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Feasibility study of a step scanned omnidirectional communications antenna for an international magnetospheric explorer spacecraftThe results of this study has indicated that omnidirectional antennas requiring directive gains steered off broadside are limited by the feed system efficiencies. The directive gain can be increased to offset the feed losses, but this approach leads quickly to diminishing returns. While gains of 4.8 db appear feasible, a system gain of 3.0 db is considered practical. These results apply to antenna configurations limited in packaging volume to 10 cm diameter by 61 cm length.
Document ID
19750006888
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Herskind, R. E.
(Avco Corp. Wilmington, MA, United States)
Date Acquired
September 3, 2013
Publication Date
October 28, 1974
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-CR-139161
AVSD-0298-74-RR
Report Number: NASA-CR-139161
Report Number: AVSD-0298-74-RR
Accession Number
75N14960
Funding Number(s)
CONTRACT_GRANT: NAS5-20020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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