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.


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    Titel :

    Eutelsat 2 Programme


    Beteiligte:
    C. Burgio (Autor:in) / J. Dumesnil (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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