See figure 7. 3.1.3 Perform Baseline Evaluation and Functional tests per the procedure listed in paragraph 3.3. Record data on QDR sheets. 3.1.4 Perform Mechanical aging tests per the procedure listed in ! paragraph 3.4. Record data on QDR sheets. 3.1.5 Perform Evaluation and Functional tests per the procedure listed in paragraph 3.3. Record data on QDR sheets. l 3.1.6 Shipping I The test articles, affixed to the test platform, will be shipped to one or more facilities as necessary to accomplish irradiation tests, seismic tests, an LOCA tests. The test platform shall be palletized and protected from exposure to mechanical damage. Transport shall be by best available means, commercial or private, that satisfies schedular constraints. Shock gauges and temperature indicators shall be mounted on the test platform to provide a indication of shipping environments experienced. The shock and temperature data obtained after each delivery shall be recorded on a QDR sheet. i l { l
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FIGURE 7 Qualification Data Record Date Record Sheet # Title of Test: Test Procedure: Sequence #: 1
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Test Article: Test Method: Test Equipment: Mfr/Model/S/N: . Calib. Due: Ambient Temp: Ambient RH: Time: Date: By: QC Stamp: Acceptance Test Article ID Reading Criteria
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[ NOTE: The KDI-1000 detectors each contain approx. 0.1 microcurie Am-241 isotope as a keep-alive source. Each carrier and laboratory requires notification of radioactive content. The source is not an exempt quantity and requires the carrier (s) and the laboratory (ies) to possess a byproducts license or under the reciprocity agreement, Kaman can temporarily extend its license to these facilities after notification to the NRC. 3.1.7 The Evaluation and Functional Test procedure of para. 3.3 shall be performed after every del ivery , prior to the subsequent qualification test. Record all dati on QDR sheets. 3.1.8 Irradiation Tests g Perform the Irradiation tests per the procedure listed in l paragraph 3.5. Record data on QDR sheets. 3.1.9 Perform Evaluation and Functional tests per the procedure listed in paragraph 3.3. Record the data on QDR sheets. { 3.1.10 Shipping Deliver the test articles to the seismic test laboratory. Follow the guidance provided in paragraph 3.1.6. 3.1.11 Perfonn the Evaluation and Functional test procedure as listed in paragraph 3.3. Record data on QDR sheets. 3.1.12 Seismic Tests
; Perform the resonance search, vibration aging and seismic tests per the procedure listed in paragraph 3.6. Record data on QDR sheets.
3.1.13 Perform the evaluation and functional test procedure as listed in paragraph 3.3. Record data on QDR sheets. r 3.1.14 Shipping (if required) Deliver th: test articles to the LOCA test laboratory. Follow the guidance. provided in paragraph 3.1.6. 3.1.15 Perform the Evaluation and Functional test procedure as listed in paragraph 3.3 Record data on QDR sheets. 3.1.16 LOCA Tests Perform the LOCA test per the procedure listed 'in paragraph 3.7. Recard data on QDR sheets. 3.1.17 Perform the Evaluation and functional test procedure as listed in paragraph 3.3. Record data on QDR sheets. 3.1.18 Shipping Deliver the test articles to Xaman Instrumentation. Follow the guidance provided in paragraph 3.1.6.
ll 3.1.19 Calibration Check De-mount the KDI-1000 fon chamber detectors and calibrate them F per the procedure listed in paragraph 3.2. Record data on QDR sheets, w " 3.1.20 Storage i The test articles shall be preserved for a minimum period of 5 1 years. J l J I 4 i i i I l s i i i i t k l l d l l l w l l
[,- h 3.2 Calibration Procedure Kaman procedure KNP 18-104 Revision A (Ref. 2.4.15) shall be performed before the detectors are mounted on the test platform (test sequence 3.1.2) (. and after de-mounting the detectors at the conclusion of Qualification testing (test sequence 3.1.18). Record data on KNP 18-104 data sheet. ( ( I f_,-- , ~ - , . -- n- . ,-,. - . , . -,. - - - . - - , -- - . , - - - -.-.-e . - . - ,v-
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3.3 Evaluation and Functional Test Procedure. J 3.3.1 This procedure shall be perfonned before and after each qualification test, at test sequences:
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3.1.3 Baseline tests before Mechanical Aging 3.1.5 After Mechanical Aging 3.1.7 Before Irradiation 1 3.1.9 After Irradiation J 3.1.11 Before Seismic 3.1.13 After Seismic 3.1.15 Before LOCA
]
3.1.17 After LOCA The Qualification Data Record (QDR) sheet is to be used to record all readings. Use a separate QDR sheet for each of the following - tests, listing each applicable test article on the QDR. 3.3.2 Test Equipment
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Equipment must be in current calibration, with calibration traceable to NBS. Record manufacturer, model no., serial no. and calibration dates for each equipment used on the QDR. 3.3.2.1 Ohm Meter, 0.1 Ohms Resolution 3.3.2.2 Megohmeter Capable of 10 13 Ohms and 500 vdc. 3.3.2.3 High Voltage Power Supply, Variable,10 to 1000 vdc. 3.3.2.4 Digital Multimeter Capable of 1.0 Microvolt Resolution -{ and 1 Microamp Resolution. 3.3.2.5 Electrometer Capable of Measuring 9E-12 Amps 3.3.2.6 Breakdown Voltage Tester capable of 1000 vdc. (opt.) 3.3.2.7 Kaman Model KEM Microcomputer Ratemeter (opt.) 3.3.3 Evaluation Tests 3.3.3.1 Conductor Continuity Continuity tests - are to be performed on the cables where there is access to both ends of the cable. For the baseline test of 3.1.3, this includes the HV and signal cables of test articles 2.5.1 and 2.5.2. After the final mating of conr.ectors during mechanical aging, these cables will no longer be accessible for continuity check until the final Post-LOCA evaluation test. CARE MUST BE TAKEN WHEN CONNECTING INSTRUMENT CLIPS OR LEADS ONTO THOSE CABLES THAT ARE NOT TERMINATED WITH CONNECTORS. 3.3.3.1.1 Record position in test sequence. 3.3.3.1.2 Record cable assembly number. L.
3.3.3.1.3 Adjust the "zero-ohms" for the scale in use. [ 3.3.3.1.4 Connect a lead to each end of the cable conductor. l 3.3.3.1.5 Determine net center conductor resistance. Record on QDR. 3.3.3.1.6 Record acceptance criteria from paragraph 2.8.1.1 for each cable. 3.3.3.2 Insulation Resistance Tests IR tests are to be performed on each cable assembly, including cable loops and High Voltage and Signal cables connected to the detectors. 3.3.3.2.1 Record position in test sequence. 3.3.3.2.2 Record cable assembly number. 3.3.3.2.3 Set megohmmeter at 500VDC 3.3.3.2.4 Connect Megohmmeter as shown in Figure 8a. Measure insulation resistance between center conductor and inner guard. Record on QDR. 3.3.3.2.5 Connect Megohnneter as shown in Figure 8b. Measure insulation resi;tance between guard and outer sheath. Record on QDR. 3.3.3.2.6 Record acceptance criteria from paragraph 2.8.1.2 for each cable. 3.3.3.3 Noise Measurements Current and voltage tests are to be performed on each cable and cable / detector assembly. 3.3.3.3.1 Record position in test sequence. 3.3.3.3.2 Record cable assembly number. 3.3.3.3.3 Set voltmeter to most sensitive (or 1 microvolt) scale. 3.3.3.3.4 Connect positive (+) voltmeter lead to center conductor, negative (-) voltmeter lead to guard. Record on QDR. 3.3.3.3.5 Set electrometer to most sensitive (or 10-11 amp) scale. 3.3.3.3.6 Connect positive (+) electrometer lead to center conductor, negative (-) electrometer lead to guard. Record on QDR. a
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3.3.3.3.7 Record acceptance criteria from paragraph 2.8.1.3 for l : each listed cable. 3.3.3.4 Voltage Withstand Tests Withstand . voltage tests are to be performed on ech cable and cable / detector assembly. NOTE: This test may be destructive if excessively high potentials are applied to the cables. Use extra caution in performing this test. 3.3.3.4.1 Record position in test sequence. 3.3.3.4.2 Record cable assembly number. 3.3.3.4.3 Connect the multimeter as an ammeter and the High Voltage P/S as shown in figure 9. 3.3.3.4.4 Apply 1000VDC (+0, -20vdc) maximum to the cables. Measure and record leakage current on QDR. 3.3.3.4.5 Record established acceptance criteria from paragraph
'2.8.1.4 for each cable.
3.3.4 Functional Tests Functional tests are to be perfonned on test articles 2.5.1 and 2.5.2 only. 3.3.4.1 Record position in test sequence. 3.3.4.2 Record test article assembly number. 3.3.4.3 Connect equipment as shown in Figure 10. 3.3.4.4 Initial Settings: 3.3.4.4.1 Set Electrometer as follows: Range: Ampere (10-10 or 10-11) Mode: Fast Sensitivity: 0.01 Rear Connecti n Points: Grounding Strap in place between "LO" and " Ground" Instrument power - grounded , 3.3.4.4.2 Set High Voltage Power Supply as follows: 0.C. Output Voltage: set to "zero" Instrument Power: grounded NOTE: Both the Electrometer and the HV Power Supply must be connected to the same facility power outlet box to avoid grounding loops.
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H.V. P/S Ammeter l l Note: Do not exceed 1000 V Output from H.V. P/S. , I l , FIGURE 9 VOLTAGE WITHSTAND TEST CONNECTIONS l l l l l . , - -
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3.3.4.4.3 Set Digital Voltmeter as follows: Mode: Volts Range: 1000 VDC Instrument Power: Grounded Instrument Power: Grounded ) 3.3.4.4.4 Verify all equipment connections and settings. 3.3.4.4.5 Turn Electrometer on, let unit warm up for at least 30 minutes for stabilization if cold start. 3.3.4.4.6 Set range on Keithley Electrometer to 10-10 or 10-11' amperes.and on " Fast" mode. 3.3.4.4.7 Turn High Voltage Pwoer Supply on; slowly increase i output voltage to 800 VDC, monitoring the output voltage on the DVM. 3.3.4.4.8 Zero Electrometer by putting sensitivity on " Auto" and energize "zero check" switch, turn "zero" knob until readout is
".00000".
3.3.4.4.9 Set Electrometer controls as follows: Zero Check Switch - on Sensitivity'g 0.001 Range - 10 Coulomb (or range corresponding to count elapsed time in step 3.3.4.4.10 times the current reading observed with Electrometer on " Ampere" scale.) (Note: Range may need to be set to a higher range during the irradiation test) 3.3.4.4.10 De-energize zero check switch and observe the coulomb count reading, using a stopwatch, to determine the approximate number of counts that occur in 60 seconds. This will be used to
- determine the count interval that will be timed in step 3.3.4.4.13. j 1
EXAMP l x 10'g:in an elapsed time of approximCoulomb reading went U from a appro ' count interval from 0.100 to 2.100 x 10'9ely 60 seconds.(count =2000x1 3.3.4.4.11 Reset the count reading to zero by energizing the zero check switch. 3.3.4.4.12 Record High Voltage Reading on DVM. l 3.3.4.4.13 De-energize zero check switch; start stopwatch when count reads the lower value of count interval established in Step 3.3.4.4.10. Stop the stopwatch when count reads the upper value of the count interval established in Step 3.3.4.4.10. Record l count interval and elapsed time on the data sheet. , NOTE: The count interval may be different than established in i Step 3.3.4.4.10. The significant data is the time that l has elapsed during a known count interval. l
l
.3.3.4.4.14 The signal current is obtained by dividing the count !
interval by the elapsed time. Record the signal current on the ' data sheet. EXAMPLE: Count Start =0.200 x 10-9 coulombs Count End = 2.300 x 10-9 coulombs Elapsed Time = 61.5 sec Signal Current = (2.300-0.200) x 10-9 61.5
= 3.41 x 10-II A 3.3.4.4.15 Confirm calculated signal current by switching Electrometer to " Ampere" mode and decade of calculated value.
Record on data sheet. 3.3.4.4.16 Record acceptance criterion from paragraph 2.8.2 for each detector. NOTE: Alternative to the above procedure, connect the test articles to the HV and SIG connectors of the KEM microcomputer. Turn-on the microcomputer, set the radiation rate conversion constant (parameter 09) to 1.00E00, let stablize for 30 min. and record the previous 10 minute average radiation rate (parameter 25). This is the preferred method for monito-ing the function during the irradiation test, or testing the long-term keep-alive average current.
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3.4 Mechanical Aging Test Procedure 3.4.1 This test simulates the expected connect / disconnect cycles for each connector. Each mechanical cycle shall consist of uncoupling the detector connector, for test articles 2.5.1.1, 2.5.1.2, 2.5.2.1, 2.5.2.2, - 2.5.3, and 2.5.4, moving it back at least 1 inch from the mating connector and then reconnecting it. Any clamps or cable supports on the last 3 feet of the cable, including the strain relief loop, shall { be removed during this test. 1 The number of mechanical cycles is based on the assumption of a detector calibration check occurring at every fuel load, and a fuel load occurring every 18 months during the 40 year operating life of the plant. This yields a total of 27 in-site connect / disconnect ' cycles. It is also estimated that up to 3 additional connect / disconnect cycles may occur during each calibration check. During calibration checks, the connectors would typically be hand-tightened, and flexible cable would likely be used rather than MI cable. The in-site connection to the MI cable would require application of the proper torque to the connector to insure integrity of the 0-ring. To simulate these conditions, a totiil of 30 connect / disconnect cycles shall be performed with the connector tightened to the specified torque value each cycle using a new 0-ring each time, and the connector hand90tightened connecteach
/ disconnect cy(cles cycle 0-ring shall be replacement perfarned with optional).
These cycle numbers include a 10 percent margin. At the completion of mechanical cycling, a new 0-ring shall be installed inthe throughout theremainder connector andtest. of the this connection shall be left intact 3.4.2 Test Equipment A calibrated torque-wrench capable of registering 25 ft. - lbs. torque is required for this test. 3.4.3 Test ' l 3.4.3.1 Record the test sequence number. I 3.4.3.2 Record the test article number. 3.4.3.3 Perform 90 hand-tightened connect / disconnect cycles on 1 each connector pair listed above. 3.4.3.4 Install a new gas-filled metal 0-ring P/N 825335-013, hand-tighten each connector pair, and using the proper tools, torque each connector pair to 25 ft. - lbs. Record on QDR. 3.4.3.5 Loosen each connector pair (again using proper tools) ' and disconnect connectors, removing the used 0-ring. ' 3.4.3.6 Repeat steps 3.4.3.4 and 3.4.3.5 28 additional times. Record on QDR. l t .
3.4.3.7 Thoroughly clean and dry each connector interface surface (Ref. 2.4.14). 3.4.3.8 Perform a cosiductor continuity .and an insulation resistance check of each mating connector half, per procedures listed in paragraphs 3.3.3.1 and 3.3.3.2. Record on QDR. 3.4.3.9 - Make final- torqued connection with a new metal 0-ring installed, per paragraph 3.4.3.4. Record on QDR. l b
N 3.5 Irradiation Test Procedure 3.5.1 Introduction This test is performed by a vendor facility. The procedure that follows may be modified as required by the test facility to adapt this i requirement to facility-specific capability and/or standard practice. Any such procedural modification shall be submitted via a " Deviations, Anomalies, and Failure Report" form (see Figure 1) and approved by Kaman prior to conunencing the test. A Kaman Test Engineer shall % present at the commencement of this test, as a minimum. The Kaman personnel shall perfonn all evaluation and functional tests, and oversee the test facility personnel in establishing the required test environments and fixturing. Instruction of test facility personnel in any procedures necessary to monitor the test articles during the test will be performed by the Kaman Test Engineer. The listed test procedure is to commence after all necessary fixturing and pre-test evaluation and functional tests have been completed. All data is to be recorded on QDR forms and/or test facility standard forms. 3.5.2 Test Equipment 3.5.2.1 A Co-60 gama irradiation source capable of providing a total dose, uniformly exposed to the test articles as mounted on the test platform of 2.20E8 10% Rads (air), in a period not to exceed 7 contigucus calendar days, at a rate not to exceed 1.00E7 Rads (air)/hr. 3.5.2.2 Dosimetry of the irradiation test, certified traceable to the NBS. 3.5.2.3 Fixturing as required by and supplied by the vendor facili ty. 3.5.2.4 Kaman-supplied monitoring equipment consisting of the functional test equipment listed in para. 3.3.2.3, 3.3.2.5, and/or 3.3.2.7, including accessory cables and fixtures. 3.5.3 Pre-requisites 3.5.3.1 The test facility shall not proceed with the test until , authorized by Kaman under a Purchase Order instruction, which ' shall include as a minimum, review and acceptance by Kaman Quality Assurance audit that the test facility conforms to the appropriate sections of 10CFR50 App. B, or equivalent, and an approved vendor test procedure or the following procedure, amended as necessary by a Deviations, Anomalies, and Failure Reportform(Figure 1). i
-3.5.3.2 A calculation of the expected minimum and maximum-expected dose rate for the specific test configuration, and a calculation of expected exposure duration to - acquire the total dose.
3.5.4 Procedure 3.5.4.1 Record the test sequence number. 3.5.4.2 Record the test article (s) number. 3.5.4.3 Expose the irradiation source. Record the time of commencement and the expected completion. 3.5.4.4 At a pre-determined point prior to one-half the Total Dose exposure, measure the actual dose and/or dose rate and confirm the expected completion time. 3.5.4.5 Kaman personnel may ' monitor the exposure rate by energizing the test articles. Such measurement does not constitute an instrument calibration nor substitute for vendor-provided traceable dosimetry. It is a functional test only. 3.5.4.6 At the conclusion of the exposure, the total dose measurement devices shall be checked for total actual dose delivered. 3.5.5 Report A vendor certification of total dose, dose rate, type, & articles tested shall be supplied as a final report from the vendor facility. 3.5.6 Records Exposure data shall be recorded on data-retrievable media for additional data reduction, if required, for a period of five years. m
3.6 Seismic Test Procedure 3.6.1 Introduction This test is performed by a vendor facility. The procedure that follows may be modified as required by the test facility to adapt this requirement to facility-specific capability and/or standard practice. Any such procedural modification shall be submitted via a " Deviations, Anomalies, and Failure Report" form (see Figure 1) and approved by , Kaman prior to commencing the test. A Kaman Test Engineer shall be present at the commencement of this test, as a minimum. The Kaman personnel shall perfonn all evaluation and functional test, and oversee the test facility personnel in establishing the required test environments and fixturing. Instruction of test facility personnel in any procedures necessary to monitor the test articles during the test will .be performed by the Kaman Test Engineer. The listed test procedure is to commence after all necessary fixturing and pre-test evaluation and functional tests have been completed. All data is to be recorded on QDR forms and/or test -facility standard forms. 3.6.2 Test Equipment 3.6.2.1 A vibration test facility capable of providing the forces necessary to meet the Required Response Spectra of Figures 2, 3, and 4 with either an independent biaxial or a triaxial seismic test simulator.
- 3.6.2.2 Control and recording equipment necessary to perform the l
described tests, prevent uncontrolled excursions of the test articles , and to provide the required Test Response Spectra i plots. Equipment used shall be in calibration and listed on a QDR, or equivalent forms. 3.6.2.3 Fixturing as required by and supplied by the vendor facility. 3.6.2.4 Kaman supplied monitoring equipment consisting of the evaluation and functional test equipment listed in para. 3.3.2, including accessory cables and fixtures. 3.6.3 Prerequisites 3.6.3.1 The test facility shall not proceed with the test until authorized by Kaman under a Purchase Order authorization, which shall include, as a minimum review and acceptance by Kaman Quality Assurance audit that the test facility conforms to the appropriate sections of 10CFR50 App. B, or equivalent, and an approved vendor test procedure or the following procedure amended l as necessary by a Deviations, Anomalies, and Failure Report form (Figure 1). l
3.6.3.2 Test article exposure to vibration spectra may comence only af ter the vibration test table has been equalized to the specified RRS using a durr.wy mass. 3.6.4 Procedure 3.6.4.1 Record the test sequence number. 3.6.4.2 Record the test article (s) number. 3.6.4.3 Perform the resonance frequency search to the parameters listed in paragraph 2.6.1.5.1. 3.6.4.4 Perform the vibration aging test to the parameters listed in paragraph 2.6.1.5.2. 3.6.4.5 Perform the seismic tests to the parameters listed in paragraph 2.6.1.5.3. 3.6.4.6 Kaman personnel will monitor the test articles during the seismic tests by performing the functional test listed in paragraph 3.3.4. 3.6.5 Report At the conclusion of the seismic tests, the test facility shall provide certification of tests run, articles tested, and the following plots, which will constitute the final report from the vendor facility. 3.6.5.1 A TRS for the resonance frequency search for each test and control accelerometer, for each axis. 3.6.5.2 A TRS for the vibration aging test for each test and control accelerometer, for each axis. 3.6.5.3 A TRS for the OBE seismic test for each test and control accelerometer, for each axis. 3.6.5.4 A TRS for the SSE seismic test for each test and control accelerometer, for each axis. 3.6.6 Records Test response data shall be recorded on data-retrievable media for additional data reduction, if required, for a period of five years.
- - l 3.7 LOCA Test Procedure 3.7.1. Introduction This test is performed by a vendor facility. The procedure that follows may be modified as required by the test facility to adapt this requirement to facility-specific capability and/or standard practice.
Any such procedural modification shall be submitted via a " Deviations, Anomalies, and Failure Report" form (see Figure 1) and approved by l Kaman prior to commencing the test.
~
A Kaman Test Engineer shall be present at the comencement of
; this test, as a minimum. The Kaman personnel shall perform all evaluation and functional test, and oversee - the test facility personnel in establishing the required test environments and i l' fixturing. Instruction of test facility personnel in. any procedures '
l necessary to monitor the test articles during - the test will ' be perfomed by the Kaman Test Engineer. 4 l The listed test procedure is to comence after all necessary
- fixturing and pre-test evaluation and functional tests have been
, completed.
1 ' All data is to be recorded on QDR forms and/or test facility standard forms. 3.7.2 Test Equiwient 3.7.2.1- A LOCA test facility (autoclave) capable of providing the required environmental transients of Figure 5 and accepting .- l the test platform of Figure 6 with necessary feed-throughs for
- external test connections.
i 3.7.2.2 Control and recording equipment necessary to perform the described tests, prevent uncontrolled excursions of the l environment in which the test articles reside, and to provide the
, required environmental plots. Equipment used shall be in calibration and listed on a QDR, or equivalent, form, i
3.7.2.3 Fixturing as required by and supplied by the vendor facility. 3.7.2.4 Kaman-supplied monitoring equipment consisting of the test equipment listed in para. 3.3.2, incluiing accessory cables and fixtures. 3.7.3 Pre-requisites 3.7.3.1 The test facility shall not proceed with the test until authorized by Kaman under a Purchase Order instruction, which will include, as a minimum, review and acceptance by Kaman Quality Assurance audit that the test facility conforms to the appropriate sections of 10CFR50 App. B, or equivalent, and an approved vendor test procedure or the following procedure amended as necessary by a Deviations. Anomalies, and Failure Report form (Figure 1).
1 l 3.7.3.2 Test article exposure to LOCA transients may commence only after the autoclave has been cycled through at least one similar transient with coinparable mass. 3.7.4 Procedure 3.7.4.1 Record the test sequence number 3.7.4.2 Record the test article (s) number 3.7.4.3 Stabilize the test articles at 150*F for 2 hours prior to LOCA transient. Do not exceed 20*F/hr rate of change of temperature. 3.7.4.4 Perform the first LOCA transient to the parameters listed in Figure 5. 3.7.4.5 Allow the test article to re-stabilize at 150*F : 10'F for 2 hours. Do not exceed 20'F/hr rate of change of temperature. 3.7.4.6 Perform the second LOCA transient to the parameters listed in Figure 5. 3.7.4.7 Kaman personnel will monitor the test articles during the LOCA tests by performing the evaluation tests listed in paragraph 3.3.3 at every stabilized temperature as follows: 3.7.4.7.1 At 150*F prior to first LOCA transient. 3.7.4.7.2 At 380*F prior to ramping down from first LOCA transient.
'3.7.4.7.3 At 150'F prior to second LOCA transient.
3.7.4.7.4 At 380 F at I hour into the second LOCA transient. 3.7.4.7.5 At 355'F prior to ramping down from second LOCA transient. 3.7.4.7.6 At 335'F prior to ramping down from second LOCA 1 transient. 3.7.4.7.7 At 316*F prior to ramping down from second LOCA transient. 3.7.4.7.8 At 267"F prior to ramping down from second Ls.'A transient. NOTE: Limit rate of change of temperature to 20*F/hr on all transients except the first and second E0CA (increasing temperature) transients. NOTE: Additional evaluation tests may be run at the discretion of the Kaman test engineer.
,e 3.7.4.8 At all times when the test articles are under LOCA testing and not being tested per para. 3.3.4.7 above, the functional test of paragraph 3.3.4 and in particular paragraph
-3.3.4.4.15 shall be perfonned (monitored). .
3.7.5 Report At the conclusion of LOCA tests, the test facility shall provide certification of tests run, articles tested, and the following plots
. 1-which will constitute the final report from the vendor facility:
3.7.5.1 Temperature Versus Time 3.7.5.2 Pressure Versus Time 3.7.5.3 Relative Humidity Versus Time (as appropriate) 3.7.5.4 Application of Spray Versus Time NOTE: The spray solution measurements of content of boric acid and PH shall be recorded prior to circulating the spray and periodically throughout the application of spray. 3.7.6 Records Test data shall be recorded on -data-retrievable media for additional data-reduction, if required, for a period of five years. t 3 i i i 1 i i b ' l i } i L. l
( {- APPENDIX B Deviations Anomalies, and Failure Reports l 460036-002 Appendix B
t Deviations from the general plan and detailed procedures (see Appendix A, Specification 460036-001, Rev. A) were allowed after full evaluation and I approval by the Kaman Qualifications Engineer. Each deviation is noted on a Deviation, Anomalies, and Failures Report. The following Deviations Anomalies, and Failure Reports were processed: DAFR-1 Required photographs to be taken during various phases of the test activity. DAFR-2,5 Added shipping and storage, and operational thermal cycling tests per IEEE-317, to two test articles. DAFR-3,4,6,7,8 Revised or added test article identification and P/N's or S/N's to represent the as-tested components. DAFR-9,10,13 Modified number of torque cycles and torque value to be applied to certain test articles. DAFR-11 Modified TID unifonnity during irradiation. DAFR-12 Allowed dose mapping and time rate dosimetry for TID. DAFR-14 Deleted voltage withstand -test on signal cables for pre-seismic functional test. DAFR-15 Changed sequence of electrical tests. DAFR-16 Required chemical spray to be applied only during non-superheat conditions. DAFR-17 Controlled activities occurring between seismic and LOCA testing. DAFR-18 Deleted one of two evaluation tests required at 380*F LOCA and modified tests applied to signal cables. DAFR-19 Permitted natural cool-down of autoclave after LOCA. t
FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. FAfR- %O0.% ~/ for program 460036-001 check one: quest for deviation from approved plan or procedure O Description of anomalous coadition or occurrence O Report of failure List the document or specification reference paragraph and requirement
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FIGURE 1 l DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. pat =K - b l &pG3C-3 (>',j e b for program 460036-001 check one:
@/ Request for deviation from approved plan or procedure O oescriptioa of ano=aious coaditioa or occurreace .
Report of failure List the document or specification reference paragraph and requirement 1//801(o -DO) EJA >s u 7/ iur ,rs . I r .s
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1 DAFR 460036-2 sh 2 of 3
)
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i Additional tests to perform in order to qualify test article 2.5.3.2 as a ji penetration cable. , I l These tests' should be performed after test sequence 3.1.3. The . test article shall be dismounted from the test platform for these tests. l A. Shipping and storage cycling tests (Ref. IEEE STD 317-1976 para. 6.4.8(1)). I
- 1. Record test sequence number. !
- 2. Record test article number.
i
- 3. Stabilize the test article et room temperature. Cap (P/N 813763-001 or equivalent) the connectors similar to the shipping and storage configuration.
i 4.. In ~an environmental test chamber, increase the test article temperature to > 150'F and minimum relative humidity ($ 15%). l Stabilize for r hour, l i , NOTE: Do not exceed heating / cooling rates of 100 F/hr in this and l subsequent steps. i 5. Increase relative humidity to maximum (> 95%). Stabilize for 1 hour. l 4 j 6. Decrease temperature to g 30"F, maintaining maximum relative humidity (condensationOK). Stabilize for 1 hr. l
~
- 7. Decrease relative humidity to minimum ($ 15%). Stabilize for 1 hr.
- 8. Repeat steps A.4 to A.7 four more times.
- 9. Increase temperature and relative humidity to room ambient conditions.
i 4 Stabilize for 1 hour. l
- 10. Perform the Evaluation tests (only) per the procedure listed in paragraph 3.3. Record data on QDR sheets.
4 4
.-. . .-. - . ._- .- = . . -
l DAFR 460036-2 Sh 3 of 3 B. Thermal cycle test (Ref. IEEE STD 317-1976 para. 6.4.8.(3)). v I'
- 1. Record test sequence number 2 .- - Record test article number.
- 3. Stabilize the test article at room temperature. Cap (P/N 813763-001 or equivalent) the connectors to simulate a mated connection.
- 4. In a temperature-controlled oven, increase the test article temperature to > 150'F. Stabilize for 5 min.
NOTE: Do not exceed heating / cooling rates of 100*F/hr in this and subsequent steps.
- 5. Decrease test article temperature to < 50*F. Stabilize for 5 min.
- 6. Repeat B.4 to B.5 119 more times.
s-
- 7. Increase temperature to room ambient conditions.
- 8. Perform the Evaluation tests (only) per the procedure listed in paragraph 3.3 Record data on QDR sheets.
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FIGURE 1 i DEVIATIONS, ANOMALIES, AND FAILURE REPORT ' Sequence No. D AFit L4(,00.76, I for program 460036-001
\
j check one: 1 i Request for deviation from approved plan or procedure ' [ Description of anomalous condition or occurrence [ Report of failure List the document or specification reference paragraph and requirement
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FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. AfC,003(,- 9 for program 450036-001
; check one:
R Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence [ Report of failure List the document or specification reference paragraph and requirement B A c R - u c co 2 L -3
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, DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. 44663&,-6 for program 460036-001 ;
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. E , Date ni %.ul M l
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1 l 1 FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. 4/bo0 A .l , for program 460036-001 f
; check one:
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DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. 4/4,003(, - 9 for program 460036-001 t
; check one:
K Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence [ Report of failure List the document or specification reference paragraph and requirement DAPd L4I, oo.1 (,-3 ; p c <> _ s . 3 Describe the Deviation, Anomaly, or Failure cL a l l ,_ d ec er*i b e l-ni a es: 0. 2. 5',1. i. it w h s, W/ k1 8 ar 2 "5 /,4 - i'2.4 - d.c.o x. i T,l hi MtC,ot-01 Name Om,ea i-9 Emr Date tc. Te.olgic 1 l Reconnended Dipsition Tke- c m (eI ,
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f - l FIGURE I DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. %803(a - 8 for program 460036-001
; check one:
X Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence l [ Report of failure List the document or specification reference paragraph and requirement'" 4 (eo o 3(a -<b o i re_v A '.' car 1. f.3 uA DAFT 466o2 L-3 ti Describe the Deviation, Anomaly, or failure e c_ edib wa A ars
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s FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT WooJ6-? Sequence No. for program 460036-001
; check one: !
Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence [ Report of failure List the document or specification reference paragraph and requirement ' H t- O O 3 L - c o 1 sA.e d k pc ra ~5 l 41 Arm 7 'l 3 n &7 an.epyk 3. + 3, ~5 aJ 3v3.t 'ru.i( ' ' i Describe the Deviation Anomaly, or Failure M eV'ta o* hva k Tr a d a. ca.a d er am d VistJ%s_ - et' am A emb la i S l ea Lmw cAn L a.w
% u[o 21 L1 14 td4 s
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f FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT 4toco w -10 Sequence No. for program 460036-001 t
, check one:
% Request for deviation from approved plan or procedure
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/ _ Report of failure List the document or specification reference paragraph and'Mquirement "'" a.4 t. o o 2 G,- 0 0 s LA nn -nsL 3. I . U n., n T J. T
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FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. [l/Z. Y/ # 8 [ - // for program 460036-001
, check one:
h Request for deviation from approved plan or procedure O oescription of anomalous coadition or occurrence . O Report of failure List the document or sppcification reference paragraph and requirement U$DD1(a -M / Pav A. par,e 3.5.z.I *
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p . 2 d E t 4 re f. L J_,G & ... " "..."7cank% n ac u llu J J h y.r... " Describe the Deviation, Anomaly, or Failuree 17 vada d del/.*/ cauu d d . J ain u,Cordo % rmi .s-a+ - > .23 ta$ uv ( k- J #d r*u larr~onf '/as s%.rn /s he m:Armenn.: I s Name?)ll/ Date Ib/2, z,/gf. Reconmended Dis osition 1)eydose eM/sy M mo/ /sse fd44 #EF dd,[ ash _ad con er/ULk'es % v ot more Au m ir M:A As->a.- wi -s.. , ~ . a ; - - u_ L2.+r es P-_^=(s), rop n,t e
/ w ole k J uAfL.. 7 <a/auJae Javi if r las ' im +ia- age; ed
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.I ' g')l Approved Disposition R o r_ , m ,,m s,.s z/ .- -,, g / , ,,,, f,. , ,, , ,. ,, v, ,4 n
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FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT l Sequence No. // [ d //4 S B J d - /4R for program 460036-001 k I
, check one:
@ Request for deviation from approved plan or procedure O Description of anomalous condition or occurrence ,,
O Report of failure 1.ist wou the - document A+ ); y ,9 oo r & v or w s. r. v.reference A- specification J .a J AJ1 ' YID .
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FIGURE 1 DEVIATIONS, AN0MAllE3, AND FAILURE REPORT l Sequence I 80,b - / 3 for program 460036-001 l
; check one:
@ Request for deviation from approved plan or procedure
[ Description of anomalous condition or occurrence [ Report of failum R,no List theu document
-Det 40Aor, specification Anru. 7. V.1 reference a d 7. 4.paragrap 7.
%rous value ic 2 rf+1 L Describe the Deviation, Anomaly, or Failure pm A),/ 4 /esw, e, b esn> aalo s '~
s Name l'/ Y . Date_/s,)z y, a... , , fY Recomended Disposition
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QA 81 W ' Date /8 8
f FIGURE I DEVIATIONS, ANOMALIES, AND FAILURE REPORT
} Sequence No. '/6 db-/ Y for program 460036-001 4
; check one:
K Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence [ Report of failurr List the document or specification reference paragraph and req 0irement 4fo o O % - O O L Ae_a A se.cA n~o-, 3. 3. 3. 4 Anomaly or Failure L \lallane-Describe theUDeviation
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,su/ date (, A[/8c/
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FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. '/@M ~ /I for program 460036-001 ; l i i
; check one:
1 K Request for deviation from approved plan or procedure [ Description of anomalous condition or occurrence [ Report of failure List the document or specification reference paragraph and requirement 4(s00%~ OO 1 Rev A Se.c. 3.3 i 1 1 Des ber the Ic.,Deviation,
,./ Jarf A0omab,l orlow Failure ( h e a e Yo / c c e.
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FIGURE I DEVIATIONS, ANOMALIES, AND FAILURE REPORT I Sequence No. Pkfx tyggg-((p for program 460036-001
,' check one:
@ Request for deviation from approved plan or procedure
/ O oescription of anomalous coadition or occurreace O Report of failure List the document or specification reference paragraph and requi fement IMnn TC ~ool Es sA FM f- C Lin vis e sta nk a f ~ Sb.rt + 3c> <re J M u,a-- 47 4 y/Ana rz Describe the Deviation, Anomal , or Failure ch, ura v ese // auc a c L & < u r e rL du e ins frH /- d llc of 4.,f
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FIGURE 1 DEVIATIONS, AN0MALIES, AND FAILURE REPORT Sequence No. f60035-/7 for program 460036-001 i l i
, check one:
O Request for deviation from approved plan or procedure
@ Description of anomalous condition or occurrence ,,
O Report of failure X List the document or specification reference paragraph and requirement g,,p h'cc3&-colvon..,, c,n tr< h d fea A ra n 3. t. 9 14< 3 t . if
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s,, eni er kre 4 J a W h. ' n,6 erkrie Name hW'/l5 Date i/b F Y i t i l Recomended Disposition $p <f/d,2, ra d
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Approved W h Date f/A,Anf QAh3/ LauL Date er//n d4 Qualification Engineer # '/
I n' K man [1]l/ ' nnEna12s I in:trum4nt si a CALCULATION SHEET \ a r ; ~-"" CALC. NO 0 SIGNATURE N'M DATE // E!Y/ CHECKED kN DATE 2 M /fi'5 PROJECT Nud 5 ( JOB NO. NO[ SUBJECT NM [6CX - / 7 SHEET / OF SHEETS 1 5 f/.S6fI f5
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- 32 Mc, l cland;A /;r du c~~A is L,><
a va c uu- ha b ad procdun- wh el d< ep-c o n c (n , i, kaled k (- ika vacu ~ s cf >p3jf. 4plyry rl.neo y praes 4,ym)y c < fo tL- /es/ ecwe
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a 888#,on CALCULATION SHEET
- SIGNATURE DATE // /1 El CHECKED III A d /AS' PROJECT M[ C N/ N k JOB NO. @
SUBJECT 9 d- NddO3d - /7 SHEET d OF 3 SHEETS 1 I huftouc/ tbvaluof.Z*iE J se<>< Sa(Ser"lf cuerd tc>
- froceed w,Y) .uksm.c hd a y <a Ab ,4a-.-f ca& a fica // )J one cal /< w A-looso faal conea)vc. Tha c e.,< u ake w a.r hea/-ect u,8 a 6 [g w [*, ), ( &g ) y,/ g)3, ,,
7 pa y p). }c g,l} ,(, ) g4l y, f p a comber wa~ 1.<syni4 J fo k /o o s e , 4<atif o)u .c deud<} s prec<e/ ws/L c<<r>~ie 4.949,. "JA.el C em/sild bsegasu/ ks< na/s
" wasl
,s/i} i dr"cc<ssi ac d d a paus /h e ur o v< s h.<, msdf%,
ta gad 13 rk fest er qua l csr,uckes. W .pserapha /Jaks_,guea7I & covey dehu A v, 7L P.d a< hcl.a usor< drop .sb ft ed n kz may u[a eh revp (.. <./:h ur p< Co/ornJc,,T7e 4, wA, A 17 ff.p. p g-l gg },j g, f,l ,g 18 f~g , j f)f;,, & y yM g (p.,y g ,,,), g, * (<. gross isuprovan,, t jn e(ec} race,/ e darac h r,s A e c-ba.} h// ed of /c 0 <cfed
' f valu < c - Tic- Nur (oa c- <r cabl<> war e 4ycen,uded fecnu fd-e fe>f &k;) r~d pfaes} i., a profu cha oa euw bafe -od ove,t o ve r y.p t.y at //fo f a Wp,' . d Im cWbw a te pfacs / i:, a a laj u cuan hd-e o d ovex af jfo *'S J 7.3*f . TE" temauty < 14r vie r-t left in k oa flw fe.rt dicl o- s/ As fesf wecJaccy (onl ) )W vacaun kkJ for L L(ou o t > aco c -
l [or Jws~M n"/becE<c c - ) All l>ehte7aalfada disarm }/ cornk 3*
%qu< Jpr valw> (w L-)-hp (su la r kb au) k I8-3Y ff f(ma
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hq! " " " ' nSN,"m t:rira CALCULATION SHEET au~; ~~ ( SIGNATURE > DATE I lJ CHECKED 8 DATE 2/d /8 5 l eno;ECT t-@ A N 8 +.[ M 30B No. &# SUBJECT NEE Y[CO7d / 7 SHEET 3 OF 3 SHEETS 1 I (Bh M& l ic wkF lit g///' c (YA o.u ac$s'4' u.>, r zt. h eryn./ffcc/[s T Ate krque6.,rbcouebef,,Jacm,s1.ju L fk/ s ccan4, a aa - n u t -s a&/ 4 & lod tL coes<c'kr sat i~ t h A kr "< - vd"k < ! 7 Jo [ gy a /,g f 9"[ * , j/, ' g &
- wkrs u>;M a ja -~/ rwer< /orpe yf b )
at aoo i.,JL rest,;,. of
~An of forgue af % va u,;
kes on a sc/c<ra0*4 r2$acm centue tu fre iAy " & e/'rs, re-kreaarh /tyunA)
,1 rerarf.,kM ex/< cadcEe I lo <s Ldn l,' t oc s , if nc<s/y .
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hermific see/ tanfocke,l puf5 on fb ym//.h.hL c>,uai4rr A,y ea v sss a-fu h h r prz>t,N f u y fo akr rG cs>,uAr k kr/;; ce ,. p vacun cm. An.yiy _ out rLu e chs,~ d, e es,a ucht 14 s J,, if u,J ), n ,
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xi.snoi23 K mcd.as: sir..a ia scum y........... CALCULATION SHEET CALC. NO - SIGNATURE Nb DATE // 2 I/ CHECKED /II DATE i (
-I 1 PROJECT KDT - sooo/M r Cable Qual:T:c adron Joe NO. YW)'
SUBJECT DAFR 460036-/7 SHEET f OF k SHEETS 1 t
^
OISC MSS ton oH "A PPR O VE D D ss Pos a rioN 3 l 2 4
/. O SUMMA RY of THE PRO 6usMs CNcoMMTCRCD l 5 '
/* l Some Tns u /a fien Res s+ance C TR) , noise cucrenf, l en d , " keep nirve " readings were n e er ee o u +s Ms the re r es p e e +s1e a cc ep fa n ee cr i fe rso n .
- I 10
/. 1 Som e c o n n e e + ors esh:bi-fed a rela ga + /en From +h eir in*+;al forg u e .
12
' 2.0 of Dis c ussion T// E PROBLEMS E N CoHH TE RK O 14 2.1 Rea 'ng s Near or du fs/de Their Re spec +/ve 16 A ccep fan c e CrI+ era ~en 17
- Tt has been observed tha f IR reading s on a given sp ecim en tend +o degrade iF a conncefor ( or bare cortdaefers on a. s e a le d c able end) is le. Ff exposed to motsfuee and impuer +/e c in the air . It is very drFlic ulf to , lies f of a ll, a++er n an d , second/y , fo '
main fain art ER r= .= ding 'o P . Io" ohms. En las-f when the um bien / humid:fy is kryh or th ere aes a ht o f imp uritie s in /k e air , m eg okm - 1 28 m elee r e a d *ng s os have been o bse r ved fo re ma. tn b elo w /0 ohms w i th +4 c. le a ds no+ conn ec +ed to any +hing . In o f/ree w ords, the l an ors fu r e- an d imp s<esfies in Hr e e re place an 31 upyee bound on th e TR +h a f ca rt be nu easure d Ter a n orma l a m bien f e n viro n m e n t . Th e loss in ER in a spe cim e.n Is a vin g en e wpore of 3" co+s n ec for (or exposed con du e / orc) is be/reva d
- fo be due permact ly to deposifron eF 36
I ya K mcn // xi.swai23 [' instrum. g , ..e..n..t
.... rir..a CALCULATION SHEET CALC. NO SIGNATURE b DATE // CHECKED /41 DATF 2 4 M PROJECT MDT-/ooo/MT C,k/s db I,* f, ca / o,. JOB NO- ~
SUBJECT DAFE 4/6ooJ56 - 17 SHEET 2 OF Y SHEETS 1 r an o is + u t e and 1.npurifie s from th e are o n fo lhe suePaeas of f4e in,rula +oes. The in;+tal 5 ER can he recoverect Co F+en complefe/y) by heaf:n3 and/ or apply io.g a vacuum to re m ove m ois fuee and Imp uer+;es fro.- these in s u le +,e surVaces. 9 If has als o been o bser ved th a + h1 I 10 cable. sp e cim en s h aving lo w XR re adin g s o Nen have hig h n ois e c u e r e a, + e e adings as we ll. This is be). e ved +, be due fa a charg e build up in the con +am in a,, +s on the i sn/e /or
' sue Faces . T4:s c h a, g e is 6- tra ved /o 6-caused by fA e bry k v o / fay e tha / is applich fo the sp ecimen by th e mey ehm m e fer during rR measure m en fs - TA e- s yn P this s fore d charge has beer, o bs erved to be reversible C in exp erim en is conduc /ect by Kamen ) by 20 crpply ing FA e 4:34 vol fay a y o fen fre/ :n th e
*pposite da rec + ton .
22 4 h ry h , n eg a f;v e n o rt e- c u rr~ e n + in 23 + n a Synel Cable w it/ eause +4 c keep a/:ve 24 lo w i 2s reading to be o r- even n e g a fiv e , l 2s wh;/* a h ig h > p oss-five as o rre currenf :n l a- Signal ca ble will cause the . keep a /;ve .. 1 27 (*- a d ing to be too h ry h . 2e Thus, T+ is ex -fre m ely i-y-e fa., t fa keep all conneefors clean an d e/ry . 30
' Relax a +io,,
2.1 From In:tral Torgue 32 1 l Relaxa fton Seem #A e in ,- +:a l forg ue
" l was observeof in. so m e vnafed con n e e + ors .
Th is apparen +/y a llo wed morgfure From the 36 l
i o p/ NICN / KI-ENG123
- scum.,e..nt:ri.m.a y~' . . . . . . . CALCULATION SHEET CALC. NO SIGNATURE b DATE // 9 IN CHECKED DATE f 3 PROJECT KDI-/soo/MT Ca6/c 6aa/IMc o //o., JOB NO. b SUBJECT D A F'E 8/6 00 74 - / r SHEET 7 OF h SHEETS i
1 2 l Sur round:ng air +o en+ee the co n n ec +or volume. l E videnc e of moisfare con fa mina / ton I,, s.*de j 5 1 conn ec +oes can be o b fa rn ed by h aa fing l the- m a fed c-o nn e e foes wr/h e. hcaf gun i 7 observing th e- ZR r s adin gs on fhe vv h ;le
- l subjeef spec
- men . A slable ER re ading In dicales l 9
no m o is +ure ls ne s en f ered llt e C
- n n e c /**~
volu me , wh /e a- signi V,'c an f e.),ang e [usua,lp an Impeeve men & :n th e IR r eading upon ham.+.ng Ic indica //ve of m e is /ure con Ar ,ina f *en . D uring fhe Pre - Saismie alcelere al fes/s, th e re was ev dene e oF m o ts +ur e confamin a /;o n 16 and forgue r elax e ft on in th e con n ee +ae on Signa / Ca ble 76601-oz onaled to 1C /A/6 2'l . Th e co nn ee foe w .e s lo osen ed sliyh //y , heaf was a y y tt e d +o drive auf th e m o ts +ur e , end ih cn 19 th e con n ecfor was r e -feef ue d. Su b s ag u e., + re ading s on +4 .*r cable were well wi//,in /4 e a cceptenee 21 c ei f e rio n. The //V con a ec }or -fo E C- I'l6 L'l and 23 bo/A th e // v and Sig n e/ e-on n ea +oes fa 24
'L c 117/o were obseeved +o have res: dual fo ey ues oP /e ss f4aa M PJ - Ibs in /A e 26 Pos/- Seiso,,tc ae+iv;/tes y er Poe,n cd by KL 27 in Co forado Sp, ,r,.y s . 74e tory u er o n. /se ;
m ale - Se male cons, ee for p are, th e Se male co n s,ec foe s f u b , a nct fhe male con n ecfor sfub were checked af 29 Ff-Ibs ; ,; e. . th e se. c o n n ec + ors 31 had main falned p e oper 'forg ue . Fuether, th e<a 3* l was no e videne e eV m eisfuee con fa min , ,tro n 33 in side them. 34 35 l 36 l
- K man /t g/-/ nr.txo123
( Ya srum. .e> n..t:se...a 3 . . ,
. . . . CALCULATION SHEET CALC. NO SIGNATURE b DATE 1/kf i CHECKED //d DATF st c_ PROJECT )<D T - looo/M I Cable Cua/t f.*fc //en JOB NO. b OI SUBJECT DAF2 44roo36 -17 SHEET M OF SHEETS 1
2
- 3. 0 - RA T/o stA L.C FOR THE A PPROVLD DIS POSI T/0N 4
3.1 Tes / - In +erhce Conn ec foes 6 l The fesf- in fae lac e c o n n ec tors aee those { co n n ee+oes on -f A e ends of th e M1 cable 9 Spe c imens +o wh ;eh th e tes f le ad.s (ee Flexible trias c.akles) are a++. eked. These 11 con n ec +oes ace ne+ con sidered +o be fe s + ar ficie s and ws// be lo ca fed ou + side fAe a ufo - clave dueing fk e Loc 4 fe s f. Caps were pleee d on 4kese c onn ec4oes a+ +h e s+e+ of +he fest ac tivi +y and aen norma //y kep t in p l ace. j ~ // owe ver, +h e se cafes anus + be ce m oved af 17
;, , 4,. , pp, , y,, p ,, , g, yee Forming evalua fr n and G nc+ tonal f es fs .
Th ere fore , +4ese con n ecfors are guifs suscey /Ible to c on fa,.,in a /to,r by m oo's f a r e ene{ impu rifie s Te a m th e s ue e o un ding air. Si>,c e +hese connee+oes ace no+ fes+ arfic les , henf and/or vacuum snay be ayy /ted 24 as necessmey th ro uyk e u + the fes+ seyue nce fo 2' eer sur e +k a + /A a.s e conn e e fees are clean and ( a r e- no+ +ke source eV any observed significanf . IR deg rada +io n andfor see ce ssive naise ; 2e ee ading s . 29 3* 31 Bare Cable Ends one M1 c able spec:m en c.corsis +s oF 3 ' ~ a cable loop wi th s ealed bu+ ex posed conduc fors on each end ( i. e . +4 /s cable does no+ h a ve c on n ec +oes on +he e nds). 74ese bare c able ends will also ha loca +ad 36
]
lf
#F3D /[/ KI-ENG123 2trJm.
'n ' .e..n..t:ss.ea
... ... CALCULATION SHEET CALC. NO SIGNATURE Yb DATE Il 74 CHECKED DATF [ [ q PROJECT K D T - /Ooo/ M T doble A. // free //en JOB NO. N#[
SUBJECT DAFR 4/4oo n-/> SHEET 6 OF f SHEETSf 1 2 oufside +he aulo clave d u ring -lh e LocA fes+. 4 E ven though e p la s f re o r- me la / c- ay may be pro vida d to .1/rp over /Ju e se ends , if l ws/l be im yass;6le /a pra ven+ s, m e mots fu . con +aa.,in a //en oF fh e seals. rs,a re for e, hea+ \ no d/or va c u u on an ay he ayylied lo lhese cable l 9 an ds as n ec e ssary- throughouf lhe fes/ segue.sc e fa en sure tha+ /A ere s eals are clean and are no+ lh e source of ay observed significa f 1R degrade fron a.,d f.e ex e c .rsive n oise , re ad:ngs. 14 "S. 3 De+ec foe - In leefac e Connec+ ors 16 Operab;/rfy o f+ th e son cham ber- de fcc +,es is e ay u ired dur:ng +A e sim u la fed LocA even+. ll owe v e r , th ere was e viden c e of snois /urs con fem in a fio n in side +Ae de fec for -in ferEnce
- 21 c on n ee for-s dueing the Fest- Sei
- mic e valu a fron i 22 oc +;v:+y . Th :s mois+uee c.aused a redue lion in 23 1R an d an in crease in th e n ois e currenf ,
24 l Sin e e lo w rR e d/-r 4 ty A noise eu cran + may in h ihil a.ecurale r eadings of /k e
- keep i alive " signal fro m th e defeaforsiif was decided tha f 4he mois fure should be re mo ve d
, Erem th ese con ne c +ces before th e LocA tes t. TA:s onay ba a ee omylished a sing h*<f a d/-e vac u u m a+ +h is y. in f in tA c +cs4 seg u enc e in order -/. res/ ore f4 e ele e fetcal preparties l aF fAese eann ec1.es f. f4er.- in:+;a/ va /u a s . I Th e- cause of +4 e. m isfure con + amin f.-n in these connee),,, y, he j;e ved ), f, dua to a refa wa +/en in the in i+ia l for g u e , slnce 1 36
K mro// y v' xi.sno123 (- 7arernme/ t....z... m ..n.. ri a CALCULATION SHEET CALC. NO , SIGNATURE b-DATE ll, 7_ 4, h CHECKED /d DATF 27 - g PROJECT KD 1 - lo co/ M 1 Ca Lla Q u a l:T:c Jron JOB nO. 2GF SUBJECT _ DA FR L/4 oo f4 - 17 SHEET 6 OF Y SHEETS 1 2 r elaoca +/en was observed on all +A e detee for - in fer face co nn ee + oes . This rela,ca fron in foey u e
- Is belie ved to have e e su lled in an inadey ue/c seal by fhe 0- ring th ereby allowing a small amoun + of snors/ure From /k e surroun ding a ro-
- ee nn e c +o,-
I fo en fer +h e vo lu m e . 4 Flee re mova l 9 of 4h e. ,nors/ure , these con n ec foes are fo Lee
! 10 torguad +o 35 TJ- Ibs ye/or fo /A e LocA te s +.
Sin es ,,,,;s +u ,.e has appere,, ft, in f:// rated lhes e so n n e e /oes , /4 e in /eyrify eF th e frapped
' 6ee n vo lu ,,, a has alr eady some wk + canpren ts e d.
r+ s ill be c o ny, le f.I, c o,,,y romised if +hese conn e efers are unc onyled f.e re m-va l of the 16 m ois fure . Ilo w e v ee , th e M-F conn e e for fair > discu ss ed in e sec tio n 1. 4 , :s f. 6e le FI mafed an d tryh f. Sin c e th ere is no e vidence of 19 mois+ure con famina f ton in fh is connec/ou- pere of 20 Yh ES yoin f in th e fes/ seg u ence , /his con n ec loe 21 y' air wlIl serve fo de m on s fra f e wh e /A er ce not 22 th e +rappe d volu m e a d if s inferae+;en wi/h th e in sula fee and seel oneferials is sen sifive +. 24 Ir ca dia fron . 25 3.il M-f co n n e e foe Pe te , l~- Co nn ee +.e s tu b, M- con n e e +ce sfah 2s Th e se co n n e c for s are tes + spe c Em en s 3* tha / will be in side th e- au foelav e during
' ih e LocA +e s + . Th e male - female ( M-f) ;
3 connec+or pair is to r e ma in enafed an d i fig k + . Sin,;/aely a the Vemale con n ector sfu b is +o re mein c-apped and f,yh f and the male c o n n e c +* r- ,s fu b is to re ene in plugged ana fig h +. as
K med!e a CALCULATION SHEET xi.zNoi23 1 Ta: scum. y , .... f..n..s:ssr... CALC. NO SIGNATURE Y A so- DATE (/7 O CHECKED DATF , PROJECT K D r- /doo/MT Cable du a/t f.'cn /,*= ~ JOB NO. NOI SUBJECT DA FR 4400 % -/7 SHEET '7 OF SHEETS 1 2 l Sven though th ers has been some elegrade fron . in 1R on som e of these sp ec ts e ns , th e rK 5 has ce ,n ain e d a bov e lh e aconyfence criferson . l
- Th ese con n e c + ors are no+ fa be /oosened and/oe subje a +ed to haaf or vacuum for r e m oval of any sn oistu re thaf s =y have en tered the frapp ed 9
volu m e . By /* a vin g th ese conn ec fors in + = c + > th es-can he used to de ferm in e iF lhere are a y. dele ferrous e TVecLe oV irradia fran on th e frapp ed volu me an d i ts in +erac +/en wifh th e insula +or a d 13 seal ma fe r rals . 14 15 3.5 Tory a e Valu e s 16
' for th e Two explan a fton s observed relawa+ ion '
- in forg u e, are : (t) /oosent y oF th e con n eefoe nu+s due to vibra fron and/or in su F Vse ten + Teic fr..,
befween the ma fing th r eads a,, d (2.) ,,,a +er ia l ,
*' j relaxa fron ce pla sfre Flo w , or+ likely +o be j o ccuretny in +4e o ring . A r e m edy F- - the Firs t case is +o add ja , - n u +s to th e fo +h e co ,, n e efor s to peeven/ /he o,n+s from
/oose*,ing . This ws// be Jane +, th e de fee for -
26 fo< f or fac e co*tn e c tors dur ir.3 f4e Fes+- Seis ,rc
- af Colo rado sye ings .
ac-fivify Som e a.ddi-/,'on a l dafa was ob farned by 2* Yaman whic h s u pyo ris f4e s econd e><r lan af fon s
- i. e - tha f- ma f erial yalaeaf,*on is oce u e e ing . Th e dafa shows tha t in sev eral cases a- c on n ee+ar-was fig h +e ed fa a. known to eg u e. va fu e . when if w as rech ecked abou+ 50 m in u +es la +ee ,
3" +h e re ridual -fo rg ac we.s sign T Vie an+/y lowe e al though +he naf had no+ ro+= fed. A ee view ! 36
\
ES#FFCff/ W KI-ENG123 L l
#a:trum.,,e..a..r ..
3~ ' t.i.o.n. CALCULATION SHEET
, CALC NO SIGNATURE -- Nb DATE //g 2f i
I'l CHECKED DATE 1j-- I PROJECT )< D T - 1ooo/ MT Cable Cum 1/ I.*c a //ma JOB NO. NOI SU6 JECT D A FJ2 6 ooE -17 SHEET A OF f SHEETS 1 2 oT +he 0 - ring anenu Fac furer's li /e va fuee in dica le s
+ka+ the 0 ring should undergo p lac +ic de for ma-
- n order +o p ro vide a pr oper s eal. Fur +her -
+;o n m or e, +he rec omm ended co mp r e ssion o f fhe 0-ro'ng should be con 1r o lle d by th e day +h of a gecove m a c h in eef in +o one *f /he maling sur Peces.
9 The o r ing :s pla cad in +. /his groove ea 10 fh e m +ing surfaces are brougAf foge/ hee i c omp r essing /he 0 r ing in th e pr oc e ss. Kaman has provided }h e r e co m m e n ded groove in fhe sn a.fing surPace oP IAe m ale co n n ec +-e s . Te-sf.s y ae Form ed by K=ma n duein y /Ae Pos t- Se ismic a e +;vi+re s a+ i+.1 Colorado Sy ria,9,
' ~
Tse ilify indicafe ih a + +he o e ig in a//y s yecifled
' of 19 F4 ~ Ibs an ay be jusf rh er / of
'forg u e full con +,c+ o f th e lha f re utred to a f fain 19 m a fin g surPaces of fh e conn e c / ors. h il 20 a f f a rn e d a. / fo r ues
' of con fa c + was 21 -'
'so - sf F+ - Ss . TheeeVere, all conn ec +oes 22 (fes+ Sp ec im ens on ly ) are fo be fo rgu e d lo 23 55 F4 - Ibs p rior to lh e tocA fes f. j 24 25 26 27 28 29 30 31 4
32 1 1 33 34 35 36 t I
K mrhild / CALCULATION SHEET KI-ENG123 j strum. y~ ~,,e..n..ta..rs.e..a
' CALC.NO SIGNATURE W C DATE / 24 FV CHECKED b DATF Zl ,4 3 PROJECT KO T-loco /M T CaLlo Q u o I: Dea f ron JOB NO. dWf SUBJECT DAfR dM00 36 - 17 SHEET 9 OF Y SHEETS 1
2 l 3 To ou rs rA blD Ibla ISS u ts 4
- Th e Tollowing issaes m as + be a ddresse d and
- re solved in su bsey uan + acf:vi+y : (
7
- forgue
/) Final de fermin a +/on oF +h e reyureed (or ma ling th e co n nec + ors . h'e su l+s from j 10
+he LocA fes+ and any a ddr //anel fes /s
" perSoemed by Kaman should be used in 12 m aKing +h ir de f erm o~na +/on. Re vise the
' 1nsfa//e fron Proc edu ee a c c ording1 y .
l
.14
- 2) De fe r m :n e TF jam -n u +s are r eyuired to preven + lh e co n n e c + ors Fr o m Joasening . if so,
' a ddre ss se ism ic gualifica +/on and r e vise '* In s +a lla+;on Pro c edu re .
19 j 0
$ Wedo +h e full - forg ue m e.chan ical aging ;F
' th e grea+er +han r eg u ired forgu e is 19 F/- Ib s.
23 ] LI) Rev:se in s +a lla + ion Pro cedure tw ensnee j tha f ma +ed co n n e e + ors are clean a nc/ \ 2s d ry . 27 28 29 [63T - SCEIPT
- QFER. To Opo% -oN 30 Af fevelix [
31 1? 33 34 35 36 l
FIGURE 1 l DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. l/ g o 4 % - I t' for program 460036-001 i
, check one:
@ Request for deviation from approved plan or procedure O oescription of anomaious condition or occurrence O Report of failure List the document or specification reference paragraph and requirement w oou.-oor tw A r cr , . ,. no . ,. <I- e alud. ( ./. - D / rA
+ sso f s oa ,& '7. ,. o. r. r a >. 4,-w & L a 1.s a.t ssr ,c Describe the Deviation, Anomaly, or Failure A l/c 22.7/o_ reewy[ /e r e n d eE u. - - = M P4eie d e r E.st. )her a Nt45 femmes #iflaarw/a d mar / "s a ea A L LaL4s is. r. 4. ~r. s - Lah L > L w 'k rUr ik .'
Ah.,e.n..-A- 4e kla4e a II k.L kn A L aba* A J.cah af
,om 11 r.n .r, s .
Name MI - I) ate ,/ .//[PA Recomended Disposition Fo d ,,rdro < = L ,,l , k /s. 4 a . d/e, Or //c u ve o alar L. 3.7. 4. r. 4 h stover,+ foir'ns rLe k.s . r cearatuk< 2,e;ma +Aa Q'gi fe ,p aru fu- . On n,'t s-o-f. ma ;v JJ 1 Cs. L J.*e a}'Asa h a omo 1.., .o. r. r a.s ' i+ ir reu.helb rela 2J k 7.7 V.7 A i Na
'V "
$ Da'.e // // 31 b b Approved Disposition 'h a _. . ,, d,o/ n , ,,,,.; #, ,, " r, ,,,,.,v s, ua4s - n. a ~ W., a o n i:<a "
.- a a 1:n 3 wa, e o +: , a - a s 1,:
e o e --2, 2 +1, e An- 1 + 1, - 21:s s. ra m o. e <e arn , o n . l Approved 4/h Qualification Engineer Date ///2,Aiv QA k[I/dimi " Date /z/ro /N' (f / / l
1 I ( FIGURE 1 DEVIATIONS, ANOMALIES, AND FAILURE REPORT Sequence No. Yh OO)b ~ N for program 6 4_60036-001
, check one:
$ Request for deviation from approved plan or procedure Q Description of anomalous condition or occurrence ,
O Report of failure List the document or specification reference paragraph arid requt_rerpent e il t, 0 0 % - o d / M A 9sm *s.7 4 7. s Alete > ht et cL9 -f +a,up Iow*.1 'e's -- 2 o *rA - Describe the Deviation,/ or Failure /0 7've - .15RO*fM. d) Reoueaf cao b w nAnomaly,a kr mr *r' ' a t m. L 1 l r- a h ' / i u s t- kee aCf <Aaa ~ e=d is f L oveA t_L: - L ac-urnidhD n L a L L-1 J. - ;,s A M y -
/
Name Y_ _Y.Y_ ,Date //fzo,)yf Rec p nded Disposition Coe[dMA - a f h m. f4 fe< f. /dY
- o-L Lt w;Hi uis -u.- a.w n. 1o-sr ,w.wg . .,
2 - A.. eaoah:Ap'J ted wNe/u' ta, su russa w p ery Name $,./))'
. ,Date II/ ,
gy I l l Approved Disposition "g,,om ,,, sed n . < g ,y r /<,,,, , s acor ave s . 7- - n a, s 1,. - - v e. +sa e 2,~. - c on /2- -
<Lall I, a en , L' a o u v su e -- ~Jc J. ~ri. i ,a/ . - - J:s oF
,., e_ Ja t aa,- h wnl - a c-,- de d fe ,,, o er a +w er.
13 rL a I Approved 9/ & n Date uhe/a4 4 8l ,La~.1 ,Date n k h v Qualification Engineer t/
~
/ /'
t
f-APPENDIX C Detector Calibration Procedure (KNP-18-104) and Supporting Data Sheets i 460036-002 Appendix C t ,_ _ . . . . _ , . , . _ - - - - - --,-
DgcunaENT mur no.
~
Koman instrumenterien corporati** STANDARD PRACTICE PROCEDURE f REv. PAGE I OF14 A DOCUMENT TITLE DATE ISSUED d_11_RA PREPAREDSY KDI-1000 FACTORY CALIBRATION ~ J. Miller DATE REVISED REV: A ORIG /NAL /SSUE PER ECO 28509 i t i APPROVED BY: ENGINEERING OUALITY ASSURANCE TEST N Y N , ~)f? YN ~$N DATE / DATE y DATE
( i DOCUMENT KNPNO. Jenseman insewsseentesfon %dio" 18-104 - STANDARD PRACTICE PROCEDURE aev, PAGE 2 OF14 A TABLE OF CONTENTS l
\
SECTION TITLE PAGE l 1 l l 1.0 SCOPE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
2.0 REFERENCES
3
\
l 3.0 QA NOTIFICATION . . . . . . . . . . . . . . . . . . . . . . . . . 3 4.0 REQUIREMENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . 3 5.0 TEST EQ U I PMENT. . . . . . . . . . . . . . . . . . . . . . . . . . 4
6.0 DESCRIPTION
OF FACILITY . . . . . . . . . . . . . . . . . . . . . 5 7.0 GENERAL PROCEDURAL DESCRIPTION. . . . . . . . . . . . . . . . . . 5 8.0 SOURCE OPERATION. . . . . . . . . . . . . . . . . . . . . . . . . 6 I 9.0 PROCEDURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 10.0 DATA SHEET. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,4 l
, _ _ _ , - . , . - . _ ~ , _ . _ _ . . _ - . , .
l
i DOCUMENT KNP NO. g,,,,, e w.,.na.. carpemede* 18-104 - STANDARD PRACTICE PROCEDURE REV. raos 3 or14 A 1.0 SCOPE This procedure covers the method by which KI Model KDI-1000 (P/N 824636) ion chamber detectors will be calibrated at Penrose Hospital, Colorado Springs, using the 1400 curie Picker Model 400 cesium - 137 teletherapy source. l These will be Primary Calibrations, traceable to NBS.
2.0 REFERENCES
2.1 KIC/Penrose Source, Equipment and Agreement File 2.2 Laboratory Notebook "Penrose Facility" 2.3 Instrumentation Instruction Manuals 2.4 KNP 30-3 3.0 QA NOTIFICATION Quality Assurance will be notified before starting this procedure. QA will perform surveillance on a timely basis. Verification, when required, shall be shown on the test record by the date and the inspector's initials or stamp. Only operators certified by Systems Test are permitted to implement the calibration procedures of this KNP. 4.0 REQUIREMENTS 4.1 General When using the source, always remember that this is a highly radioactive source, and all operating and safety procedures established by KI and Penrose Hospital should be followed with care. Wear your KI film badge at all times. Expedite activities in the Calibration Room, especially around the source. Minimize source "0N" time when taking readings. mas.,a -
, ,,,+,w- ,,,.,,,,,m- , ,.. ---- -, ---n-.. ,, ,.c-
DOCUMENT KN9NO. h# W STANDARD PRACTICE PROCEDURE ev, PAGE 4 OF14 A l 4.2 Record Keeping , Record all data on the data sheets contained in this KNP. 4.3 All electronic equipment used to set or record test parameters must be in the KI QA instrument calibration program and must be in current calibration. l 5.0 TEST EQUIPMENT , l 5.1 Ion chamber Readout: Keithley Model 616 Picoameter, or equivalent. l 5.2 Collection Voltage Supply: Canberra Model M3002 or equivalent. 5.3 DVM: Fluke Model 3040A or equivalent. 5.4 General l
- 1. Detector Fixture (P/N 952848-001) 9
- 2. Approximately twenty feet of low noise co-ax cables for connection between detector and readout I .
l 3. Six foot steel tape measure 1 r
- 4. Interlock extender
- 5. Stopwatch with 0.1 second resolution.
- 6. Three prong extension cord, 6 ft. minimum, with 3 tap cube socket.
l
- 7. KDA-HR Energy Response Shield Kit (P/N 451221-001).
i l
DOCUMENT KNPNO. Kmsesslastrumentation Wh STANDARD PRACTICE PROCEDURE nev, PAGES opl4 A
6.0 DESCRIPTION
OF FACILITY 6.1 The facility consists of a Calibration Room and a Control Alcove. It is located in the basement level of Penrose Cancer Hospital, Colorado Springs. 6.2 The calibration source is mounted on a steel stand in the Calibration room such that the collimated radiation beam will be projected parallel to the floor. 6.3 A single U-channel track is positioned on the floor extending from the source stand and running parallel to the exposed beam. 6.4 A moveable table with casters, two of which are in the U-channel, and height adjustable top, is used for positioning the detectors in the radiation beam. A detector fixture is fastened to the table top. 6.5 A hinged Attenuator Assembly is attached to the source stand in front of the source beam collimator. , 6.6 The source control console is located in the Control Alcove. 6.7 Test equipment is kept in the KI Rad lab, but may be stored .in the Penrose Calibration Room during protracted calibrations. 6.8 Radiation beam intensities used in this KNP have been measured with an ; fonization chamber whose Cs-137 calibration is traceable to NBS. Pertinent l data is located in the "Penrose Source and Equipment" file and the "Penrose Facility" lab notebook. Official copies are maintained in the XI ESD QA' record files. 7.0 GENERAL PROCEDURAL DESCRIPTION Radiation beam intensities are adjusted by means of source-detector distance and attenuator combinations, which are listed in the specific detector sections of this KNP.
-_m mm -
ooCUMENT KNP NO. Mammenfostromsentation C c-h STANDARD PRACTICE PROCEDURE n av. PAGE 6 OF)4 A The detector fixture is fastened to the detector tabletop, the detector fastened in place, the detector height adjusted so that the detector is centered in the radiation beam, the detector table moved to the, appropriate distance, the proper attenuator combination selected, and detector output is recorded as a function of radiation intensity. 8.0 SOURCE OPERATION 8.1 Connection (Make sure that the mains switch on the Picker control panel is 0FF). '
- 1. Unco 11 control cable from source and connect to J-box receptacle fastened to wood platform at rear of room.
- 2. Plug line cord from wood platform into line receptacle on side wall of Calibration Room.
- 3. Source is now ready to operate.
8.2 Control Panel: The Picker Control Panel, located in the Control Alcove, has, a mains j switch, a key switch, a timer with center knob detent minutes adjustment l and outer ring seconds adjustment, a timer on-off toggle switch, and one ) green and one red light. Upon turning on the mains switch, the green light comes on. When the source begins to leave its fully closed position, the ' red light comes on. When the source reaches its fully open position, the green light goes off, the red light remaining on. l . 8.3 Operation:
- 1. Turn on mains switch.
- 2. Select exposure time on timer, appropriate to the operation being performed.
I s
I DOCUMENT KNP NO. h #"*8"*"#* W STANDARD PRACTICE PROCEDURE g y, PAGE 7 orl4 A
- 3. Turn timer toggle switch to "on".
- 4. Rotate spring loaded key switch ccw and hold in that position until green light goes out.
S. Source is now in fully open position. T
- 6. When the preselected time has elapsed, the timer will shut off the source.
- 7. To terminate exposure manually, switch timer toggle switch to "off".
- 8. Note that green light comes on and red light goes off on source
, control panel, before entering Calibration Room. 8.4 Emergency Procedure: If source sticks in the fully open position (green light does not come on) or halfway in between (both lights remain on), lock the door, and immediately contact the Penrose Health Physicist and the Kaman Engineering Physics Group (phone no. 599-1776 or 599-1788). The source will be manually closed by turning the emergency handwheel, and then placed out of use until repairs are made. 9.0 PROCEDURES 9.1 Preliminary Contact the Penrose Health Physicist (Greg Gibbs or Jerry White, 630-5285) to A) confinn that the source facility will be available for the anticipated calibration time, and B) arrange to obtain the Source key and the Calibration room key.
i coCUMENT KNP NO. h deedmmendsafen W STANDARD PRACTICE PROCEDURE nev, PAGE O OF14 A 9.2 Upon Arrival at Penrose:
-1. Place upi.olstered, fire resistant, screen (located in the adjacent hallway) across the entrance to the Control Alcove. This is to screen calibration activities from patients using the adjacent treatment room, and is a condition of the Penrose/Kaman agreement for the use of j this facility.
- 2. Connect source.as described in " Source Operation" section (8.1).
I
- 3. Place interlock extender at top of narrow door to Calibration Room, allowing ~ this door to remain open about one inch for power and instrumentation cables, while keeping background in the control alcove
; at safe levels (well below NRC limits), and turn on the chirper clipped to the source frame.
l The remainder of this procedure assumes the use of the Keithley model 616 picoammeter and Canberra model M3002 HV Power Supply.
- 4. Place the picoameter and HV supply in the control alcove.
l 5. Run the extension cord from the wall plug in the calibration room , adjacent to the access door, to the control alcove and plug in the l picoameter and HV supply. , l i
- 6. Connect the low noise co-ax cable marked "SIG" to the Keithley input, and the cable marked "HV" to the HV supply. Use the ends opposite the ends marked.
- 7. Fasten the detector fixture to the detector Jable, using the holes and bolts provided. Bolt the detector clamps at the widest position (7 inchesapart).
i
- 8. Adjust table height so that the table top is 33.25 inches from the floor.
pocWMENT KNPNO. 18-104 4 Kmesam ih*8888 W STANDARD PRACTICE PROCEDURE n Ev. PAGE 9 0F14 A l
- 9. Attach energy response shield to detector per KNP 30-3.
- 10. Clamp detector to fixture, centering the sensitive volune (section of reduced diameter) between the clamps.
- 11. Connect the marked ends of the cables to the appropriately marked terminals for the ion chamber, using MHV-N adapters.
- 12. Move the detector table so that the horizontal distance, D, between the detector center line and the ph'ilips screw on the source collimator (Fig.1) is:
D = 39.34 e -0.01155 (T-To) - 6.09 inches where .01155 = in .5/2 (30) 30 = Cs-137 half life, years T = date of calibration To = date of source calibration = 3/26/84* 1 (T-To) is in years, to nearest tenth 6.09 = distance in inches between reference point and center of source 39.34 = source to detector centerline distance at time of source calibration This distance is shown in Figure 2, for convenience.
- Distances and intensities to be re-measured by Engineering Physics Group at intervals not to exceed four years.
4 l
l DOCUMENT KNP NO.
" - ~
Kansaninstrammentation c ;1 STANDARD PRACTICE PROCEDURE a y, PAGE10 OF14 A FTC3 Rn 2 33 ' G ,Y ' 7
=
N s o -
? l 31 o - I/s4 1/ss I/s6 t/87 t/se
' ' YEAR j 9 . g_ --
det. e . coli./ NOTE: Attenuator shelf must be swung out of the way to access the FIGURE I source Collimator, and reference point. There are five attenuators in the attenuator assembly. They will be referred to as no. I through no. 5 beginning with the one closest j to the source.
- 13. Pull no. 1, 4, and 5 out, push no. 2 and 3 into the beam path. ;
\
- 14. Turn on HV supply and adjust to +800 10V. '
Keep-Alive Current:
- 15. Keithley Setting for current integration:
\
back panel: connect shorting bar between "GND" and "LO" terminals. l front panel: upper toggle switch on " FAST", lower toggle switch on l "ZERO CHECK", range selector on E-9 COULOMB, sensitivity on fourth position from "AUT0". l
DOCUMENT KNP NO. Karmenimeirvementatten Omrperses'" 18-104 - STANDARD PRACTICE PROCEDURE n ay. I PAGE llOF14 A
- 16. Adjust "ZER0" on Keithley to an indication of 0.00 0.01.
- 17. Flip lower toggle switch on Keithley to the left. The meter indication will begin to ramp up.
- 18. With a stopwatch, start timing when the panel indicates 0.10 or other conveniently low indication. Record this initial reading on data
~
sheet.
- 19. Let indication ramp up for at least 60 se'conds.
- 20. Stop timing when indication is 01.1 or higher. Record final reading on data sheet.
- 21. Record time interval in seconds on data sheet.
- 22. Compute Keep-Alive current as directed on data sheet and compare with acceptance limit.
- 23. Flip lower toggle switch on Keithley to "ZERO CHECK".
- 24. Close Calibration Room Doors so that interlocks are engaged. ,
l 3.04 R/hr Reading:
- 25. Turn source on (Ref. section 8.0 for source operation).
- 26. Adjust "ZER0" on Keithley to an indication of 0.00 0.01.
- 27. Flip lower toggle switch on Keithley to the left. The meter indication will begin to ramp up.
~
- 28. With a stopwatch, start timing when the panel indicates 1.0 or other conveniently low indication. Record this initial reading on data sheet.
DOCUMENT KNP NO. h '"*8N"**#88h 8898"88"" STANDARD PRACTICE PROCEDURE nev,
' ^
PAGE 12or14 A
- 29. Let indication ramp up for at least 60 seconds
~
- 30. Stop timing when indication is 3.5 or higher. Record final reading.
- 31. Record time interval in seconds.
- 32. Turn source off. Note that green light comes on and red light goes off, on source control panel.
- 33. Compute current as directed on data sheet'.
- 34. Subtract the " Keep Alive" reading from the source reading and record on the data sheet.
- 35. Compute Efficiency (A/R/hr) as instructed on the data sheet and
- compare with the acceptance limits.
30.1 R/hr Reading:
- 36. Enter Calibration Room and pull attenuator no. 3 out. Return t Control Alcove and close doors, engaging interlocks. ,
f
- 37. Keithley Setting for direct current reading:
Same as step 14 except front panel range selector on E-10 AMPERES. ! 38. Adjust "ZER0" on Keithley to an indication of 0.00 .01.
- 39. Flip lower toggle switch on Keithley to left.
- 40. Turn source on.
- 41. Record reading on data sheet. -
- 42. Turn source off. Note that grean light comes on and red light goes off, on source control panel.
w
DOCUMENT KNP NO. h """*" W STANDARD PRACTICE PROCEDURE any, PAcel3 oF14 A
- 43. Subtract the " Keep Alive" reading from the source reading and record on the data sheet.
- 44. Compute Efficiency (A/R/hr) as instructed on the data sheet and compare with the acceptance limits.
299 R/hr Reading:
- 45. Enter Calibration Room and pull attenuator no. 2 out. Return to .
Control Alcove, closing door to engage interlocks.
- 46. Turn range selector on Keithley to E-9 AMPERES
- 47. Adjust "ZER0" on Keithley to an indication of 0.00 0.01.
- 48. Flip lower toggle switch on Keithley to left.
- 49. Turn source on.
- 50. Record reading on data sheet.
- 51. Turn source off. Turn Collection Voltage Supply off.
- 52. Subtract the " Keep Alive" reading from the source reading and record on the data sheet.
- 53. Compute Efficiency (A/R/hr) as instructed on the data sheet and compare with the acceptance limits.
- 54. Complete Data Sheet, filling in all information called for.
- 55. Move on to the next detector, or restore facility to its original condition. (Don't forget to turn off the chirper).
i 4 y - - . . - , - - , --
I DOCUMENT KNP NO. Kaman instrumentation Corporatto" - STANDARD PRACTICE PROCEDURE asy, PAGE 14 OF14 A l 10.0 DATA SHEET - KDI-1000 PRIMARY CALIBRATION, Cs-137 l Calibration Date Customer / Channel KI Detector Part No. Mfgr. Serial No. ITEM MFGR MODEL S/N CAL DUE Picoammeter HV Supply DVM I Keep-Alive Current (Acceptance Limits = 0.9 to 5.5 x E-11A):
- 18. Initial Reading (E-9 Coulombs)
- 20. Final Reading (E-9 Coulombs)
- 21. Time Interval Second (60 seconds minimum)
- 22. Current = (Step 20 - Step 18)/ Step 21 = Amperes 3.04 R/hr readings:
28.' Initial Reading (E-9) Coulombs
- 30. Final Reading (E-9) Coulombs ,
- 31. Time Interval Seconds (60secondsminimum)
- 33. Current = (Step 30 - Step 28)/ Step 31 = Amperes
- 34. Net current (Step 33 - Step 22) = Amperes
- 35. Efficiency (Step 34/3.04)) = A/R/hr
- 30.1 R/hr readings:
- 41. Gross current = E-10 Amperes
- 43. Net current (Step 41 - Step 22) = E-10 Amperes
- 44. Efficiency (Step 43/30.1) = A/R/hr
- 299 R/hr readings:
- 50. Gross current = _E-9 Amperes ._ .
- 52. Net current (Step 50 - Step 22) = - E-9 Amperes u - ,
- 53. Efficiency (Step 52/299) = A/R/hr *
- Acceptance Limits = 0.8 to 1.2 x E-11 A/P,/hr By Date QA Date l
DOCUMENT KNPNO.
-I04 Maneam ineiramensatten Corporah STANDARD PR ACTICE PROCEDURE n ev.
PAGE 140F14 A 10.0 D/ TA SHEET - KDI-1000 PRIMARY CALIBRATION, Cs-137 Calibration Date /o/e[& V Customer / Channel Gaa/ 1 <'d XI Detector Part No. P-7(43c-oo3 Mfgr. Serial No. */46:2 4 l ITEM MFGR MODEL S/N CAL DUE Picoanineter /Gi& Icy 6 n ra*
- 8 N Y '8/#
gooz wr p 1.V W.~3 **l"lW HV Supply on Jerro DVM w/4 Keep-Alive Current (Acceptance Limits = 0.9 to 5.5 x E-11A):
- 18. Initial Reading a/o (E-9 Coulombs)
- 20. Final Reading /. e o (E-9 Coulombs)
- 21. Time Interval 46.0 Second (60 seconds minimum)
- 22. Current = (Step 20 - Step 18)/ Step 21 = /,5.7 E-u Amperes 3.04 R/hr readings:
- 28. Initial Reading o f8 (E-9) Coulombs
- 30. Final Reading 3 ED (E-9) Coulombs
- 31. Time Interval 49.4 Seconds (60 seconds minimum)
- 33. Current = (Step 30 - Step 28)/ Step 31 = '/.3 / #-// Amperes
- 34. Net current (Step 33 - Step 22) = .7.7f E-// Amperes
- 35. Efficiency (Step 2H3.04)) = . 92 E-" A/R/hr
- 30.1 R/hr readings:
- 41. Gross current = 2.90 E-10 Amperes
- 43. Net current (Step 41 - Step 22) = # 7# E-10 Amperes
- 44. Efficiency (Step 43/30.1) = + 9/ E-// A/R/hr
- s 299 R/hr readings:
- 50. Gross current = 2 73 E-9 Amperes
- 52. Net current (Step 50 - Step 22) = 2. 7 / E-9 Amperes
- 53. Efficiency (Step 52/299) = . 9/ E- // A/R/hr
- l
- Acceptance Limits = 0.8 to 1.2 x E-11 A/R/hr BMd Da te /p[8k'/' QA c.dm24' Date /04k '
# O .
DOCUMENT KNPNO. Mamm. lastrwaentation corpor ena"
- 04 STANDARD PRACTICE PROCEDURE n ev.
PAGE 14 OF14 A 10.0 DATA SHEET - KDI-1000 PRIMARY CALIBRATION, Cs-137 Calibration Date /o[#/P'/ Customer / Channel d 5* * /- (/= M KI Detector Part No. &#W 3 4 -ooS Mfgr. Serial No. - <?A 7/O ITEM MFGR MODEL S/N CAL DUE P1coansneter f(,;6p /e y c tt, przg /a osmy g jy ,e y , goo:z pgy+tvns s//t/tr HV Supply % 4, a,.a DVM s/A Keep-Alive Current (Acceptance Limits = 0.9 to 5.5 x E-11A):
- 18. Initial Reading o./c (E-9 Coulombs)
- 20. Final Reading /. / o (E-9 Coulombs)
- 21. Time Interval 9 7. 2- Second (60 seconds minimum)
- 22. Current = (Step 20 - Step 18)/ Step 21 = /.0 3 5-// Amperes 3.04 R/hr readings:
- 28. Initial Reading 0 So (E-9) Coulombs
- 30. Final Reading % r0 (E-9) Coulombs '
- 31. Time Interval /os./ Seconds (60 seconds minimum)
- 33. Current = (Step 30 - Step 28)/ Step 31 = 9.Pe ^// Amperes
- 34. Net current (Step 33 - Step 22) = #.7.5~#-// Amperes
- 35. Efficiency (Step 34/3.04)) = . 94' E-// A/R/hr
- l 1
! 30.1 R/hr readings:
- 41. Gross current = 3. o 6 E-10 Amperes
- 43. Net current (Step 41 - Step 22) = S 9 4 E-10 Amperes
- 44. Efficiency (Step 43/30.1) = . 9P 3-// A/R/hr
- s 299 R/hr readings:
- 50. Gross current = 4. 9 P E-9 Amperes
- 52. Net current (Step 50 - Step 22) = S.97 E-9 Amperes
- 53. Efficiency (Step 52/299) = .19 E- // A/R/hr *
- Acceptance Limit:; = 0.8 to 1.2 x E-11 A/R/hr By 0 Date lef8 h QA h./ Date }O " T &,
y .
l I Y DOCUMENT KNPNO. Kansan instessmentatten Watto" STANDARD PRACTICE PROCEDURE c y, PAGE 14 0F } 4 A 10.0 DATA SHEET - KDI-1000 PRIMARY CALICRATION, Cs-137 Calibration Date 4 /),, JJ Customer / Channel 6.f . [ /[, ,'! KI Detector Part No. B2VL3 6-oo3 Mfgr. Serial No. f c/6 Z.y ITEM MFGR MODEL S/N CAL DUE Picoammeter f,'/// 4,4 gs/zofy of/oV[BS' HV Supply g,,, f ,,.m Nb 2y W.s G,. edcL / DvM g/sh ,,e4 Ef / zos7 ov/<r/sr Keep-Alive Current (Acceptance Limits = 0.9 to 5.5 x E-11A):
- 18. Initial Reading 1 (E-9 Coulombs)
- 20. Final Reading n.1 (E-9 Coulombs)
- 21. Time Interval &c Second (60 seconds minimum)
- 22. Current = (Step 20 - Step 18)/ Step 21 = i.G 4 4. " Amperes l
3.04 R/hr readings: I
- 28. Initial Reading I .0 (E-9) Coulombs .
- 30. Final Reading 1.70 (E-9) Coulombs
- 31. Time Interval __ &t Seconds (60 secer.ds minimum)
- 33. Current = (Step 30 - Step E8)/ Step 31 = 4.42 (" Amperes
- 34. Net current (Step 33 - Step 22) = 2.% E'" Amperes i
- 35. Efficiency (Step 34/3.04)) = 4. o 1 / -' Z- A/R/hr
- i 30.1 R/hr readings:
- 41. Gross current = 2.8 T E-10 Arperes
- 1. 0 t
- 43. Net current (S tep 41 - Step 22) = -fr&6, g. -**E-10 Amperes
- 44. Efficiency (Step 43/30.1) = i.co E -" A/R/hr
- 299 R/hr readings:
- 50. Gross current = 2 85 E-9 Amperes
- 52. Net current (Step 50 - Step 22) = 2. s 4 t-i E-9 Amperes
- 53. Efficiency (Step 52/299) = =F52 E ~'* A/R/hr *
- Acceptance ' . its = 0.8 to 1.2 x E-11 A/R/hr By / e f,&f QA 8f o Date / .J-f R
occuM[NT KNPNO. Kaman inste umentation Corpor ation
- STANDARD PR ACTlCE PROCEDURE u s y.
PAGE 14 Of l 4 A 10.0 DATA SHEET - K01-1000 PRIMARY CALICRATION, Cs-137 Calibration Date 2. L 86 Customer /Chanr.el C)dd. KI Detector Part No. 8 2.84 43L 003 Mfgr. Serial No. , 2 2.~1 \ O ITEM MFGR MODEL S/N CAL DUE P.icoammeter g'4\ ggg g g 2,og 3 fgy P ' tl \ t \l'\c.3
" C.e.n\aeeea 3002 3 st sg Flo Re, 8040 A. (S ROT 3 4l a5 i Keep-Alive Current (Acceptance Limits = 0.9 to 5.5 x E-llA): !
- 18. Initial Reading .) (E-9 Coulombs)
- 20. Final Reading g.) (E-9 Coulombs)
- 21. Time Interval c)l.7 5 Second (60 seconds minimum)
- 22. Current = (Step 20 - Step 18)/ Step 21 = 1.o 2 8 L~"Ampe res 3.04 R/hr readings:
- 28. Initial Reading s. o (E-9) Coulombs l
- 20. Final Reading 3.5 (E-9) Coulombs
- 31. Time Interval __ M . 5' Seconds (60 seccrds minimum)
- 33. Current = (Stt_p 30 - Step E8)/ Step 31 = J;1oif.j.Arperes
- 34. Ne t cu rren t ( S t ep 33 - Step 22 ) = _2.],]5_f.j'Ampe r< s
- 35. Efficiency (Step 34/3.04)) = _8.8ci[-A/R/hr
- 30.1 R/hr readings:
- 41. Grcss current = t_mS G E-10 kperes
- 43. Net current (Step 41 - Step 22) = M T'l E-10 Amperes ,1
~
44 Efficiency (Step 43/30.1) = _8. 8 2.S t._ 'h/R/hr
- 299 R/hr readings:
- 50. Gross current = 2. S \ C. ~i E-9 Amperes
- 52. Net current (Step 50 - Step 22) = _2.8 E - I E -9 Amperes
- 53. Ef ficiency (Step 52/299) = 9 . 3 dt.-i 2-A/ R/ h r *
- Acceptance Limits = 0.8 to 1.2 x E-Il A/P,/hr l l
.A l By Mw0e te g&&S- QA6 _ Da tepsr- fg
f" l i APPENDIX D Mechanical Aging Test Data 460036-002 Appendix 0 i
FIGURE 7 Qualification Data Record Date Record Sheet # //d '/ Title of Test: MarhmUc c( A ai wa Test Procedure: a.J Loo 3 6.-00 t bd\ \ Sequence #: 3,4,3,3 Test Article: mA I ed(A - d1 lOd ekaulcer Test Method: hamd ~I~In e_w, d Test Equipment: QA. __ Mfr/Model/5/N: 11 A Calib. Due: il A_ Ambient Temp: 2 4 *C., Ambient RH: J 2 */, Time: 0900 Date: in ad 84 By: Owukf-s go QC Stamp:6 / I / 5 ,5/-f f~ v - Acce nce Test Article ID Reading Cri ria l Wi l J e_ %/.02.-c 1 3 . . 1461_ , L, bar 2 2A to t (c. 2 e a L a,_ c.a c\e_ .4 2.< C4/LL. _iL.2 h k 4- '/ ' ' ' w.' wers af su sf tu r iRt w ifft- e uAt e
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FIGURE 7 1 Qualification Data Record Date Record Sheet # bhN Title of Test: T o ev - C ac_ker \ i l Test Procedure: 4t e o m -e>ct ds_o A sequence a: 2.q.3.4 Test Article: MAj c (d,_ d lod cha%bor i Test Method: 1 Jg ce L u e c (o ce. Test Equipment: T~ro a e- kl.r em e_k ) T.Que.N1 ore Mf r/Model/S/N: bdhm.m /4L1847 & / kl ff-096. I klA Calib. Due: ig[gtl a d, A Ambient Temp: 2_4 *c, Ambient RH: 398/o Time: ogeo Date: -22 och 3 4 By- Cmh 77,, - QC Stamp:- A f l [ jd/ g-3 g- -, Accep ce Test Article ID Reading Crit ia HAl G_d ( e 7 6L0 2_-01 tom 227to sic . A c_uelee v och O L Cbe o A c__etab w o. 9 L.A 4 Ao ~' ser
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to d 2.rt t o 4, t/. . 1 ea cJ e r ,# c.L o - C m. ,xc_e o b we . 9 L., 4 4am" o r u el e'c e. w L us. to L-c' t. kor ' ur i i , , , , , , , , , , , , J 1 ; J q 1 J o1 J A 1 J c t J r 1 t i / t & i t J / \ 9 / t J l t .U 1
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10 ' VVVV I
FIGURE 7 Qualification Data Record Date Record Sheet i M/t 3 Title of Test: gA,, b 2 ul A .'. m a t- i Test Procedure: gr.oo3t _ oog d,a A Sequence f: 3.9 3
.i Test Article: s4) O.Lle Mo4-o f - U f.GOf-oi M.
Test Method: _ % ,e g<fml,_ 2 G%.la comae.c_le v ( , Test Equipment: D ga L)m.s,1 ( Eness Ru k.a .e e Mfr/Model/S/N: ( n b u m - 4t N *1 3 - (1W5'-b96 Calib. Due. if /26[8p ! i Ambient Temp: 7.4 *c_ Ambient RH: 3 2*/. Time: t a; 3o Date: gCc/81 By: boa,.9. //- _ QC Stamp: i j-Acceptance Test Article ID Reading Criteria wI ol m i
. m au-1 Arse el C u-Il il J i
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Connector Test Article 2.5.2.1.1 After Mechanical Aging l Photograph D-1 l l
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Contactor Ter.t Article 2.5.2.2.1 Af ter Mechanical Aging Photograph D-2 l
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! Ion Chamber Test Article 2.5.2.3.1 After Mechanical Aging Photograph D-3 l l 1 i l l l'
1 1 APPENDIX E Irradiation Test Data i l I 4 i i i f i i i i 460036-002 Appendix E
APPENDIX E Irradiation Test Data The irradiation test certification from International Nutronics (plus . subsequent correspondence) is attached. The test articles were positioned next to the shroud that surrounds the Co-60 source plaques when they are in the " source up" position, as shown in photographs Figure E-2. Figure E-1 shows the chart recording of the ion chamber signal current during a " source up" and a " source down" transient inanediately prior to the conclusion of the irradiation test at T.I.D. of 2.2E8 Rads. 1 4 s 4 i 1 4 I
. , _ - . . , - . _ . - _ . . . - . _ , _ - . - - _ . _ _ . _ _ _ - . _ . . , _ _ _ _ - . _ _ _ . . . . ~ _ , _ _ . _ , . _ _ . _ . .
~ APPENDIX E Irradiation Test Data The irradiation test -certification from International Nutronics (plus , . subsequent correspondence) is attached. The test articles were positioned next to the shroud that ' surrounds the l Co-60 source plaques when they are in the " source up" position, as shown in photographs Figure E-2. Figure E-1 shows the chart recording of the ion chamber signal current during a " source up" and a " source down" transient inanediately prior to the conclusion of the irradiation test at T.I.D. of 2.2E8 Rads. 4 I 't i e I i 1 4 _ , .. -. . . , . , _ . . . . . . . - . , _ . _ _ . _ . ~ . . . . - . . _ _ _ _ . , . . . . _ . . . , . - . _ . _ . _ . . _ - ,
CUSTOMER NAME rAnw 1Mstmmrxion/ CUSTOMER JOB NO. P o. Piz 7'is I.N.I. RUN NO. #2-oo/ DATE Jo-zs- W TEST SPECIFICATION: T-6t b h he etcvraf b 2.owlo* P d_z 4 *r Ecos tana (A.c.h a 2.9 v io%f- A .E . bm PA n et -L o u o.r / I.o w g nos A.E./Ar. ROTATION REQUIRED: YES N NO TIME / DOSE INFORMATION: I A pgne.,A ,*~o CrlS r,_*b a a" 6 , b of /11 to6(bel: AE dr.
- [. c e. 6M J t L 4 hrs .
RUNNING TIME METER (RTM) . f DOSE MIN 2.o VOV DOSE RATE MIN l.22.viD-DATE /o-ry.# RTM IN 74 2 ,<. / RTM OUT7%o.\ SIDE DOSE RATE MAXl. & #c' DOSE MAX 277,,o8 DATE ti.3.% / TOTAL HRS lbi . DATE RTH IN DOSE RATE MIN DOSE MIN DATE RTM OUT __ SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE RTM IN DOSE RATE MIN DOSE MIN DATE RTM OUT SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE RTM IN DOSE RATE MIN _ DOSE MIN DATE RTM OUT SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE p.s.4A TOTAL HRS l(cM SIDE l DOSE RATE MIfl bl.#o' DOSE MIN *2.o >#ot DOSE RATE MAX 1%#o' DOSE MAX 2.hlo 8 BY . M. ,
...- B, avn , .
CUSTOMER NAME k;emw retstrunnuM77ed CUSTOMER JOB NO. Po. P/2 74 I.N.I. RUN NO. #2-ool DATE /0 U TEST SPECIFICATION: T-dt N-r lo he egwafJe 2 000 Pd 3 /t.r Eovid %4 (A.c.) a 2.9 so%f. A.E. Dm PA net b oucd f.n>gruesAE.[Ac. ROTATION REQUIRED: YES .>r NO TIME / DOSE INFORMATION: Ib. pw) ,sa CalE n_.% o ad h olcu of
/.2.2 stok 4d; A.E./Ac.
[. r. o b bt ef ( L4 hrs . RUNNING TIME METER (RTM) . DATE u-771/ RTM IN 7429./ DOSE RATE MINl.22.vol- DOSE MIN 2.o VOV DATE ().3.% RTM OUT'1 W o.\ SIDE / DOSE RATE MAXl.6hto' DOSE MAX 2'17 ,o8 TOTAL HRS S M . DATE RTH IN DOSE RATE MIN DOSE MIN DATE RTM OUT SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE RTM IN DOSE RATE MIN DOSE MIN DATE RTM OUT SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE RTM IN DOSE RATE MIN DOSE MIN DATE RTM OUT SIDE DOSE RATE MAX DOSE MAX TOTAL HRS DATE p.%% 10TAL HRS l MJ SIDE I DOSE RATE MINI.n+#o' DOSE MIN *2.o viot DOSE RATE MAX 1 % o' DOSE MAX 2. Thio
- BY .
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9 INTERN ATION AL NUTRONICS. INC. RECEIVED DEC 101984 November 5,1984 Mr. Pat McMillan Kaman Instrumentation P. O. Box 7463 Colorado Springs, CO 80933-7463 Ref: 460036-001 Rev. A., DAFR 460036-011, DAFR 460036-12 Drawings from Gary S. Turner - Dated 9 October 84.
Dear Pat:
On 10-12-84 I received drawings from Gary Turner. The purpose of these drawings was to point out the areas of concern where the test specifica-tion must be maintained. These drawings reflected four areas of concern marked A-A, B-B, C-C, and D-D. In subsequent phone conversations with Gary Turner, it was established that section A-A could not be maintained. This section was then taken off the list of areas of concern. The three main areas remaining were sections B-B, C-C, and D-0. Upon arrival at I.N.I. with the test unit, a fourth section was again added. This section was not specified on the drawings, but I make reference to it in attached drawing by Gary Turner. This fourth area was determined to be the mini-mum while section B-B was determined to be the maximum. The positions dose mapped are delineated on the attached drawings by myself showing the test specimen's relative position to the Source array. The curves included in the test certification package were plotted from dose points mapped for each section. All dosimeters were located at four replicate locations perpendicular to the Source. These locations are; the shroud, 5 inches out,10 inches out, and 15 inches out. Section B-B has three separate curves. These curves represent the top of the unit (B-B 1) the middle of the unit (B-B 2) and the connectors (B-B 3). Although unit C-C was mounted horizontally, instead of vertically, the positions were enumerated as Section B-B. (i.e. C-C 1 is the top of the unit, C-C 3 is the connectors.) Section D-D required only one curve so explanation is not necessary. Section RS was the fourth specified location and also the minimum for purposes of meeting test specifications. All Sections are located on attached drawing by myself. 1962 Barranca Road /Irvine, California 92714 (714) 863 9361 1 1
k
~. .
U INTERNATIONAL NOTRONICS, INC. Page 2 - Mr. Pat McMillan Kaman Instrumentation 9 I hope this information satisfactorily completes the test referred to above, but if you have any questions, or need any additional information
- please call me.
Sincerely, pM. Kevin M. O'Sullivan R.S.0./Q.C. Manager K0/ sat '! Enclosure i , 4 1 2 i e t
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- 1
+
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e s m o Chart recording of ion chamber S/N 22710 i output current during irradia tion tra nsient. Chart speed = 8 in/ min. Spikes in recording l are due to manual range switching on the picoammeter. Data recorded 11/3/84. Figure E-1 i ?
February 13, 1985 INTERNATION I Mr. Pat McMillan Kaman Instrumentation 1500 Garden of the Gods Road Colorado Springs, CO 80907
Dear Pat:
In response to your request regarding measuring equipment used to determine dose at I.N.I., Irvine, the following is a list of I.D. numbers, and explana-tion of calibration intervals associated with that equipment.
- 1. A.E.R.E. Harwell Red Perspex Type 4034 Dosimeters These dosimeters are calibrated on a "per batch" basis in accordance with our procedures and are traceable to the U.S. National Bureau of Standards.
- 2. Baush & Lomb Spectrophotometer Model: Spectronic 710 Serial #: Ol37418J The spectrophotometer is cleaned and checked with Standards traceable to U.S.N.B.S. , in-house, on a weekly basis. In addition, it is serviced an'd calibrated by Baush & Lomb on a semi-annual basis.
- 3. Mitutoyo Digital Thickness Indicator Model: 543-202 l Serial #: 110209 1
The thickness indicator is calibrated on a monthly basis, l in-house, with Standards traceable to U.S.N.B.S. All pertinent information regarding these calibrations is recorded in a bound log book used to document performance of these tests. Also serves as a perma-nent record. Certificates of Traceability, and Calibration Procedures are on file at this facili ty. I hope this letter meet your needs, but if you need anything else, you have but to call. Sincerely, ,
'lbH.C&dL.
Kevin M. O'Sullivan R.S.0./Q.C. Manager 1962 Barranca Road /Irvine, California 92/14 (714) 863-9361
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l APPENDIX F Seismic Test Data 460036-002 Appendix F l l
MMM 26 December 1984 Kaman Instrumentation P. O. Box 7463 Colorado Springs, Colorado 30933-7463 Attention: Mr. Pat McMillin
Subject:
Qualification Test of Model KDl-1000 Radiation Detector and Cable System, Wyle Job No. DE-58998
References:
- a. Seismic Test Data on Qualification Test of Radiation Detector and Cable System.
- b. Telephone Conversation, P. McMillin to C. C. Lee, 17 Decem-ber 1984 Gentlemen:
In response to your questions concerning the test data sheets on the referenced seismic test, I have the following replies:
- 1. A damping factor of 5% was chosen over 4% on the vibration aging test, since the Wyle shock spectrum analyzer does not equip with a 4% damping. We believe that it is a more conservative approach to choose 5% damping than to use 4% damping.
- 2. Due to the limitation of the Wyle seismic table, portions of TRS curves (below 1.25 Hz) do not envelope the RRS curve of the OBE and SSE tests. We l do not think that this would present any problem since a review of the l resonance search test records indicates no resonance frequency in that
! frequency range.
- 3. The TRS curves on vibration aging are now re-plotted for 5% damping from 1 to 1000 Hz. Please replace the old ones with these new data sheets.
If there are any additional questions, please contact me. l Very truly yours, j WYLE LABORATORIES C. C . W C. C. Lee Test Engireer
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SCIENTIFIC SERVICES & SYSTEMS GROUP
Enclosures:
12 TRS curves WESTERN OPERATIONS. NoRCo FACluTY 184I H.llside Avenue, Norco, California 91760 Area Code 114 7374871 TWX 9843321204 Telecopy (714) T374871 l l
v i A TEST DATA SHEETS IVR - RECEIVING INSPECTION, SEISMIC, AND IDCA TESTS ON RADIATION DETECTOR AND CABLE SYSTEM FOR KAMAN INSTRUMENTATION, INC. 1 9 f i I 4 f i l 4 6 j l l 1
WYLE LABORATORIES DATA SHEET co,too,e, ~KAM Ad IMST' so. ~o. 6Pf98 o,,e //-S-8d soecimen IAbWOAlbCIOR lbW RECElVING INSPECTION No. of Specimens Received: O Record identification information exactly as it appears on the tag or specimen: Manufacturer SMAA/ NN Part Numbers NA136.b- E bI~IOOO NId kAhlc d - ~' ('?ROToWfe-7 s How does identification information appear: (name plate, tag, painted, imprinted, etc.) S k SOMEd N6,d OM./b Serial Numbers:' Examination: Visual, for evidence of damage, poor workmanship, or other defects, and completeness of identification. Inspection Results: There was no visible evidence of damage to the specimens unless noted below,
- If additional space is required for serial numbers, use an additional page, or reference first functional test data sheet (if appliCJble).
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inspected ey DM D/Amsw sheet No. og Approwea C.C.. M Date il-Y"Y4 W-614 Q.C. Form Approval _.M
w WYLE LAeonatosutS SC.ENMC SEmnCES & SYSTEFS G80uP DATA SHEET SEISMIC 12ST TEST TITLE CUSTOMER AM AN D Job No. d SpecimenknBIATidkl DETMib9 f. CABlc 9 6EM Date Started II-bb Part No.sc. Fsn,. Tusp. Seriai No.9a Teni. Id Date Comp. 11- PW o F Spec. M OO MW I Par.2 4. f.f.5 Photo ES Amb. Temp.EO 3 p5 , TEST RECUIREMElffS Specimen Mounting NfflMEM W AS MIAcWGOTo h-No bVi~uttE t bolts / size / grade / torque lb Ud[ bolts. M86 kA Orientation: $DEetMGA bl:T14 ftWiaQE. \lff(L klGlDro To TEST heLE ! No. of Accelerometers: Control: 2- Response: i Locations /O
, RESONANCE SEARCH No. of Axes: b Ranges l-200 to l Hz Sweep rate: TMl n octave per Mini.Ts.
Acceleration level: O. E g SEISMIC RANDOM (BIAXIAL) No. of Tests & Damping: ld OBE's - 2.- % Damping
- 2. SSE's - 2 % Damping Range: 1. Z 6 to 100 Hz Amplitude controlled in I/3 octave increments Input source: M/1/ '/~[MO t1/ Ald/ NOOM tuned with a bank of parallel k3 octave filters with j individual output attenuators to meet RRS.
Response Analysis: Performed in 4 octave frequency increments. INSPECTION Following each axis of test. FUNCTIONAL RLQUIRDfENTS A L( YIJM CT/oNA L 5 hERfoRMED bY O.t1ST(%AG/2. Chatter Monitoring: h channels; for chatter in excess of Of/l (continued) f Tested by V W614A-82 OA Form Approval N - Engineer C. C.' M l
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