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32 GHz deep space communicationsThe present analysis of the use of a 32-GHz (Ka-band) downlink for deep space communications notes significant benefits over current standard 8.4-GHz downlinks; the consequences of the 8-dB telemetry performance gain thus obtained is presently evaluated for the case of the Cassini and Mars Sample Return missions. This potential can only be realized, however, with upgradings of both the ground stations in the Deep Space Network and the spacecraft communications subsystem. Proposals are made for the use of a Ka-band beacon on the Mars observer spacecraft, as well as the demonstration of such a system aboard the CRAF.
Document ID
19880047895
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hansen, D. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Horttor, R. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Riley, A. L.
(California Institute of Technology Jet Propulsion Laborataory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS PAPER 86-420
Report Number: AAS PAPER 86-420
Meeting Information
Meeting: Aerospace century XXI: Space flight technologies
Location: Boulder, CO
Country: United States
Start Date: October 26, 1986
End Date: October 29, 1986
Sponsors: AAS
Accession Number
88A35122
Distribution Limits
Public
Copyright
Other

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