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Design study for a liquid metal slip ring solar array orientation mechanismThe design of a single axis orientation mechanism for solar arrays on high power synchronous satellites is studied primarily with respect to providing 116 liquid metal slip rings for reduced friction and improved electrical characteristics. Designs and tradeoff studies for the slip rings and other components are presented. An assembly containing 33 slip rings of three design approaches was designed, fabricated, and vacuum tested to 30 amperes and 30,000 volts. Containment of the liquid metal gallium in large diameter slip rings was difficult. A design approach is presented which is expected to provide improved retention of the liquid metal.
Document ID
19730004488
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Clark, R. B.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 30, 1972
Subject Category
Electronic Equipment
Report/Patent Number
NASA-CR-120954
Report Number: NASA-CR-120954
Accession Number
73N13215
Funding Number(s)
CONTRACT_GRANT: NAS3-13731
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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