NASA NTRS · 20020073837
A Precision, Thermally-Activated Driver for Space Application
Abstract
This 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.
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Murray, Robert C., Walsh, Robert F., Kinard, William H.. 1986-05-01. A Precision, Thermally-Activated Driver for Space Application. https://ntrs.nasa.gov/citations/20020073837
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