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Pioneer F/G Feed Movement MechanismThe Pioneer F/G spacecraft achieves the desired earth-pointing direction through a system requiring the shifting of the main antenna feed 1 in. off axis. The feed is pivoted to this position by an electrically heated thermal actuator consisting of an electroless nickel bellows in a copper housing and filled with Freon 21. The actuator overtravels and maintains the feed in the offset position in a thermostatic limit cycle operation mode until commanded off. The mechanism is expected to operate in a -240 F environment near Jupiter and was successfully tested at such temperatures.
Document ID
19720018731
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
R. M. Acker
(TRW Systems Group Redondo Beach, CA, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Publication Information
Publication: 6th Aerospace Mechanisms Symposium
Publisher: Ames Research Center
Volume: NASA-TM-X-2557
Issue Publication Date: June 1, 1972
Subject Category
Machine Elements And Processes
Report/Patent Number
A-4047
Meeting Information
Meeting: 6th Aerospace Mechanisms Symposium
Location: Moffett Field, CA
Country: US
Start Date: September 9, 1971
End Date: September 10, 1971
Sponsors: Ames Research Center
Accession Number
72N26381
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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