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A technology development program for large space antennasThe design and application of the offset wrap rib and the maypole (hoop/column) antenna configurations are described. The NASA mission model that generically categorizes the classes of user requirements, as well as the methods used to determine critical technologies and requirements are discussed. Performance estimates for the mesh deployable antenna selected for development are presented.
Document ID
19810003645
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Russell, R. A. (NASA Langley Research Center Hampton, VA, United States)
Campbell, T. G. (NASA Langley Research Center Hampton, VA, United States)
Freeland, R. E. (JPL)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81902
IAF-80-A-33
Meeting Information
Meeting: Intern. Astronautical Congr. of the Intern. Astronautical Federation,
Location: Tokyo
Country: Japan
Start Date: September 21, 1980
End Date: September 28, 1980
Accession Number
81N12155
Funding Number(s)
PROJECT: RTOP 506-62-43-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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