This paper details the objectives of the mission, the key constraints that influenced the mission design, and the flight and ground system implementation. Issues that influenced the mission architecture are discussed, as well as the technology assumptions.


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    Title :

    A fission powered Mars Telecommunications Orbiter mission concept


    Contributors:

    Publication date :

    2003-02-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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