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Offset wrap rib antenna concept developmentThe demonstration of 50 to 150 m, STS compatible, offset antenna technology readiness is reported. Fabrication of a ground and flight testable partial 55 m reflector section and feed support structure is discussed. Reduction to practice through ground test verification is presently contained in the program. Key objectives for the program include the design of a compatible feed support structure and the fabrication and testing of critical components.
Document ID
19820011385
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Woods, A. A., Jr. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Garcia, N. F. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., Pt. 2, 1981
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
82N19259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19820011383Collected WorksLarge Space Systems Technology, Part 2, 1981
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