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A release mechanism with mechanical redundancyA simple release mechanism is described that achieves high reliability through active mechanical redundancy on the SERT 2 satellite. Principle of operation, design details, and the test program are discussed. Examples of developmental and proposed alternate configurations also are included.
Document ID
19720005757
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Paradise, J. J. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: NASA. Goddard Space Flight Center 5th Aerospace Mech. Symp.
Subject Category
Machine Elements And Processes
Accession Number
72N13406
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19720005742Collected WorksFifth Aerospace Mechanisms SymposiumN72-13391 04-15Collected Works
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