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Space payload dynamic testingMore cost effective methods for insuring payload reliability are required to efficiently utilize the projected payload capacity of future space systems such as the Space Shuttle. Studies are needed to better define the vibration environment of space vehicles to develop improved and more routine methods of testing and to develop better dynamic protection systems. Such improvements in environment definition, testing, and isolation will lead to less stringent design specification, improved payload reliability, fewer and more realistic qualification and flight acceptance tests. This paper presents current payload test philosophies, effectiveness of testing, and research needed to achieve more cost effective payload reliability for future applications.
Document ID
19750034068
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Pinson, L. D.
Stephens, D. G.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Reliability design for vibroacoustic environments; Winter Annual Meeting
Location: New York, NY
Start Date: November 17, 1974
End Date: November 21, 1974
Accession Number
75A18140
Distribution Limits
Public
Copyright
Other

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