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The linear boom actuator designed for the Galileo spacecraftBecause the linear boom actuator is to be used on a flight spacecraft, as opposed to a ground based application, there is a comprehensive set of requirements. First, of course, the actuator must be capable of positioning and holding the load. Initially the load as predicted to be 4448 N (1000 lb) but with subsequent spacecraft configuration changes the load has been greatly reduced to a constant tensile pull of 1477 N (332 lb) due to centrifugal force. Lesser compressive loads of 1317 N (296 centrifugal lb) may be experienced during launch and deployment. This actuator must have the maximum redundancy possible. Life requirements were defined by the 10.16 to 15.24 cm (4 to 6 in.) total liner travel expected during the five-year flight duration. Liner range required of the actuator was set at plus and minus 5.08 cm to accommodate configuration changes.
Document ID
19830016615
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Koch, E. F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1983
Publication Information
Publication: The 17th Aerospace Mech. Symp.
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
83N24886
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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