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A simultaneous spin/eject mechanism for aerospace payloadsA simultaneous spin/eject mechanism was developed for aerospace applications requiring a compact, passive device which would accommodate payload support and controlled-release functions, and which would provide a highly accurate spin-ejection motion to the payload. The mechanism satisfied the requirements and is adaptable to other deployment applications.
Document ID
19760021200
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Palmer, G. D. (TRW Systems Group Redondo Beach, CA, United States)
Banks, T. N. (AVCO System Div.)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: JPL 10th Aerospace Mech. Symp.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N28288
Funding Number(s)
CONTRACT_GRANT: F04701-74-C-0328
CONTRACT_GRANT: F04701-74-C-0326
CONTRACT_GRANT: F04701-74-C-0325
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19760021184Collected WorksTenth Aerospace Mechanisms Symposium
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