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STS payload retention system conceptA payload retention concept that may be utilized on Space Shuttle missions is investigated. This concept appears to embody all the desirable features for the very demanding requirements for space flight. Desirable features include light weight, low cost, high reliability, excellent load distribution, versatility, and insensitivity to critical alignment.
Document ID
19830005881
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clark, K. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Space Transportation
Report/Patent Number
NAS 1.15:82505
NASA-TM-82505
Report Number: NAS 1.15:82505
Report Number: NASA-TM-82505
Accession Number
83N14152
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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