The Eutelsat 2 spacecraft is a spacebus 100 B model, three axis stabilized, with a launch weight of 1800 kilograms, designed to be operational during eclipse and to be compatible with Ariane 4 and Atlas Centaur launch vehicles. The predicted in orbit lifetime is above seven years. The Eutelsat 2 mission is reviewed and a technical description including the communications payload, of the satellite is given. The program schedule and future prospects are discussed.
Eutelsat 2 Programme
1991
4 pages
Report
Keine Angabe
Englisch
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