Conceptual design of a synchronous Mars telecommunications satellite

Details Conceptual design of a synchronous Mars telecommunications satellite Conceptual design of a synchronous Mars telecommunications satellite

Nov 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989cdsm.book.....b&link_type=abstract

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Command And Control, Communication Satellites, Structural Design, Mars (Planet), Space Exploration

Scientific paper

Future missions to Mars will require a communications system to link activities on the Martian surface with each other and with mission controllers on Earth. A conceptual design is presented for an aerosynchronous communications satellite to provide these links. The satellite provides the capability for voice, data/command, and video transmissions. The mission scenario assumed for the design is described, and a description of a single aerosynchronous satellite is explained. A viable spacecraft design is then presented. Communication band selection and channel allocation are discussed. The communications system conceptual design is presented along with the trades used in sizing each of the required antennas. Also, the analyses used to develop the supporting subsystem designs are described as is the communications impact on each subsystem design.

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