ML20073N917
| ML20073N917 | |
| Person / Time | |
|---|---|
| Site: | San Onofre  |
| Issue date: | 07/05/1979 |
| From: | Casaubon M, Esposito B, Gilfoy R ACTON ENVIRONMENTAL TESTING CORP. |
| To: | |
| Shared Package | |
| ML13309B258 | List: |
| References | |
| 14950, NUDOCS 8304220588 | |
| Download: ML20073N917 (22) | |
Text
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No. 14950 l
Test Procedure ii
.!.i SEISMIC VIBRATION TESTING OF GNE (1) HYOR0 GEN ANALYZER ASSEMBLY 4
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GENERAL ELECTRIC SPACE SYSTEMS
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VALLEY FORGE SPACE CENTER UNCER PURCHASE ORDER NO. A28000A10155 Prepared b M <p p hm Date C/92,[
Bruce Esposita', Proje~ct Engineer
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Acton Environmental Testing Corporatten/ g /
533 Main St., Acton, MA 01720 Reviewed by:
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e Date 7Idr '7 f
'R4cnarc Gilfoy Jr., Ahief tynamics Engineer Acton Environmental Testing Corporation Reviewed by:278 tee /d dmd 440 ate _ 7 /"/74 Marcel E. Casaubon, Section Leader Acton Environment T *ing Corporation 7/i 77 Approved by:
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Date Marvin L. Tolf, Preside ActonEnvironmentalTes~p I
ing Corporation Approved by:
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j Gerkfal E,lectric Space Systems
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3 Valley Forge Space Center, King of Prussia, PA 3
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Y.1C 8304220588 830420 PDR ADOCK 05000361 P
1.0 TEST ITEM One (1) Hydrogen Analyzer Assembly P/N 47E240609 consisting of one (1) free standing enclosure apprcximately 72-1/16" X 25-1/16" X 31-9/16" containing signal conditioning for hydrogen analyzers, one '
(1) hydrogen sensor and one (1) pressure transducer with a total
- N weight of approximately 660 lbs will be submitted by General Elec-st ' '
.4 tric Space Systems, Valley Forge Space Center for seismic vibration s
testing at Acton Environmental Testing Corporation (AETC).
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Test Procedure No.
Page componA m F-17 i
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2.0 TEST REQUIREMENTS The purpose of this test is to subject the panel specified in section 1.0 above to the seismic vibration test specified in sectim 3.0 below to determine its ability to withstand such
'I vibration without evidence cf mechanical damage, deterioration,
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.I or loss of its ability to operate properly during or after the f
simulated seismic event.
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3.0 TEST PROCEDURES
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.3.1 1EST MOUNTING The hydrogen analyzer assembly specified in section 1.0 above will be mounted to a test fixture fabricated from structural
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steel.
The test fixture will then be securely attached to the if N
45* biaxial table of the AETC Seismic Test facility. The use
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j of the 45' biaxial. table results in equal horizontal and verti-cal components.
3.2~ TEST' MONITORING The hydrogen analyzer assembly will be monitored with triaxial groups of accelerometers to determine its mechanical response during the resonance survey and multiple frequency tests speci-fied in sections 3.4 and 3.5 below.
One(1)controlacceleraneter will be mounted on the test fixture.
Up to eleven (11) monitor-ing accelerometers will be located on the hydrogen analyzer il 3
assembly / test fixture assembly at locations to be detennined at
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the time of test.
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b During the resonance survey, data fran all twelve (12) accelero-meters through appropriate signal conditioning,will be recorded Test Procedure No.
14950 S023-508-17-18-0
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onto visicorder recording paper to be included with the final test, report and cnto magnetic tape.
During the multiple frequency test specified in section 3.5 belew, data from all twelve (12) accelerometers, through appropriate q
signal conditioning will be recorded onto magnetic tape.
Data from the one (1) control accelerometer will also be analyzed on 1
line by a Spectral Dynamics SD321 Shock Spectrum Analyzer and the L y; X-Y plots of the Test Response Spectra (TRS) of the control accel-erometer will be indluded as part of the final test report.
The hydrogen analyzer assembly will be visually monitored for any evidence of mechanical damage or deterioration.
General Electric personnel will monitor the hydrogen analyzer assembly performance.
General Electric will supply the required performance monitoring equipment including gas. AETC will supply l
two (2) channels of brush recorders.
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f 3.3 TEST CONDITIONS E
Q The hydrogen analyzer assembly will be tested at room temperature, t
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During the resonance survey specified in~section 3.4, the hydrogen I
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Test Precedure No.
14950 l
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CC8moRATioM F-20 e em m
analyzer assembly will not be operational.
During the multipi,e frequency test specified in section 3.5 below, the hydrogen analyzer assembly hd11 be operational, All electrical and operating test conditions will be set and controlled by General Electric personnel.
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Acton Environmental Testing Corporation (AETC) will supply 115 VAC, u
j single-phase, 60 Hz power and 220 VAC 3-phase power.
3.4 RESONANCE SURVEY The resonance survey will consist of a biaxial sinusoidal input with peak horizontal and vertical accelerations of 0.2g's at fre-(
quencies from 1.0 through 35.0 Hz. The resonance survey will be performed at a sweep rate of 1/2 octave / minute. The input will be applied in two biaxial directions of excitation as follows:
' TEST'NO.
BIAXIAL DIRECTION OF EXCITATION 1
Front-to-back & Vertical a
2 Right-to-left & Vertical 1.
f3 3.5 MULTIPLE FRE00ENCY TEST ii 5
A biaxial multiple frequency excitation will be applied.
The 14950 Test Procedun3 No.
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S023-506-17-18-0 5
i ACTON Page cxwwTxm F-21
test input will be recorded on a 14-channel tape. recorder,.
each track having discrete frequency sine beats recorded at a dif'ferent frequency and delay between beats.
All frequencies will be recorded at maximum levels.
The input will be played back through a 14-ch'annel tape re-i corder.
The output.s of the 14 channels will then be combined i
in a 14-channel mixer which will result in a multiple fre-quency output.
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The individual mixer channels will have gain controls so that the level of each output tape channel passing through the mixer can be controlled.
In this manner, the required test spectrum can be shaped by controlling the level of individual fre-quencies.
Qualification tests, consisting of biaxial periodic pseudo-random excitation, will be performed. The level of the periedic pseudo-random excitation will be such that the Test Response Spectra (TRS), frcm the control acceleraneter will envelop the I
appropriate Required Response Spectra (RRS) shown in Figure 1, 8
except where limited by AETC shaker table capabilities.
14950 Test Procedure No. '-
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resne<2 Page comoum F-22
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The input will be appl'ied six (6) times in each of four (4) biaxial directions of excitations as follows:
' TEST NO.
BIAXIAL DIRECTION OF EXCITATION 3
Right-to-left & Vertical 4
Back-to-front & Vertical
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5 Left-to-right & Vertical ij 6
Front-to-back & Vertical The test duration for each input will be thirty (30) seconds.
The level of the first five (5) inputs in.each biaxial direction i
will be such that the TRS fran the control accelercrneter computed at Q=10,:(5% damping) will envelop the OBE RRS shown in Figure 1, except where limited by AETC shaker table capabilities. The level of the sixth input in each biaxial direction will be such that the TRS computed at Q=10 (5% damping) will envelop the SSE RRS shown in Figure 1, except where limited by AETC shaker table capabili-ties.
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Figure 1 is a composite curve of. Revisions A of sketches.5023-SK-S-I k
655, SO23-SK-S-656, 5023-SX-S-633, 5023-SK-S-634, 5023-SK-S-739, 5023-SK-S-725, 5023-SK-737 and 5023-SX-5-701 of Revision 1 of 14950 Test Procedure No.
S023 -50 E -l ?- 15 -0 n.
Page F-23
of Appendix 4F " Criteria For Seismic Qualification of Seismic Class.1 Equipment", dated July 20, 1973.
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The test' report will include but not be limited to a detailed des-cription of the test item, requirements, procedures, mounting,
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monitoring, test descriptions and test results.
The test results section of the final report will include the X-Y plots of the Test
( '.1 Response Spectra. for the control acceleranater.
A test equipment l y list and photographs of the test setup and accelerometer locations 1
5 will also be included in the test report. The visicorder chart ut recordings of. the t-esonance survey will be sent along with the final report.
The test report will be presented in the same general fomat as this test procedure.
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