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Appendange deployment mechanism for the Hubble Space Telescope programThe key requirements, a design overview, development testing (qualification levels), and two problems and their solutions resolved during the mechanism development testing phase are presented. The mechanism described herein has demonstrated its capability to deploy/restow two large Hubble Space Telescope deployable appendages in a varying but controlled manner.
Document ID
19850025220
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Greenfield, H. T. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: NASA. Ames Research Center 19th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
85N33533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19850025199Collected WorksNinteenth Aerospace Mechanisms Symposium
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