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A Precision, Thermally-Activated Driver for Space ApplicationThis paper describes a space qualified, precision, large force, thermally activated driver that has been developed jointly by the NASA Langley Research Center and PRC Kentron. The driver consists of a sealed hydraulic cylinder containing a metal bellows, a bellows plug, a coil spring, a spring retainer, an output shaft, a shaft guide, and a quantity of silicone oil. Temperature changes cause the silicone oil to expand or contract thus contracting or expanding the bellows/spring assembly thereby extending or retracting the output shaft.
Document ID
20020073837
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Murray, Robert C.
(PRC Kentron, Inc. Hampton, VA United States)
Walsh, Robert F.
(PRC Kentron, Inc. Hampton, VA United States)
Kinard, William H.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 20, 2013
Publication Date
May 1, 1986
Publication Information
Publication: 20th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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