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A foldable 4.27 meter (14 foot) spacecraft antennaThe problems and solutions associated with the design, fabrication, and testing of a large, lightweight, radial-rib, folding, spacecraft antenna reflector are discussed. The antenna reflector was designed as a highly efficient communications system for outer-planet missions extending as far as approximately 59.839 x 10 to the 11th power meters (40 astronomical units) from the sun. The methods used to obtain a lightweight precision rib surface, the evaluation and fabrication of the metallic reflector mesh surface, and the surface-evaluation techniques used on the assembled antenna reflector are included.
Document ID
19730010143
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Starkey, D. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1972
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center The 7th Aerospace Mech. Symp.
Subject Category
Electronic Equipment
Accession Number
73N18870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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