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Design and test of a low-temperature liner driver/rate controllerThe design and testing of a force/rate control device used to deploy an Earth shield on an orbiting satellite is described. Test experience, failure modes, and applications are emphasized.
Document ID
19840017015
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lowry, C. H. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1984
Publication Information
Publication: The 18th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
84N25083
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19840017010Collected WorksThe 18th Aerospace Mechanisms Symposium
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