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Shock response spectra variational analysis for pyrotechnic qualification testing of flight hardwareShock response spectra data from flight certification tests were analyzed to determine envelope variation with respect to mean values in each axis. An overall variation of + or - 8.61 dB or 169 percent exists for the data. This large variation may be attributed to one or more of the following: (1) Instrumentation problems may exist. (2) Variations in the source charge (blasting caps) such as shape or explosive load may exist. (3) Two blasting caps were used to excite the pyrotechnic plate tester. Delay time between charge firings may have varied. The cause or causes of the variations need to be identified and researched to prevent future pyroshock problems.
Document ID
19840015608
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Smith, J. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TP-2315
NAS 1.60:2315
Report Number: NASA-TP-2315
Report Number: NAS 1.60:2315
Accession Number
84N23676
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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