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Delayed simultaneous release mechanismThe disclosed appendage release mechanism is particularly adapted for use with spacecraft operating with despin mechanisms and releasable appendages. It includes a flexible loop and a number of appendage releasing devices which are attached to the flexible loop. The appendage releasing devices are made up of piston-cams and ball latches which hold the appendages as long as the flexible loop is maintained in a taut condition, but which release the appendages upon relaxation of the flexible loop. The flexible loop remains taut as long as the despin weights remain attached, but relaxes when the despin weights are released.
Document ID
19730011312
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Moyer, X. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Webb, J. B.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
February 6, 1973
Subject Category
Auxiliary Systems
Report/Patent Number
Patent Number: NASA-CASE-GSC-10814-1
Patent Number: US-PATENT-3,715,092
Patent Application Number: US-PATENT-APPL-SN-41404
Accession Number
73N20039
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-GSC-10814-1|US-PATENT-3,715,092
Patent Application
US-PATENT-APPL-SN-41404
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