ML20023C041

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Affidavit of Dh Wade Re Midland-Ross Superstrut Matl (Board Notifications 83-02 & 83-14) & Welds in Main Control Board Panels (Board Notifications 82-90,90A & 116)
ML20023C041
Person / Time
Site: Comanche Peak  
Issue date: 05/05/1983
From: Wade D
TEXAS UTILITIES ELECTRIC CO. (TU ELECTRIC)
To:
Shared Package
ML20023C035 List:
References
NUDOCS 8305090521
Download: ML20023C041 (90)
v • d • e


Text

{{#Wiki_filter:, 9 I d 4 UNITED STATES OF AMERICA NUCLEAR REGULATORY COMMISSION BEFORE THE ATOMIC SAFETY AND LICENSING BOARD In the Matter of ) ) TEXAS UTILITIES GENERATING ) Docket Nos. 50-445 COMPANY, _et _al. ) 50-446 ) (Comanche Peak Steam Electric ) (Application for Station, Units 1 and 2) ) Operating Licenses) SUPPLEMENTAL AFFIDAVIT OF DAVID H. WADE REGARDING (1) MIDLAND-ROS'S SUPERSTRUT MATERIAL (BOARD NOTIFICATION 83-02 AND 83-14) AND (2) WELDS IN MAIN CONTROL BOARD PANELS (BOARD NOTIFICATIONS 82-90, 90A AND 116) I, David H. Wade, being first duly sworn, do depose and state as follows: I am employed by Texas Utilities Services, Inc. as Senior Licensing Engineer, Comanche Peak Steam Electric Station (CPSES) Project. In this position I am respon-sible for the evaluation and resolution of licensing 1ssues. As such, I am familiar with Applicants' commitments and program to assure the quality of conduit and instrumentation support materials supplied by Midland-Ross Corporation. I am also responsible for coordinating activities to address the welding matters in the Main Control Panels at Comanche Peak identified in IE Information Notice 82-34. A statement of my educational and professional qualifications was attached to my affidavit l of March 16, 1983. l l 8305090521 830505 PDR ADOCK 05000445 T PDR

o 2-I. MIDLAND-ROSS SUPERSTRUT This portion of my affidavit supplements the information provided in my affidavit of March 16, 1983, in which I dis-cussed the Applicants' program to insure the quality of materials supplied by Midland-Ross Corporation. I stated in that affidavit that procedures were being developed to assure that appropriate material physical properties are in accord-ance with applicable material specifications. These pro-cedures have been completed, and testing on a statistical sample of superstrut material is underway. To date, tensile and shear tests on welds have been completed and material tensile and bolt pull-out. tests are ongoing. Following the completion of these tests, the test data will be evaluated to verify the acceptability of materials in accordance with Applicants' commitment to per-form thest tests, set forth in the FSAR at Table 17A-1 (sheets 33 of 48 and 48 of 48, n.

49) (Applicants' Exhibit 3).

The test results will be available for review by the NRC. II. WELDS IN MAIN CONTROL BOARD l f In my affidavit of March 16, 1983, I addressed l Applicants' program to resolve questions concerning welding anomolies in the Comanche Peak main control board panels supplied by Reliance Electric Company, as identified in IE Information Notice 82-34. At that time, testing of the Hot l l l l I

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a osy.. ' attached.chereto. */.., - is.. ~ .c.e..- . The. obiective. of the t'est was to' q'ualify.the. welding ~ of ~ ..w ~~.the ' HSP.' and h.y. i.ir.tue of 5 structural. sim.Narity..th'e w$1 ding 1. <fc .w. . +. o g. n. w. g.. t h .of the' maid.E..o'ntrol' kE&Yd. pan'Qs..The report _ indicates 'that t ..a.

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u '.r. "nolwerd-related failuresh.er problems occurred during the' -.1.,. . Thus~, the rep' ort. concludes that.t.he panels Ifurnished t

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  • The Board h'ad' re'qhb'sted. thati~.this i% port. be. provide.d.then coinpleted.- Abril; 7,.1983, conference ~ Call) : Tr. 22-23f.
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GT " ~ RELIANCE ELECTRIC b Re, lance Electric 4900 Lewis Ad. Stone Mountain, GA 30083 (M34) 938 4888 April 14, 1983 Texas Utilities Generating Company P. O. Box 1002 Glen Rose, Texas 76043 Attention: Mr. J. B. George

Reference:

Comanche Peak Steam Electric Station 2300 MW Installation, Purchase Order CP-0605 Units 1 & 2

Subject:

Seismic Simulation Testing on the Hot Shutdown Panel (HSP), Tag No. CP2-ECPRLV-01, Wyle Report No. 46623-1 Gentlemen: The attached Wyle test report documents the results of the testing performed on the Hot Shutdown Panel as modified for the purpose of evaluating the "as'-built" weld ancmalies that are present in the welds in various panels as supplied. The results of this test show that the weld anomalies in the Hot Shutdown Panel which are considered to be worst-case of all panels supplied had no adverse impact on the structural soundness of the Hot Shutdown Panel. No veld related failures occurred. The report also contains information pertaining to the natural resonances of the panel tested. In order to accurately evaluate the report and its contents, the following comments should be carefully considered if conclusions are to be made on the comparison of the natural, frequencies between the original design of the RSP, the modifed HSP for HFE design [~on the test panel in this report. .$n d 1. The test specimen did not correspond to the panel as installed in the field. Prior to the HFE redesign, the HSP utilized a security enclosure which surrounded the control panel area. Thi pre-HFE design was seis-mically qualified by analysis and modal testing. The post-HFE panel re-placed the enclosure with a light box, and lengthened the panel by sixty inches (60"). Both the light box and the extension are bolted to the remainder of the pre-HFE structure when installed in the field. This con-figuration was also qualified by analysis and modal testing. The tes.t specimen did not have all of the characteristics and structure of the panels qualified by previous analysis. Neither the enclosure from the old de' sign. nor the extension from the new desir,n were present. Therefore, the natural f requencies and mode shapes obtained during the resonance search runs on the test specimen will not reflect the same results obtained from the as-bu ilt configuration by means of analysis and verified by a low impedance test. i e l

ew Page Two Texas Utilities Generating Company Mr. J. B. George April 14, 1983 2. The removable side sheet mentioned in the report was used during the resonance search runs in order to more closely approximate the pre-HFE design. The sheet was removed for the OBE/SSE runs in order to insure it added no extra strength or stiffness to the structure, and to increase the stresses seen by the welds. However, the bolted arrangement does not provide the stiffness of either the original welded side sheet or the "X"- f rames used in the post-HFE structure. This adversely affects the fra-quency plots obtained from the resonance search tests. I 3. The light box was installed in order to more closely match the post-HFE design and to increase the stresses imposed on the welds. 4. The panel was welded to a tubular steel fixture (see Photograph 1, page 14). This in turn was welded to the test table (see Photograph 2, page 15). Close examination of Photograph 2 indicates the panel / fixture overhung the table top. Therefore, the ends of the panel were canti-levered and without direct support. This condition does not accurately reflect the field mounting conditions. In terms of weld stresses, the test mounting is conservative, since the lack of support artifically in-creases the flexibility of the panel. This in turn, adversely affects the frequency plots obtained from the test runs. 5. The height of the panel was increased by the depth of the mounting fix-ture. This artifically increased the cantilever arm of the specimen when compared to the location of the control accelerometers. This fac-tor adversely affects the frequency plots obtained from the test runs. 6. The doors of the panel were not tightly restrained during the resonance search runs, and as such caused impact-related shock frequencies. The shock frequencies resulting from the local door modes occurred near eleven hertz (11 Hz) and were quite violent in nature. These shock frequenciest adversely affect the frequency plots obtained from the test runs. 7. Reliance routinely performs resonance search tests prior to performing the OBE/SSE teat runs. The resonance search is used for design pur-poses only and is not intended to provide mode shape data or frequencies. Basing a panel's seismic qualification on the resonance search results of a few accelerometers would be highly inaccurate due to the test method itself. Several factors, such as panel overhang, potential table rocking motion, potential dynamic coupling between the heavy panel and the smaller i size shaker table, and insufficient specimen response accelerometers all lead to inaccurate and/or misleading results. Modal testing provides fre-quency and mode shape data that can be relied on, whereas a shaker table resonance search under the above suspect tests conditions cannot. The original objective of the test was to qualify the welding of the HSP, and thus the welding of the Main Control Boards. The justification for this approach has been detailed in Reliance document WQP-0404-A. The Wyle report indicates the original objective has been achieved. No weld-related failures or problems occurred during the tests. Therefore. the tests prove the panels furnished by Reliance Elec-t z- --,-,.,--.-,.-.,.m m ,..,.,.m... ,_-_,-,.m __--.,--r.,,,,_. m.-

w-Page Three Texas Utilities Generating Company Mr. J. B. George April 14, 1983 tric Company for the Comanche Peak Steam Electric Station are suitable for the use intended, are structurally sound, and do not compromise the performance or saf ety of the station. Should you have any questions, please contact the undersigned. Sincerely, RELIANCE ELECTRIC COMPANY CUSTOM CONTROLS DIVISION ~~ Vijay Bhandari NEQ Manager JW/in cc: R. E. Ballard/C&H [ Bandyopadhyay/G&H . Knight /TUSI R. Kissinger/TUSI M. Dunne/RDA C. McCarthy/RNY D. Roy/RSM R. Drew /RSM W. Allen /RSM J. Welsh /RSM i l l I e j I e

'lc SEISMIC SIMULATION TEST PROGRAM ON A HOT SHUTDOWN PANEL RELIANCE ELECTRIC COMPANY 4900 LEWIS ROAD STONE MOUNTAIN, GEORGIA 30083

E b e w sa % r5I i t-SEISMIC SIMULATION %@ n d s a e x i Test Report t = Y, L . ' \\ \\\\\\ \\ \\\\ @N $ l...\\lllElll i REPORT NO. 46623-1 ... g - g gg l [.?1 46623 ) y WYLE JOB NO. ~ p,, I 3 1 ] CUSTOMER 302943 { .g' P. O. NO. fGd NI I 83 I PAGE 1 0F PAGE REPORT l ggg -EN Mar h 7, 1983

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DATE .? .tr'Q p r R $yff. hn 4 SPECIFICATION (S) See References w:mswL

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in Section 7.0 1.0 CUSTOMER Reliance Electric Company ADDRESS 4900 Lewis Road, Stone Mountain, Georgia 30083 Hot Shutdown Panel 2.0 TEST SPECIMEN "*11*"** *1* *#1 C "P""Y 3.0 MANUFACTURER 4.0

SUMMARY

A Hot Shutdown Panel, hereinafter called the specimen, was subjected to a Seismic Simulation Test Program as required by the Reliance Electric Company Purchase Order Number 302943, and Wyle Laboratories' Seismic Test Procedure 541/8498-1/WB, dated January 21, 1983, Revision A. This test program was performed on February 10, 1983. The test program consisted of resonance search testing and triaxial random multi-frequency testing. The specimen was instrumented with accelerometers during the test program. It was demonstrated that the specimen possessed sufficient integrity to withstand, without compromise of structure, the prescribed simulated seismic environment. However, the doors opened during two of the random multifrequency tests as described in Paragraph 6.3.1. STATE OF ALABAMA Ala. Professional Eng. 7"7M"MTQ,"E7b"*7d / CtUNTY OF MADISON Reg. No. 12761 PREPARED BY O/tatEl [ E6 Vincent F. Kearns III ~ . being duty owom. J. E. Kuy nd'all %/ # deposes and says: The information conta.ned in this report is the result of co,npeste J/7/83 and carat ny conduct.a t.ets and is to tne b t or his knowi true and correct in APPROVED BY Cn [D WYLE Q. A. SUB ! BED and sworn to be e ene his '7 day of /7 A 4, t9 5' E T. R. Stinson ~ // YM Ex1,.Y Not. # u m.nd,o,io si.. o, m e. g / LABORATORIES SCIENTIFIC SERVICES & SYSTEMS GROUP HUNTSVILLE. ALABAMA

e PAGE NO. 2 TEST REPORT NO. 46623-1 4.0

SUMMARY

(Continued) Table I contains descriptions of the tests. Figures 1 and 2 show the horizontal and vertical Operating Basis Earthquake Required Response Spectra. Figures 3 and 4 show the horizontal and vertical Safe Shutdown Earthquake Required Response Spectra. Figure 5 shows a sketch of the weld locations. Photographs 1 shows a typical view of the specimen welded to the mounting fixture. Photograph 2 shows the specimer., mounted on the Wyle Triaxial Seismic Simulator. Photograph 3 shows a view of the specimen with the side plate removed. Photograph 4 shows the door fastening mechanism that was bent y during Run 12. l Photographs 5 through 8 show the accelerometer locations. Appendix I contains Transmissibility plots from the resonance search tests. Appendix II contains the Test Response Spectrum plots for the Operating Basis Earthquake and the Safe Shutdown Earthquake tests. Appendix III contains the Instrumentation Log Sheets and the Instru-mentation Equipment Sheets. Appendix IV contains the Wyle Laboratories' Seismic Test Procedure 541/8498-1/WB, dated January 21, 1983, Revision A. i [ l l WYLE LABOR ATORIES Ps yM gvitt, 5 3cm.

PAGE NO. 3 TEST REPORT NO. 46623-1 5.0 TEST REQUIREMErrS 5.1 Specimen Mounting and Orientation The specimen shall be welded to a Wyle-fabricated base-mount test fixture. The test fixture shall be welded to the Simulator Table. The specimen's mounting shall simulate its in-service configuration as closely as practical. The specimen shall be installed on the Seismic Simulator Table such that its principal horizontal axes shall be colinear with the horizontal axes of excitation of the table. 5.2 Resonance Search A low-level (approximately 0.2 g) single-axis sine sweep from 1 to 50 Hz shall be performed in each of the three (3) orthogonal axes to determine major resonances. The sweep rate shall be two octaves per minute. Transmissibility plots of the specimen response accel-erometers shall be provided. The side panel shall be removed following the resonance search tests. 5.3 Random Multifrecuency Tests The specimen shall be subjected to 30-second duration triaxial multi-frequency random motion wnich shall be amplitude-controlled in one-third octave bandwidths spaced cue-third octave apart over the frequency range of 1 to 40 Hz. Three simultaneous, but independent, random signals shall be used as the excitation to produce phase-incoherent motions in the vertical and two horizontal axes. The amplitude of each one-third octave bandwidth shall be independently adjusted in each of the three axes until the Test Response Spectra (TRS) envelop the Required Response Spectra (RRS). The resulting table motion shall be analyzed by a response spectrum analyzer at two percent (2%) damping for the Operating Basis Earthquake (OBE) tests and at three percent (3%) da= ping for the Safe Shutdown Earthquake (SSE) tests, and plotted at one-sixth octave intervals over the frequency range of 1 to 200 Hz. Five (5) OBE tests, followed by one (1) SSE test, shall be performed. The OBE RRS are shown in Figures 1 and 2. The SSE RRS are shown in Figures 3 and 4. WYLE LABORATORIES Huntsville Facility

j I l PAGE NO. 4 TEST REPORT NO. 46623-1 S.0 TEST REQUIREMENTS (Continued) 5.4 Specimen Response A total of six (6) specimen-mounted uniaxial piezoelectric accel-erometers shall be provided for the specimen during the test program. Placement of the accelerometers shall be as directed by the Reliance I Electric Company Technical Representative. Transmissibility plots of the specimen response accelerometers from the resonance search tests shall be provided. TRS plots of the specimen response accelerometers, for a selected OBE test (2% damping) and the SSE test (3% damping) shall be provided. l l [ [ WYLE LABORATORIES Huntsville Faethty

.=~ PA%E NO. 5 TEST REPORT NO. 46623-1 6.0 TEST PROCEDURES AND RESULTS 6.1 Specimen Mounting and Orientation The specimen was welded to a Wyle-fabricated base-mount test fixture using 1/4" fillet welds, 4 inches long on 12-inch centers, as shown in Figure 5 and Photograph 1. The fixture was welded to the Wyle Triaxial Seismic Simulator Table such that its principal horizontal i axes were colinear with the horizontal axes of excitation of the table (Photograph 2). The specimen's mounting simulated its in-service configuration as closely as practical. 6.2 Resonance Search Test Procedures A low-level (approximately 0.2 g) single-axis sine sweep from 1 H: to 50 Hz was performed in each of the three (3) orthogonal axes to determine major resonances. The sweep rate was two octaves per minute. 6.2.1 Resonance Search Test Results At the completion of the three single-axis sine sweeps, inspection revealed that the specimen's mounting bolts had 1 ened. The bolts ) were tightened, the side panel was removed, and th front-to-back sine sweep was repeated to ensure that the loose 1 tts had not affected the prior tests. Descriptions of the resonance search tests, including test numbers, axes, and input accelerations are presented in Table I. l Transmissibility plots (specimen response acceleromters divided by the control accelerometers) from the resonance search tests are pre-sented in Appendix I. 6.3 Random Multifrequency Test Procedurec The specimen was subjected to 30-second duration triaxial multifrequency random motion which was amplitude-controlled in one-third octave band-widths spaced one-third octave apart over the frequency range of 1 to 40 Hz. Three simultaneous, but independent, random signals were used as the excitation to produce phase-incoherent motions in the vertical and two horizontal axes. The amplitude of each one-third octave bandwidth was independently adjusted in each of the three axes until the TRS . enveloped the RRS. The resulting table motion was analyzed by a response spectrum analyzer at 2% damping for the OBE tests and at 3% damping for j the SSE tests, and plotted at one-sixth octave intervals over the fre-quency range of 1 to 200 Hz. I VWYuE LABORATORIES Huntsville Facility l 4 r-..-

PAGE NO. 6 TEST REPORT NO. 46623-1 6.0 TEST PROCEDURES AND RESULTS (Continued) 6.3 Randem Multifrecuency Test Procedures (Continued) J Five (5) OBE tests, followed by one (1) SSE test, were performed.

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CBE and SSE RRS are shown in Figures 1 through 4. 6.3.1 Random Multifrecuency Test Results It was demonstrated that the specimen possessed sufficient integrity to withstand, without compromise of structure, the prescribed random multifrequency tests. However, the center door came open during Run 5 (<OBE). The docrs were taped shut and testing continued. The right bay door came open during Run 12 (SSE). Photograph 4 shows a view of the door fastening mechanism which bent and allowed the door to open. Descriptions of the random multifrequency tests are described in Table I. TRS plots of the control accelerometers for a selected OEE test at 2% damping and the SSE test at 3% damping are presented in Appendix II. 6.4 Specimen Response Procedures Six (6) specimen-mounted uniaxial piezoelectric accelerometers were located on the test specimen as shown in Photographs 5 through 8. A magnetic tape recorder provided a record of each accelerometer response. Placement of the accelerometers was at the direction of the Reliance Electric Company Technical Representative. 6.4.1 Specimen Response Results Transmissibility plots of the specimen response accelerometers from the resonance search tests are presented in Appendix I. TRS plots of the specimen response accelerometers for a selected OBE test (2% damping) and the SSE test (3% damping) are contained in Appendix II. 6 I f, WYLE LABORATORIES Huritsville Facshty

PAGE NO. 7 TEST REPORT NO. 46623-1

7.0 REFERENCES

7.1 Reliance El,3ctric Company Purchase Order Nurter 302943 7.2 Wyle Laboratories' Seismic Test Procedure 541/8498-1/WB, dated January 21, 1983, Revision A 7.3 IEEE Standard 344-1975 Specification entitled "IEEE Recon = tended Practices for Seismic Qualification of Class lE Equipment for Nuclear Power Generating Stations" 7.4 Wyle Laboratories' (Eastern Operations) " Quality Assurance Policies and Procedures Manual," revised July 1981 WYLE LABORATORIES Muntsville Facshty

PAGE NO. 8 TEST REPORT NO. 46623-1 TABLE I TEST RUN DESCRIPTICNS I INPUT ACCELERATION RUN, (g) NO. I TYPE TEST AXES LEVEL FB-ZPA SS-ZPAlV-ZPA RE M S 1lSineSweep SS .2 g 1-50 Hz 2 I Sine Sweep FB .2 g 1-50 Hz i I Removed side pan-3 3 Sine Sweep V .2 g 1-50 Hz 3 el; discovered i specimen mount, [ i ing bolts had i l i loosened during i I l test. 4 Sine Sweep FB .2 g 1-50 Hz Rerun of Run 2 i with side panel l removed. l_~ 5 l RMF FB/SS/V <OBE Center door came open approx. I 25 seconds into j test. Taped all ! f doors shut. { 96i RMF FB/SS/V <OBE 7 RMF FB/SS/V OBE .7 .95 1.0 l i 8 RMF FB/SS/V OBE .7 .95 1.0 9 PM FB/SS/V OBE .75 .85 1.0 I l 10 PM FB/SS/V OBE .7 .85 1.0 11 RMF FB/SS/V OBE .65 .85 1.0 12 RMF FB/SS/V SSE 1.1 1.3 1.6 Right bay door came open approx. 15 seconds into test. Front-to-Back LEGEND: FB = Side-to-Side SS = Vertical V = Zero Period Acceleration ZPA = Operating Basis Earthquake OBE = Safe Shutdown Earthquake l SSE = Random Multifrequency 8 RMF = WYLE LABORATORIES Huntsville Facility

= e e Page No. 9 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peakl i 1.0 0 10K 100 0 10000 DAMPING l 2.%l 4 e e 7 6 4 l I 3 s J 1 / i I 1 1 .t Ir !Jji ,ii rM i I I i i i e r i n, i ,i i 4 4 1,ii i,.. .i.. e 4i 4 i,. ni. ,i s o i, ..o o. i i .u .u. i no

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il , I 4 i ,a.i i i i e e i 16i i 9 1 2 3 4 6 4 7 8 9 10 2 3 4 6 4 7 8 9 to 2 3 4 6 6 7 8 9 10 1 10 100 1000 Frequency (Hz) t 4 FIGURE 1. HORIZONTAL OPEFATING BASIS EARTHQUAKE REQUIRED RESPCNSE SPECTRUM ___ _ _ _ _ _ _ _ _ _ _.. _ _ _ _. _ ~. _, _ _. _ _.. _ _.. _.., _ _. - - _ -.. _. _. _ _, _ _. _ _.,._. _ _ _,.,,,. _, _ _ _ _ .~.. _.,._.-

Paga No. 10 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1.0 i 10 JE(, 100 0 10000 DAMPING lR%l e a 7 i- -+ e 4 f 1 [ ] 3 .s s .g i j i .,/ 8

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Page No. 11 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) l 1.0 10 X 100 i 10000 1 DAMPING l3 %l 10 e i e 7 e 4 I I 3 P T 1 a I # i I . h i t .I .*II I I I Ti i 6 l t i i I 3 ii. ' tli t Is . [* ti' } i !\\ 3 I I It il { i f j iii I i gg l y l l . I e., ifi .ie i 6 i e' i . 3 I 4i i i 6 i i 6,. .i. .4 e i 6 r e / N, F I i : ,.. x > i, 4 1 1 e 4 F I i IL

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i , i ! 4 i. .,i a a 4. i 4 6ei i i i i i i e i .6 6 l i a ... r e so a + e e i e s io a ... r e e sa l 1 10 100 1000 Frequency (Hz) i FIGURE 3. HORIZONTAL SAFE SHUTDOWN EARTHQUAKE REQUIRED RESPONSE SPECTRUM . _, ~. -. _ - - _ - _ -.. --_ - -.,,. _. - _ _. _.... _.. _ _ _ _ _ _... - _. _ - _ _ _ - - _, - - _. _. _ -.., _ _ _ _ _ _ _ _. _ - _ _ _,

Paga No. 12 Report No. 46623-1 FULL SCALE SHOCM SPECTRUM (g peak) 1.00 10 M 100 0 10000 DAMPING l3 %l s 7 A i I E I 3 . y-l 9 4 3 z E N .N Y

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Pags No. 13 R3 port No. 46623-1 I40 (TYPICAL 3 SIDES y 3 S' DES) _ k2 ceares:s (ry> CAL REFJ a L I J 42 l ~~ 1 - 4" wes b (Typoent. 3 s des) m (RER) FRoHT SibE PLAN VIEW i l l FIGURE 5. WELD LOCATIONS I VJYLE LABORATORIES ,,...,..., =,,

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I Page No. 22 Report No. 46623-1 1 I II l J 1 I This page intentionally left blank. ,l 1 I .4

PAGE NO. 23 TEST REPORT NO. 46623-1 APPENDIX I TRANSMISSIBILITY PLOTS TEST RUN AXIS 1 Side-to-Side 2 Front-to-Back 3 Vertical 4 Front-to-Back Horizontal Control Accelerometer HCA = Vertical Control Accelerometer VCA = i i WYLE LABORATORIES Huntsville Facility

Page No. 24 Feport No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 dif 100 0 1000 0 10 M g r r r -t-e ._ _q ,__y_ H-4 i_..

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Page No. 25 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100 3 1000 O to 9 I 7 1 + i i s 4 0 _m ~ - P, i .i i

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Page ::o. 26 f' Report No. 46623-1 FULI. SCALE TRANSMISSIBILITY 0.1 0 1.00 10 Q 100 0 1000 0 10 ~ - + _ --.l _-p, l L m l l + l __m.. _ ___m_ i --p-i ~~' s _..__ _-_.. _i_. a '1 9! 1 a e 7 12 l', c'.:--j.il ,r e i t : e w g l L -v+ M+ _ f ft._f g_ ,l' i s 1 l / 9 3 _m .~ +-___ y -y.__.- j a } 's I: .g i 3 ui , i, f a I i 1 !I I i.. e _s i 4 . - ;i i ' ' i W 10 [ in e l 2 i, .,/ ? 3 = z a ~g g a,; e a p 8= 0 s. ~/ i i A [q. h' ? "l" w b J I I I I I S .-.,_-R i _i. F i. g i i c i ... 7 e s ie a .r... a .,,a .q g 1 i 10 100 200 p p Frequency (Hz) F ACCEL NO. 3 Y NO. D f' SPEC! MEN ~ E Axis 55 I TEST RUN NO. e. .d

Page No. 27 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 @ 100 0 1000 O ,o +- p _u_ ---q_ _t p 7 l .+ i i e ..g_. ;n .t -. + - _ .q x _4-_ t i i e i 4 i 4 6 i ii j ji --+F F m i I -i ! I r i e s i, : s t, -_-.=_=. g + =_+_.i.;, =s =.,=t=. tu

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Page No. 25 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 2 100 0 1000 O 10 s ~ t-e M w Q 7 4 i, l 4 8 -- g-t___ 4 _g_._ _. p __ v_ --- + - - 4_._ 4 I j I I 2 i i + i i, r 4 .i. i e 7 4 ____f. z._. \\l I.. l l >e a_3 9 ) __u T.5 m t s m 1 y _- cr o a 1 i g r. 1 - 4 a 5W 4 i a 4 I i i I. ! ! I ,,1 1 e jj 'Ii - 8 i iit.- 6 L j g .i g i i i 1-e e u i. , (_ n ;. -__'.--r._, i n y. < ;t - 4 p.

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Page No. 29 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY \\ 0.1 0 1.00 10 ( 100 0 1000 O to i 1 7 i H e =-

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Page No. 58 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.00 10 3 100 CB 10000 DAMPING y usu 8 a 7 e 6 4 2 1 li' I 3 i l I 3 =!t3 I f 1 + , i i, f... ii, 4 i si 3 [ i 44 .e i - i 4 i , i i .i.' i. i.,

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Page No. 31 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 2 100 0 1000 0 10 4_- 7 r i- -4 l --t-m

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Page No. 33 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 $ 100 0 1000 O io ~ r l .+ l _= 4 _w l. i- _ I I 6 l+ t

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j j ii ii t j e i . {. e i i e e a eei. i 6 4 4 e 9 lfi 1 g f y i I' l L a p r i e 5 4 l s M = 1 i r N d I LE [ r El J" I.' f n f E',1 ~2 V .1 1 I f d L I-I -'W; i. I ! l. 1 i i a 1 Mf-t 8 !+1i!.. I!: 3 ! I i t 1 3 'i, i

  • g Jwi

[in/ 6 i ,t;4.1

6t 1

i 63 f-w i: e ~~ u r i. -i Wf: e i p. 8.- e a I s e !5,, 1..,s. 1 I i. a 1. ii ,i a . e e r e v io a . e e r e so a . e e r e s io 1 10 100 200 Frequency (H7) SPECIMEN ACCEL NO. NO. M ~ AXIS EO TEST AUN NO. b

l Paga No. 62 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.0 10 0 100 9 10000 DAMPING d Wfa& %1 [ f 4 r g i 3 I 3 __ I ri1 4 r I ' s6 : . ! li i i = if ,II I I I . i ,,'3 i, f 3 i ! 3 i ( t f i *t iiII

4+

i i 6 66 i 3 ie t 4 e I i ii eei3 .6 i e i 6 4 4 6 6 i is6 i e ) 1 f 4 4 o I y m 15 - En o i 1 5 , I a 1 i i i. 1 e ,i1 i ,1 1 i i i i. o +- i i ,n, i ni, .i ii. ..ii .o i.., W . t.9 i W t sg ~6 GO s i a. 8m 4 de i s 3 I ( t . t i.3 iJ l I. i l l I ' i !!!i - f. 11 6 ( I q l 7 ! l 4 i . i. n. .i,., 1 i. i i i... it. ..o i e a + o e r a s io a r... .7 ..i. 1 10 100 1000 { Frequency (Hz) 4 SPEC 7 MEN LOCATION NO. / 8d l AXIS NI TEST AUN NO. I1 s a 9 -m-- a-x,-, ,+--. ww,--m.,n ,-...an .,e , w .n-nn n- -an ,n----,..

Page No. 35 l Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100 0 1000 C to 9 1 7 i i s S r_ + ~. I 1 ~ l s t i t + + i t a- + i i i i1 8 I' r y 4 4 ,4 4 I ri p a k' us 'W i n . m r I 1

  1. s T

I 1 ' Ii I e r r r s y! a c ; i l,,, ,r 5j, ,p i t i I ! . ?ti ~ff

  • t Ii 6i I

[ 6 i g. i,i .p4.- 6. i 6 i, <y 9 e l, 7 L. / l 2 i 3 a g 4<. s 8-I F U s 1 ., z a f t E I I 1 I i. i i., i i i, i 1

ei iii.

i. i t ,i a ... r.. ie a ... r e io a . e e i. io 1 10 100 200 Frequency (Hz) 1 SPECIMEN ACCEL NO. b O NO.N @ ~ AXIS FB TEST RUN NO. l

+ Page No. 64 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1.00 10 0 100fZL 10000 DAMPING l3 %l vu:u e ? i ] e 3 e 4 l 3 t 1 1 1 .I I I I 3 I P f 1 i f I ,1

i; i

3 i, i ,, i 3 u, I .. i. i i , 4 ii .66 n.!.. i. e

  • 7 i

i r-4 a 3 o$ 1 3 I N l .5 m 3 l t f !!L ri. ..I i i. i' 3 l Q) i I i i 4it i il ii-1 b 6 i i i f! illi i fl! 1 if!. i l I 3 I. g,, 4. i. i i .r. . 4,i i. o, o<e 2 7 , i sg g G3 e a-08 4 Ja i a l ] I J l 1 - I A i i ! I 1 i! i e + ! 3 e i a 4e i!ti it i l i i !, I! i 3 i i ; a; i, 4. 1 iI. i;; r i a a ... 1 e e so a ... r e e io a a 4 e e r e e so Frequency (Hz) l SPECIMEN LOCATION NO. 2Y Ob N/ TEST RUN NO. AXIS

Page No. 37 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 $ 100 0 1000 0 10 9 0 I ? l + s s 4 I T I 3 w 2 l 1 d4 1 i.- [ ). i e i 1 %i e g'.

Ii i

. 4 a 6. 9 e 'a 4' 'i 'r r 1 I L y J 1 1 I i i I 3 1I g i T~' -'~ f ~ '-i j s ~ Q .,e 1, -is "Y s i 11 sa in (/) i a ~ s 1 E 1 . +. i 't.. I i I i i Q i t i i

1.

I i I g s p. .[] 6 i e e i e e 4 1 e l 2 l ? i z ge -,/ 8 l a. l -h / m r rtEMQ[ w 9 P + i ' li; i i, . i i ii4 .. t > t s a s e s s i e e so n a e s s i e e,o a s e s e r e,,o 1 10 100 200 Frequency (Hz) SPECIMEN ACCEL NO. 2 M NO. V ~ 3 AXIS TEST AUN NO. l l l

Paga No. 30 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100 3 1000 0 +_. 7 ,i i i 4 _m._ .__4 2 E R Mm - 14 i i I ni. li . i., , i i.. i s e ,' i .,i I 1 1 I i s 3.-.; s ll f' i 1 6 j.. _. i >2 3: Tn \\ 1 m a 1 1 i N m i e i i i i i I : # 'i. i 1 3 1 i

  1. i:

t e i .I-i i, I i i ! i .iii p i > l. 1 i. .l; i I 1 8 I' .I' 2 7 7 i zg i i i a 1

5. 3

. g/55E =

g

. "e 4 s 1 i i. 8 i l I I ' I 8 P . t .I t t i i . i i i i .i. ,1 2 3 4 S S F S 9 10 2 3 4 5 4 7 8 9 10 2 3 4 6 6 7 8 9 10 1 10 100 200 Frequency (Hz) SPECIMEN ACCEL NO. I EE NO. NM ~ AXIS N TEST AUN NO. 1

Page No. 39 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100 21 1000 C io 9 7 l l .+ s = = _. t. .._.~ _. _ _. _._ - + _ _ -. _ _=___- _=_ _.- e s h ~ I a 'I' i i ~~ ~ 9 s l 7 s 4 [, a j._,__- >~ a j a f rn m g m i .f . i 1. e i I 3 '.r 1 .i i,. i1 n. i i i g. i si4 i i 6 a i i g e 9 7 z Z= 6 tt o

  • j u 8 -

4 a. r i ii i !i! i : ,i , i 4 k I f i 4 i 4 I + { I I i a ... r e e so a a 4 .. r e e io . e e :.. io 1 10 100 200 Frequency (Hz) NM SPECIMEN AC,CEL NO. N N O. AXIS VAT TEST AUN NO.

Pags !!o. 32 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY t e, o ,.c c ,0, ,m a ,oe a 1 l i-H- ~+ i _.__p-7. _1__ =. r j

.=
rg

-_;nr_2 ..___m I y i j9 4 1 i. 4 6 t i i 9 A i -t 0 m 'I 4 "" -[ l: mh g

== ._4J M ,I l _k i 'E l E i: l; i

. i ;

.i. i ,i i 3,, ,i m

-+--

If 2 7 i. 2a i i ri Z 0 1- -~ -e-b GG .~~ 'p

=:1..

8 e t-i se U-3m d l , p) 6__ s d I W -- f2 4 i i _$ X ~ ~ ' $ ~# .E .b l i i i. 'i y y. ..r .7 1 t ( h 9 10 100 200 i Frequency (Hd SPECIMEN ACCEL NO. 3 Y NO. McA Axis FB TEST AUN NO. E

Page No. 41 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1O O 10 0 100 0 1000 C ,o 9 i 8 i 7 + e 4 I I m__ t i i i 4 i . i ; ,ii. i. 1 .i. 6 I e 6 i - 6a. l 3 i e ? o s 4 1 a =.. 3 - = = =- 1'.' Zi

  • b, rnm

'E -4 e 1 i i g . i. i !.. r m ,o 4 3 . 4 a a i e io, i i. .I 4 ii e t. 6 g 4 9 8 2 7 3 y 3; a. -/; a .l~ ':#-L$p1 F .s : .J 1 1 i .AR I 11 ll 1 i ! I. I i's. i ; g,,

i, i

l-6 ,1 i I l. _ ii! j,r i i, i ii. i 1 i A i 4 e i . I, ii i a L .r a a a + , e r e e so a . e e i a e io ] 100 200 Frequency (Hz) ACCEL NO. b NJ NO. YM SPECIMEN 3 YEILY TEST AUN NO. AXIS

Paqs No. 34 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY f 0.1 0 1.00 10 0 10000 1000 O 10 9 s l 1 .T I I I j O t l s 3 l li, l-t Y i., ,i .m 1: e i 9 8 7 0 i i 4 ./ / e.- n. t-, sa M*. I i i -m. s 1 e i J .) I L i i i 'l . '#m" \\ l . 1! i h i l i 3 i . t i t < r. ' # t i i U 'ii lIi. I I p M' ~ p-i e]. .i .i 1 .a. 6 . 1 i e,ei Ft _ 8 'a 2 \\; ? i, 3 e m, 1 0 g 40 = 8=- a. m s 2 1 f T t 1. i

1 i

6.. ii 1 2 3 4 4 6 F e 9 to 2 3 4 6 6 7 8 9 to 3 3 4 6 6 F e 910 1 10 1C0 200 Fre Jency (Hd SPECIMEN ACCEL NO. O O NO. N@ l ~ Axis CB TEST RUN NO. i

Page No. 43 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 Si 100 0 1000 O 10 I 8 l ? l + l +- - + - - - 4 i l 1 3 --__+- 2 1 I I

)

e i ii +

  • t i

e 4 e e ili 6 i i 9 8 I 4 4 4 l l s t .e.e

63 m

l. Kj ..-i I st) hI E4 a y l: L Lip l l l .u y a 6 . i 6i i s 6 i i.i .6. . 4i i l. [ g i. A' 8 I ' f U 7 j X" 4 ~ ty !3. E : - E E !3

=

M* g; 9 4.c i = = w [

1 ,.r _A.b _3, a m _e_..____g ,_.__.5 y-- t ,:.= 1 3 r+ __,_-a. }i G.,f i.EI_ ~ E E ~ 4 F

  • ~_

"9 r i I '~ 1 ii 'U j I ! i s 1 i i 4. 1 i 2 3 4 6 6 F S 9 10 2 3 4 b 6 7 8 9 10 2 3 4 6 6 7 8 9 10 1 10 100 200 Frequency (Hz) NCb ACCEL NO. 2 6 NO. ~ SPECIMEN b AXIS FO TEST RUN NO.

Page No. 36 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 q 100 0 1000 C io e e 7 -+ l e _. m ._a_ _._w. s 4 f_ i i__ m_ l d ] i i i i i r 4 e i + i e t l' i ... It + + l 64 I e .,/ t i i i i i ii. .o i, 58 s,,.. i e e s i 1 ' \\ [ i 1 I L I s i

g.._

~ e 1; 4 Y i. i 3. b* m .m.. I a r i i - r us i { P 6 i! Y l } l 5W f e i. ! 4 ei i e i i i i .6. . 1 [ l e4.6 ieIi I i e p i 8 2 ,I z, i 7 .i s: s _ _._j.

  • u C C.

s 8.- a s 2.__ =+--- _..

-1 m-J 2

/ j'; 1 I i , 3 i 'i eIi l Il l 4 h 1 il i l t 1 l, 4 6 0 i a .7 a e io a ... r e e io a ... r e e io 10 100 200 l k I Frequency (Hz) I s ACCEL NO. I O NO. VGA ~ l AEN 3 AXIS \\lET TEST RUN NO.

Paga No. 45 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 Cd 100 0 1000 0 0 1 e -i l 7 a -= t_ . -m T,. _= _;- __4 _ m_. _. _ e r _..

4 4

s -__.= 2 I l t i r t i 6 .. 6 i i i h_.. 1 9 a 7 s s t, s ~~ m . _.i. %

=

i j 3 i = - s* N ; ggra = l m r 1 >, r t - 'g l l m i r-1 =B i i t 1 i t i .2 i. t 3 i. f i I i i . I t? FL J!. t i t i. I i iill i

  • i it:

t 3 h10 ...a./N#hi F 'i4 ' i* i = - Mg+ = f j g f Y i u 7 i. +M l if s y 50 s 8.- a 1 x. t ' Ii i i 1 ! I i i ta !i4 e e i !I t

4i i.

i i, e i e ai 1 2 3 4 6 6 7 8 9 to 3 3 4 6 6 F S 9 to 2 3 4 6 6 7 8 9 to 1 10 100 200 Frequency (Hz) ACCEL NO. 4 V NO.RA SPECIMEN IE TEST AUN NO. AXIS

Ptga No. 38 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY f 0.1 0 1.00 10 0 100$ 1000 0 t 'O I I W I i I i a I i I I l 6-4-- 0 ..-w 4 I 4.... --..--g-- 7 a-M I }, 1 t t 8 t 4 ia, I e i s e 'O O 0 4 ? l~ A O .=; m i A 4 l 1 i . I ... f ...-_w.__ >j

=Il 2 8 i

~W a 1 11 1 [ % ' f , QI) I ' I 3 % ~ T" Y ! 1. I i i V iI' I i i !: i i i I !!3 . I

e' ri'-

'I !' - - iL- '.f g a i .8 I r a. s. i I -%c i( p <g k-l 1 I I { j ] 2g r r + r S S .~. ..n .~7._ n,; e g 8-a. 1 s

  • ~

3 I I 1 I _ [ i i 3 1._ I 1 i -l. t l. i.

i-i a

a . s e r e e so a a e e r e s ie a a ... r. la 1 10 100 200 Frequency & z) SPECIMEN ACCEL NO. DY NO. NA ~ AXIS \\DY TEST AUN NO.

Paga No. 47 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100p 1000 O ~ + _=_-r.. ~__ ___. q __ + 3 y _p 7 y ._n i l I s + -f ? i + i i? 1 l 6 i i i e i i 4 i i 9 m ? i i i

== u_

; p-b:-

r t Id F% _ s __._ 7, L, -._- .y r .;:= -B3 l" E I I W r i m i ,1 1 .t

  • c J'

.\\ I I : s

_r.

, I,

I.

I I i , i 1. L. p 6 I li .I

31..

4.

6.

1 i i I 4. 4 i h 2. 7 i n. 3 8 - a. a _.._ _ _.,__[ l j i t, 6 ! !3 3 ' t i i i 1 .. i, a i i. es i 4 3 4......... Frequency (Hz.) ACCEL NO. MB-- NO. D ~ SPECIMEN IO TEST AUN NO. AXIS

Ptgs No. 40 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY f 0.1 0 1.00 10 $ 100 0 1000 O ^ ' - ' ' * - ~ - e ~ .._:4 ___..-=.. _. = 1 __..__m_.... z ~ 1 - I . i ._4 4 i b e _s. ..d o 4 l l .3.__ ~ h-4: m m ~@ ?) iJ m , ~ 1 i r [ i r ,,i, 1 h 9g _ JI* 1 (_ l 1 4 I e a i e a I 1. Y 1 f: [ I N- .k ' _ _.. -g t_ y.v m._ g-8 us: ee -f

  • .zj;f

-~~ 3fg:-la=== ~~ . ---tes g i_.. t 4M. __ ,, _ _ _ _,. 1x M (4 Jy%i g{ ]- 4 I. _J, l 1 [ 1 i q 3 + 1 i ~ '

j j;

.l., L-l 1 10 100 200 Frequency (Hz) ~ SPECIMEN ACCEL NO. 5 N NO. V@ AXIS VN TEST RUN NO. 3

PAGE NO. 49 TEST REPORT NO. 46623-1 'I APPENDIX II TEST RESPCNSE SPECTRUM PLOTS TEST NO. LEVEL AXES PIDTS 11 OBE Triaxial Control and Response Accelerometers @ 2% damping 12 SSE Triaxial Control and Response Accelerometers @ 3% damping Front-to-Back Horizontal Control Accelerometer FBHCA = Side-to-Side Horizontal Control Accelerometer SSHCA = Vertical Control Accelerometer VCA = WYLE LABORATORIES Huntsydle FacHity

Pr.ga No. 42 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY 0.1 0 1.00 10 0 100 2 10C0 0 .0 N i g i o 7 i i -t- . _ ~ + - ..__7 s 4 r '~'- 4 s y. t 1 i i , 1 1 l i ; e .i 4 i i; 3 =*j e I 3 s i i e e e I ~ t=== 0 i ? I e .w. f /1 ~== ~. ww = _f- _ '.. = _= 8 g _ _.w__ --.f -t----,- _= I 4 .l@ ,/. (._ 1 / L .7 l t f I I C + t r 1 i i i CD 4 3l . i i t i e i i i i p -7 .l. 4 ( i a 1 a.: i r a 8 2 i E I 1a ,. 2,h_. I ag i UW 8 {g,_ . ~. f W-y_ e_ -- m e" 4 I I -9___ 4.. L' I I I I l l - l 1 I [ I 1 + l 1 i ..i 1 2 3 5 6 7 8 9 10 2 4 [6 6 7 8 9 10 2 4 4 6 6 7 8 9 to 1 10 100 200 Frequency (H; SPECIMEN ACCEL NO. I N-N O. ~ Axis EO TEST AUN NO.

a s Page No. 51 Report No. 46623-1 .t i FULL SCALE SHOCK SPECTRUM Ig peak) 1.00 10 & 100 0 100CX3 i 5 DAMPING d 4fo& 13 is e 6 e 7 3, e e e 4 w a e y 1 s s 4 I I r \\' I iiii .i i} I . i i 1 ! k I'I I Ie I i 1-- e t t i l E i f. i i 4 4 i 4 i e i t i e,i, in. i n o I i i 4 6 i ii i i. I ,i - j 4 IT I iii6 eili 1., i i. 66.. ,li i e F-h ,F M, L. T: .,.f e . i 1 i,. i, i e s M ~, t 'i2 e $, [ m i 1 I 1 t i i rIi1 1 3 i i I iI ' i.

1=

8 I lie i I!! I ii!8 I 1 Ii I i i.i ! I I i l i!'i + tit I i .i I I i t 1 I et?! ii? i j i i . it; in. i .,i, u 30 3 u e ta 1 y t s.- e 4 2:2 e a*v 8, s. 3 2 r .i i i-i !ii. I t t i. t i I i l 14 i r 6 s ii i' I f I 1 s.I ! i 1, .. '.u. i, i r I Illi i t! ? 3 i i 6 1 + i. .ii. ii . e e 7 e e so a . e e i e s ie . e e r a s ie 1 10 Frequency (Hz) t S3 NOM SPECIMEN LOCATION NO. Nf TEST RUN NO. // AXIS I

m..

,,,,m_, ,m_.._-~~v...,.-.

Page :o. 44 Report fo. 46623-1 i FULL SCALE TRANSMISSIBILITY ,I 0.1 0 1.00 10 8 100 0 1000 O i. ? ___=w-2- .=__ -.f.__ I 3 ~ W, '~ I I I i i 10 ] ' i i '\\ e i s i i s. n n,, 2 -,4 .e I-1 h l _1 _v .,4 -m i -+ g _.0,.,, i D k' l. = lN NJ ii 't/s I i ,I c J l i n. .i.- i: P i. I i i i 1 I' Ii m - r io, i i p,, i i 4 i r S 1' r, "~ ^ 0 1 a' ^ .1, I I !( -.,I ! I I g g 4__.: 2____=u-- -c l 0,0 ."v'-- .~. s ,i ' gT = m,._._,_.. v =,

==n .-a y __q ] ;i i 1 i L

2 9

3, \\ v. - H l, j i' E L i .r.... r.... 1 10 100 200 Frequency (Hz) SPECIMEN ACCEL NO. N NO.NM FE TEST AUN NO. k AXIS

Paga No. 53 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1.00 10 C 100 D 10000 DAMPING l1%l

  1. G413 e

? .. + - 8 e 4 1 s I I 2 I. I 4 1' 1 E I i ! 3 I ( l i .i ,1 it I f I i !1. I [ 3 f f 3I l!4' i ? j i e!,i i t! ij. t !ii f i!}- i 6 . 4 i3. i, i 6 a 6 6 1 6+ iee.

  • 66 6i 4

6 i 4 i i a i3. I i i e -7 e e i i i i i,, r i r 1 i i i i i i. is S 4 &I 1 E -2 5 I 3 I I II: A i "y h.

I t i i i

l !t! j r a p , i i r 3 e i !!ti 11' I I i l I I 3.. i, j [ l g 1 i3i' f d5 I i ,i f t li! 3 itti i i i i. i, u i i i i. n., i i.n n. o e t. 2 i, ? s , e z. 22 a so al. 4 s i . 1 - I I I 1 ' I]. 6 i i. =.1 1 i.! 'l. 1 1 + 11. i . !I*

li i 9 6i E!

j { j i i ! I!! I i ' I! t !i + 6. i e i 4 6i 1ie i.i4 4 i e. 4e i* i I. , i ;i i . e e i e eio a a 4 e e i a e so a . e e r. io 0 Frequency (Hz) SPECIMEN LOCATION NO. I II AXIS TEI TEST RUN NO.

Page No. 46 Report No. 46623-1 FULL SCALE TRANSMISSIBILITY ( 0.1 0 1.00 10 0 100p 1000 O g 4 --* 7 l l - - +

==;==- _..=..g

= =--- ---- -= = =_. _==. _._== 4 l l s i l l 1 i 6 l .{,. i a i. i i i a + B 2 7 j 6 V4 y W. I L 1 _...= -. _. s _._= = [ 4 r m-l \\' m 1 ar e' s N

M t. I'I I

/ 1 II i f i I I I M, 3 i ..r. 1 ..,, g. ., p 9 n 11 g 3 Z O

r,.
-g a

8 - s ,k i a _e ,I y g 5 l t j_ f 1 ) l a I l 3 i - j ~ I e s l i 8 2 3 4 6 6 7 8 9 to 2 3 4 6 6 F e 9 to 2 3 4 6 6 7 8 9 la 1 10 100 200 Fregt ency (Hz) SPECIMEN ACCEL NO. 6 FB NO. WA ~ FD 4 Axis TEST FIUN NO.

. -. = - - 4 Pago No. 55 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) i 1.0 i 10 qL 100 0 10000 DAMPING l 1%l ,o 9 e ? i , e i i i s i 9 m 9 I3 L 1 .) '.i i i 1 ii i ,Ii I i i i i i ii i!!. i i I t i I t-iI-i i I I I

46 L

i 2 1 1i 3 I.. ii. 4 t 1 i 6i s a i ii .i. a 6 6 3 i 3 1 4434 i i e e i u e i } p c 1 t i 5 i: i i m 1 I i a as i i i 1 iio i

oi i

ii, i 1 lii ii I lit 'if ill f i l t 1 i I I i !!6! t i 4 + 6

i
1i i

e i i 6 1 6 4 4 i .;iI 4 Ili 6 64 i u 2 2 7 -.,1,. p s g.o 8. a T I II l s i ,i i ,n r,! I )I. i I h ll k!I t I

  • 8!

k i i ee iie6 i ai6i e e i i i 6i I,i. 6 4 e i e 3 ie i 6ei i

1.. e io a

a ... r s ie ... r e i. O Frequency (Hd l SPECIMEN LOCATION NO. ~ ll MI TEST RUN NO. AXIS l . -. - -.. -..... ~. -

Page No. 48 Report No. 46623-1 [ I l i This page intentionally left blank. [ I

Paga No. 57 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1.0 0 10 O 100 C!!- 10000 DAMPING l 10/ol Yd6%1 I 7 i ^ s S 4 r I I e o i l I I E 4 i l . ( ' i l k I ..' i i ...i ,.i i l i i ii i.,, m i i. e t 4 s 52 toW O 3 S I c .9 1: i I ! !I i. I I I i, I lI lI 1 .J d i .i! I ..i i. m i 4 l i,, i.n 0 i a.. i., ii ..i l 3,, uo, i i ce 2 7 p 4 I T, e 3= a. I i i i 1 gi4 ,{ j _ I

)I i !

,ii; f e f3 - te i I i !I r 4 , t' l 4 i. i i i ..i i i e

  1. 3 ii 1:

.ii i i a a e e e r e e so a a ... r e so a ... r.,,o Frequency (Hz) t w 8 FA SPEC: MEN LOCATION NO. AX)S I TEST RUN NO. II 1

Paga No. 50 Raport No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1,00 10 5 100 0 10000 4 f,. 6 3 T e L 4 I s f ( / L a, A i x, i .,r n. 4 ,i,, . r i i i,. o, i i xi .i, i ni ei.i i, i,, .r. i s s .I L x-N i,. v. ,r s. , y I i 3 V I __=w r - e 4 ,z 1 s-y .1, v" I A i z . -e _..,a e E., / 2 h M l I,' 7 Ii 1-I 3 i r_s [, i 3

J53, I

3

  • I l

l tI )6 j 6 i l j ii r i.. 6 teti t i ,ni:., i i ; i... i,.i uE,* o e 33 i i i r 1 ir i i ii z h u. G: s a. =., a e 1 i i I 3 i i,ii i 1 i,, i i a ... r e s ie a ... r., io a . e so Frequency (Hz] SPECIMEN LOCATION NO. - F/b NCM ~ AXIS Uf TEST RUN NO. I(

Paga No. 59 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.0 i 10 S 100 i 10000 DAMPING M WGM 10 9 e 7 s S 4 3 4 I 1: a I ,4

s 4
i,

., -u ,!,i .i,.. o 1 ,r. I I. I II\\ ?t ir i.i-3ii! ! t !- 1 =i FF C: i t i i. 4 e iI5* aii ~/' I i.. ie p. 4 i i I iis' i6ii al. i.s ii66 iili .;a i i i 6 i i ii 6 i ri i ,. i e ,~, i s _. l _~- l l 4 l ~ 1, \\ ~~ 2 'h-e2 9

    • '5 1

1 1 1 hi i i I 1 6!. I l I t i 3 i 3 I i ~g 4 i i l' 4 I i i t Ili

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Pags No. 52 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak) 1.00 10 5-100 0 10000 DAMPING l 1%l 44G 3.2 e e ? e . i M 6 i 4 I t r s x , x,.i i i

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Paga No. 61 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.0 i 10 S. 100 0 10000 DAMPING l'R%l n6 2i se 9 s e L ? 4 S 4 y I E 3 ^ ^ L_ g 1 8 g ~ a' t 1 i t, e i i i i 1 i 3 t Y-il i ! i si. 2e i d. i i i i t l 't i i ,1 I 1 !I l'* 1 4i'

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.i Page No. 54 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.0 0 10jiL 100 0 10000 DAMPING d 10 9 ? 6 l .I 4 3 _ _ _ _ _ ~. t i .i. i +> 1

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i Page No. 63 Report No. 4662F1 FUU. SCALE SHOCK SPECTRUM (g peak) 1.00 10 0

1009, 10000 1

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Page No. 56 1 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.00 10 0 100SL 10000 DAMPING l1%l W 6 23 s B 4 s _.Y_ t E i i l,l. l .i .l. 1 . i 1,i m e e r s i je 4 I I s 3 .i. ca i l lll , i; ir i i i,..r i ,1 i i i g i m ii. 4.o m si, i i 3,, i i d' <a U T 2 :* ,i.l z s i i i s '.gu. A s i. i

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Pags No. 65 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g peak) 1.00 10 0 100 S 10000 DAMPING d A/G G 1 3 v. 9 8 7 i 1 i . i e s 4 3 t J. ~ m. 1; +-tv,. l l, 4 u.. i o i!i, n 4 .ii s>> ..i .m i i ... e .o i 1 9 8 7 1 1 I-4 ~E, a 5 a i i 1 i 1 ,o y 3 1 i i i. 3 l. t 3 t i E 2 e i t it. 6 I ! glig si I { lij. I i g i i4 i l E= i

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Page No. 66 Report No. 46623-1 4 FULL SCALE SHdCK SPECTRUM (g Peaki 1.00 10 Q 100 E 10000 l OAMPING l3%l Vleb L3 f, e 7 i a, i e _ e - 4 s a l I 4 i. 4 6 ! 4.,i i,. .,i I f i8 r ,3 ,.i o. i. i, i i i i f, i ~ e t u e w I 1E: 1 .mmy f.

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Paga No. 67 Report No. 46623-1 FULL SCALE SHOCK SPECTRUM (g Peak 3 1.00 10 D 100 g 10000 DAMPING M '/ 6 (, 1 % 10 e e 7 i i, o _ __ e I s I I f f ? } 1 I h I A 1 i[ i i i i. + 1 i . i i 4 i !; i-.. i 6 e ii4 I i Ia e i 3 i ' i e 1 4 4 3 e e e r 1, -v-e 3 2 m 9 r C .9 . i ;

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I Page No. 68 Report No. 46623-1 ( I i i

  • is page intentionally left blank.

l

PAGE NO. 69 TEST REPORT NO. 46623-1 APPENDIX III INSTRUMENTATION LOG SHEETS AND INSTRUMENTATION EQUIPMENT SHEETS All test equipment and instrumentation used in the performance of this test program were calibrated in accordance with Wyle Laboratories' Quality Assurance Policies and Procedures Manual, which conforms to the applicable portions of ANSI N 45.2,10 CFR 50, Appendix B, and Military Specification MIL-STD-45662. Stan-dards used in performing all calibrations are traceable to the National Bureau of Standards. WYLE LABORATORIES MUM 15v6110 Facility -,.. ~

W E2 z? u l'E N :' ? ;0"" R R t } S F ~ \\ } 3" L o L A F / O c o r T T d J Y m 4 o 1 i n n o i a /m m /r r s I c t i / T 7 c u m c c o n 3 i O. R o o 1 E S N E D 3 N E I s G G b e c d A N g n P E n n A m g a r G T h O E s 2 A. 1 S C c O e L T t 0 D E f i 0 E E S o hS C P s J e E E n O A C f T g 3 E a P T t H EH h) t H H n~ S S Co S i l u E t O a E o G I t O O ad A d D a R r ~ E K b S O L Pt ra T n o S C c t A N r,e R en OO bi 6 o t 1 l I r BT me R 1 AA up ? LT Nr 3 ) N e n / A P P A t ut a G G E E E EL E nh m ?r E E E P YM ? R o c T WU l c G G v w W G i C R el T da ic P s S S w N lu E S m E 5 d c n I n R i a o P J E E E-( c S A A d N C ) rn C S i t i ) S 2 3 n I I l S n S L D E S l K o E E L "C R a Y A i. E A u c 3 G 2 M c 1-E L A A L L 1 E I L R T a T M F d F J F ) I I IF E c u u J u m n e T n R R R R 4 C (o M / 2 9 D A E A M 2 4 4 /' I 0 M o 0 0 3 T J b E 1 1 l Y 2_ R E t O M P 2 N O E 2 T T 3 B S A A W O U D E J C F a l 1 i

m ? d w (EuY" x. M / 3 1 tr A T tR F O r 2-R O E N EN E I s e G G e A N g P E n r n a s S C D n G T h O E 3 U L T t f i c hS = e n se T g r~ E n g A E a H h) o o S S Co n o t E t a A D G I rd RO O o Pt L T n A N en r e R O bt i O I r BT me AA up G E. G C C E LT Nr B 1 N e t G A 1 i L E nh D o O o o o E ut YM R o WU l 4 R el da TS u d l N c n F Fa P F 6 F-n I i a m ( 1 [ n m m n h 0 (a R R 7 R Y R 9 R / S A K R A X E 6 E O E 7 E T G 9 G I M L L L L L t E I i F J F n F s f M P d F I I ) ) ) t I R r n u a a u u a R R 2 R R R C 1 7 3 G! E 3 G 4 ) 1 1 2 o M S 0 h I 4 4 s I T 't / 4 8 5 3 1 a I b M 1 1 1 Y 3_ R 3 E M V O 2 N O E 2 L T T 3 B S A E O U D W C F J o t

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A A W I t N T T R A F O 3 R O E N EN E I s 6 G G e A N g P E n h a G T h S C O E L T t f i h S se T g E n E a H h) S Ca S t E t a G rd I O R G a O O W Pt L T n A N en r e ROO bi t BT me [ E r I S M AA up 6 LT Nr 6 N e S E nh 0 E L E ut YM R o WU l N el R da TS u D d P F l N c n n I i a n m ( N e R 2 R 8 O 1 l S 1 # K R I E E A 1 I M L L I I ) E ) F A F R n u u R R E C M_M_ I y S k 9 EM ( 6 T l 6 6 M 4 i t /' 0 R 3 E O M T 2 N O E 2 T T A 3 B S A C O U D W C F J o t M W

je ao s f O", 5. u 't 3 3 3 3 3 3 s 3 3 2 3 7 3 3 3 i3 r 3 T T 3 3 i i w T i 9 Ti h ? 7 T s r l r 5 i T l e 3 D o 2 F o o o 3 3 u r 1 t t t t l t t 1 u i s i s t s E s 1 s 6 t g t n. t i 1 r 7 7 7 7 1 m t 3 3 3 3 5-3 3 3 7 a b ta r h. L, 9 g ?'A 2 W E 3 a-a c C 3 a 3 3 s 3 3 C h v E 3 s m E 3 9 V 1 ? 7 9 t ? 5 r T f o o o 3 n O o 1 7 g u_ u u t t t 2 F t t u t t t m t t \\ i t i t t t 2 P 2 2 2 p a n p t t t t t t t t t T t 1 R 1 s i g 8 t E E D5 y L-t % o E w c o 7 c, r t n s G 6 a 5 S 6 l*5 5 6 r F p ( C r t r a s u w F r F s 5 5 H e s e c t r c A T A r t t 2 A n m m o M m_ mM t S e t s p e y E b_ h y T T i e C= C 6 G G A G T 6 r e h 2 3 e B e (. M 4 ( M 4 l d l n o 0 o o o o o o y-V- ni V v-E V g t e t gn N a o o 0 o o c n o c o o o o v )< O o o o ie R E o c 0 o o o o o c t t t t t t c g i t e s t 1 t l t t t g R M 7 9 P r-d l' 7 4 o o o s 7,- d 3 h r o P o 4 h oN z c i 5 3 P 4 o B e x 3 9, r 9 e i i n 1 W 't 4 4 4 4' l -4 4 s-3 3 d b c I v 4 R k y o o o 4 U c o e l e G t i t 9 5 S 5 5 9 o o o o o o o o o o o x t n Q em t t l ?r E 3 ? R 3 -c 3 5 6 1 e ta d o 4 o o d 3 b A {A A (A A A A A,h 3 1 n o, o Ts eN N 2' G A A A A T 6 T g N n M a N u4 M S l l { l k l, ,c O 6, L E d M M u J 3 U B } T E o o o O B O S e D D S D IT 4 T l 2 a-3 p 2 o o o s t t ) i s e. 7 i 1 t t l ) t t A d o 1 7 1 d 4 d r 2 z t_ 2 z t 2 2 2-o N r 7 i. n 7. 7 1-7 7-A 2 A M 7 r o o o T m 2 3 e J" p 2 p n 7 2 2 2 2 2 2 2 r 2 r o N o T 9 1 N t b s E o u J C o o o

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M o o o e-o o_ o o D o o_ c c C o t t t ( c e t c c t r c 9 v N u e v u v q c c c dr c V V r v y V V N U u v s t E c c e c e fi M c c c E E c e e a r s R f o c o 0 O 0 O o O D o O p 0 u o n t O n M u M u u u M x M t 1 3 o u u m u u x M T a M S v r S e e E G e E e e E G E c c E e e e N n L a 2 E P e-I 2 t E F D i e e u w w_w f r / l_ )4 f f f 8 p M ) d e n 2 b m % u e r t e T m a e e e y c w c a m A n w o 8 t r i / t 1 r A 4 m A A A A A d t t s o n m w m n n n t t h a 1 e t o n R e o c o o o m r r C u R t z t M (4 E-C z E, e A F R z t E R. t r e r e m t E_ e c. c z E c e s i s s c L 6 c G u. R(~ n ( o i w z 2 2 2 d r v s (2 z t t t t t t 0-e e e a e e a e A A A A a A A A A s R 2 f f t e s 1 / r I c c c c r c c c n 6 A 4 t l 1 A d t n M c c c c c c c c i I i s 4 a c O e C c 9 i A A A \\ A A A A A C d e ic 2 t 0 n 2 4 6 p 6 o t h a 7 3~ 4 5 (- 7 S 1 1 e l i t l' ( t 1 1 t c N t t 1 i 1 a e 3 D T 1

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PAGE NO. 75 TEST REPORT NO. 46623-1 APPENDIX IV SEISMIC TEST PROCEDURE ( WYLE LABORATORIES Huntsville Facility

- -. _ _. _,.. ~ -. - - _ - -

Page No. 76 Report No. 46623-1 541/8498-1/WB TEST PROCEDURE NO. s scianriric samviCas a systEus oaoue e o. som ions. m,ai n - aiact January 21, 1983 ueonsomes twmeim r2+222s. itLErnont aos asrun DATE: Revision A J/N 4f623 SEISMIC TEST PROCEDURE FOR A HOT SHUTDOWN PANEL (TAG NO. CP2-ECPRLV-01) FOR RELIANCE ELECTRIC S ENE MOUNTAIN, GEORGIA (REFERENCE #99AX400404) F A E M NAGER: M# M ~ ~ APPROVED BY: APPROVED BY FOR: QUAUTY ENGINEER-APPROVED BY: PREPARED BY FOR: PROJECT ENGINEER: W l REVISIONS A l REv. NO. CATE ,A E5 A,,ECTEC A,n. OESCRi,r:0N O,C AN E5 A 2-10-83 All BQ gp Complete revision per Customer / (M' request. l l 1 l 1 COPYRIGHT By wvLE LA80RATORIES. THE RIGHT TO REPRODUCE. COPY, EXHIBIT, OR OTHERwlSE UTILIZE ANv OF THE MATERIAL CONTAINED HEREI WITHOUT THE EXPRESS PRIOR RERMISSION OF WY6E LABORATORIES 15 PROHIBITED. THE ACCEPTANCE OF A PURCHAS THE MATERIAL CONTAINED MEREIN SMALL SE EQUIVALENT TO EXPRESS PRIOR PERMISSION. 4

Paga No. 77 Report No. 46623-1 PAGE NO 2 TEST PROCEDURE NO. 541/8498-1/WB Revision A 1.0 MOUNTING 1.1 Specimen orientation and Tie-Down A Hot Shutdown Panel,140"L x 42"D x 90"H, weighing approximately 8000 pounds, hereinafter called the specimen, shall be placed on the Wyle Multiaxis Seismic simulator Table. The specimen shall be oriented such that its horizontal axes shall be colinear with the table's horizontal axes of excitation. The specimen shall be welded to a Wyle-fabricated base-mounting fixture with 1/4" fillet welds, 4 inches long on 12-inch centers. Mounting of the specimen shall simulate its actual in-service con-figuration as closely as practical. The test fixture shall be welded to the test table. 2.0 EXCITATION 2.1 Simultaneous Triaxial Excitation Both horizontal axes and the vertical axis shall be excited separately, but simultaneously. The input acceleration level for each of the three axes shall be phase incoherent during the multifrequency tests. 2.2 Resonance Search A low-level (approximately 0.2 g) single-axis sine sweep shall be performed in the three orthogonal axes from 1 Hz to 50 Hz to determine major resonances. The sweep rate shall be two octaves per minute. Transmissibility plots of the specimen-mounted accelerometers from 1 Hz to 50 Hz shall be provided in the test report. The side panel shall be removed following the resonance search tests. 2.3 Random Multifrequency Tests The specimen shall be subjected to 30-second duration triaxial multi-frequency random motion which shall be amplitude-controlled in one-third octave bandwidths spaced one-third octave apart over the frequency range of 1 to 40 Hz. Three simultaneous, but independent, random signals shall be used as the excitation to produce phase-incoherent motions in the vertical and two horizontal axes. The amplitude of each one-third octave bandwidth shall be independently adjusted in each of the three axes until the Test Response Spectra (TRS) envelop the Required Pesponse Spectra (RRS). The resulting table motion shall be analyzed by a response spectrum analyzer at two percent (2s) damping for the Operating Basis Earthquake (CBE) tests and at three percent (3%) damping for the Safe Shutdown Earthquake (SSE) test, and plotted at one-sixth octave intervals over the frequency range of 1 to 200 Hz. WYLE LABORATORIES

  • 1050 a" Oct M Hunt 5velle F4Clisfy

1 e Page No. 78 Report No. 46623-1 PAGE NO 3 TEST PROCEDURE NO. 541/9498-1/WB Revision A [ 2.0 EXCITATICN (Continued) 2.3 Random Multifrequency Tests (Continued) Five (5) OBE tests, followed by one (1) SSE test, shall be performed. The CBE and SSE RRS are shown in Figures 1 through 4, respectively. i 3.0 INSTRCMENTATICN All test equipment and instrumentation to be used in the performance of this test program shall be calibrated in accordance with Wyle Laboratories' (Eastern Operations) Quality Assurance Policies and Procedures Manual, which conforms to the applicable portions of ANSI N 45.2,10 CFR 50, Appendix B, and Military Specification MIL-STD-45662. Standards used in performing all calibrations are l traceable to the National Bureau of Standards. 3.1 Excitation Control Control accelerometers shall be mounted on the test table at a location near the base of the specimen. TRS plots (filtered at 100 Hz) of the control accelerometers from the OBE tests at 2% [ damping, and the SSE test at 3% damping, shall be provided in the I test report. 3.2 Specimen Response A total of six (6) uniaxial piezoelectric accelerometers shall be provided for the specimen. The placement of the accelerometers shall } be at the discretion of the Reliance Technical Representative. Magnetic tape shall provide a record of each accelerometer response. A TRS plot (filtered at 100 Hz) from each specimen response accelerometer from a selected CBE test and the SSE test, at the test damping, shall be provided in the test report. 4.0 IN-PROCESS INSPECTION } The records shall be checked for quality of performance after each test. 1 The specimen shall be examined for possible damage and weld, failure following all violent tests. All important vibration effects shall be logged. Photographs shall be taken of any noticeable physical damage and weld failures that may occur. WYLE LABORATORIES

  • '05* 7 aa oci is Huntsysile FaCahty y

Pags No. 79 Raport No. 46623-1 PAGE NO 4 TEST PROCEDURE NO. 541/9499-1/WB Revision A 5.0 REPORT Ten (10) copies of a certification-type test report shall be issued subsequent to completion of testing. This report shall be signed by a Registered Professional Engineer and shall summarize the response spectrum plota of the table motion, results and conclusions, details and recomendations concerning deficiencies and repairs, and photographs of test setups, failures, etc. TRS plots of the control accelerometers from the OBE and SSE tests shall be included. The RRS shall also be included. The report shall also contain a list of test equipment used, calibrations, and Instrumenta-tion Log Sheets. 1 i i i l WYLE LABORATORIES

  1. cau 24 7 an mi N Huntsville Facinty

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