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Selection of an optimal plan for construction of a spacecraft antenna systemAn attempt is made to summarize the experience of the design of antennas for various types of spacecraft: fully oriented, partially oriented, and with arbitrary orientation. Several examples of the construction of antenna systems and their characteristics are given. The optimal relationship between weight, dimension and power characteristics of on-board devices allows selection of the most acceptable versions. Questions are presented for consideration in design of optimal spacecraft antenna-feeder systems.
Document ID
19750002926
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Prigoda, B. A. (Kanner (Leo) Associates Redwood City, CA, United States)
Faynshteyn, M. B. (Kanner (Leo) Associates Redwood City, CA, United States)
Guryev, V. A. (Kanner (Leo) Associates Redwood City, CA, United States)
Markin, A. S. (Kanner (Leo) Associates Redwood City, CA, United States)
Date Acquired
August 8, 2013
Publication Date
October 1, 1974
Publication Information
Publication: Equipment for Space Res. (NASA-TT-F-785)
Subject Category
Communications And Radar
Accession Number
75N10998
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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