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Deployment/retraction mechanism for solar maximum mission high gain antenna systemA mechanism called a deployment/retraction assembly (DRA) which provides not only a stable, but a deployable platform for the high gain antenna system (HGAS) aboard the Solar Maximum Mission (SMM) spacecraft is described. The DRA also has the capability to retract the system upon command.
Document ID
19790013199
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bennett, N. (Sperry Flight Systems Phoenix, AZ, United States)
Preiswerk, P. (Astro Res. Corp. Santa Barbara, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
April 1, 1979
Publication Information
Publication: NASA. Ames Res. Center The 12th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
79N21370
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19790013181Collected WorksThe 12th Aerospace Mechanisms Symposium
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