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Space Shuttle S-band antenna systemThe NASA Space Shuttle Orbiter presents some very challenging antenna design problems for the S-band Orbiter to ground and Orbiter to relay satellite communications links. The line of sight to the ground and/or relay satellite during the various mission phases dictates an almost omni-directional coverage requirement, but the circuit margins require at least a 3 dB gain over this same coverage region. In addition, the environmental conditions imposed by the Orbiter mission dictate a flush mounted rugged antenna design. A number of potential antenna designs have been evaluated and found not to meet the Orbiter requirements. A small passive array of cavity backed spirals was found to offer the most potential to meet the design requirements. New circuit margin requirements presently under study have forced the consideration of the use of an active transmit/receive phased array design that considerably complicates the antenna design, but provides more than 10 dB of additional gain for circuit margin improvement.
Document ID
19750035401
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Walton, M. D.
Cubley, H. D.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Meeting Information
Meeting: National Telecommunications Conference
Location: San Diego, CA
Start Date: December 2, 1974
End Date: December 4, 1974
Accession Number
75A19473
Distribution Limits
Public
Copyright
Other

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