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A precision, thermally-activated driver for space applicationA space qualified, precision, large force, thermally-activated driver that has been developed jointly by the NASA Langley Research Center and PRC Kentron is described. The driver consists of a sealed hydraulic cylinder containing a metal bellows, a bellows plug, a coil spring, a spring retainer, and 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
19870006904
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murray, Robert C.
(PRC Kentron, Inc. Hampton, Va., United States)
Walsh, Robert F.
(NASA Langley Research Center Hampton, VA, United States)
Kinard, William H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA. Lewis Research Center The 20th Aerospace Mechanics Symposium
Subject Category
Mechanical Engineering
Accession Number
87N16337
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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