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Design tradeoff study for reflector antenna systems for the shuttle imaging microwave systemA general tradeoff is made of the symmetric Cassegrain antenna with regard to the possibility of meeting a 90% beam efficiency. The effects of aperture taper and blockage are calculated using an adjustable sidelobe circular distribution. Numerical integration is used. For the feed spillover calculation, a low sidelobe symmetric feed pattern is used with the equivalent parabola and numerical integration. Reflector cross polarization is calculated using double numerical integration. Reflector back lobes are estimated from radiation pattern envelopes of commercial common carrier dish antennas. The curves allow a range of f/D to be determined for a specified edge taper and blockage diameter ratio, and with a table of Cassegrain parameters, a range of possible designs that meet the 90% beam efficiency is obtained. It is shown that the feed and reflector design and implementation must be carefully done.
Document ID
19750006868
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hansen, R. C.
(Hansen (R. C.), Inc. Encino, CA, United States)
Date Acquired
September 3, 2013
Publication Date
August 30, 1974
Subject Category
Communications And Radar
Report/Patent Number
FR-636-1
NASA-CR-140915
Report Number: FR-636-1
Report Number: NASA-CR-140915
Accession Number
75N14940
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-954026
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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