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Latch mechanism for the space telescopeLatch mechanisms to secure, release, and relatch deployables on the Space Telescope are described. The latch mechanisms are mechanical pre-loading devices composed of a four-bar linkage driven by an electro-mechanical rotary actuator. The latch mechanism requirements, unique design features, analytical highlights, and the development testing are discussed.
Document ID
19810013879
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmidt, H. F. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: NASA. Marshall Space Flight Center The 15th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
81N22410
Funding Number(s)
CONTRACT_GRANT: NAS8-32697
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19810013857Collected Works15th Aerospace Mechanisms Symposium
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