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Design and development of a linear thermal actuatorThe design and development of a linear thermal actuator (LTA) for space applications is described. The actuator is driven by thermal energy and utilizes the property of thermal expansion to do work. Equations to predict performance are developed and used to optimize the design of the development model LTA. Design details and test results are presented and discussed.
Document ID
19850025205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bush, G.
(Spar Aerospace Ltd. Sainte-Anne-de-Bellevue Quebec, Canada)
Osborne, D.
(Spar Aerospace Ltd. Sainte-Anne-de-Bellevue Quebec, Canada)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: NASA. Ames Research Center 19th Aerospace Mech. Symp.
Subject Category
Structural Mechanics
Accession Number
85N33518
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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