Optical multiple access intersatellite links

Physics

Scientific paper

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Data Links, Multiple Access, Optical Communication, Satellite Networks, Spacecraft Communication, Tdr Satellites, Satellite Design, Satellite Tracking, Systems Engineering, Target Acquisition

Scientific paper

The feasibility of an optical implementation of a multiple access medium data rate data relay service on the timescale of Euro-DRS was assessed. The service requirements for the feasibility study are based on the service which, in existing or planned systems, is implemented at S band. The system should communicate simultaneously with up to 8 LEO users in orbits of radii up to 7400 km providing 8 independently agile links. On each link, it should communicate at up to 2Mb/sec, at bit error rates of 10 to the minus 6th power in the return direction (LEO to GEO). A design concept for the GEO central node was produced. Mass and power estimates were evaluated and a preliminary spacecraft accommodation study performed. The system weighs 130 kg and has a power consumption of 300 W. The optical subsystem occupies a 75 x 75 x 30 cm volume on the top floor of the spacecraft. A number of trade-offs were identified and performed in reaching the final system configuration. The system should have 1 telescope system per user, a periscope mirror configuration for coarse pointing, a single telescope for both transmit and receive, and the use of both 0.8 micron for the LEO-GEO link and 1.3 micron for GEO-LEO.

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