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Communication system for the Viking mission to MarsThe Viking communications system discussed comprises a UHF relay link and an S-band communication link. The design of both links was guided by the design of the mission itself and its constraints. The most important of these are: the available launch opportunities; the effect of interplanetary distances on the power and bandwidth of the S-band link; weight; reliability and survival in the Martian environment; the up-link command philosophy; the landing problem; and the requirements for planetary quarantine and cleanliness. The Viking mission, with its orbits and trajectories, launch and landing sequences is described and illustrated.
Document ID
19750027654
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Brown, I.
(RCA, Astro-Electronics Div., Princeton N.J., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1974
Publication Information
Publication: RCA Engineer
Volume: 20
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Accession Number
75A11726
Distribution Limits
Public
Copyright
Other

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