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SERT 2 gimbal systemThe gimbal system is described that was designed to mount the thruster and to reposition the thrust vector of a mercury ion bombardment thruster through the center of gravity of the SERT 2 assembly. The SERT 2 assembly was launched 3 February 1970. The gimbal ring, gimbal mounts, bearings, actuators, and environmental testing are described. Due to the accurate alinements provided, it was not necessary to use the gimbal for the intended function. However, the gimbals were operated successfully numerous times in space after 8 months of storage.
Document ID
19720005264
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Zavesky, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Hurst, E. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-2427
E-6449
Report Number: NASA-TM-X-2427
Report Number: E-6449
Accession Number
72N12913
Funding Number(s)
PROJECT: RTOP 164-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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