The way a Proposed Deep Space Mission is designed should be linked to additional design parameters/ constraints such as the availability of the Deep Space Network to support communications. This paper explores this exact methodology by examining the launch opportunities of a simulated mission to Jupiter during a decade long timeframe.


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    Title :

    Using available DSN tracking converage as a design parameter in mission proposals


    Contributors:

    Conference:

    12th AAS/AIAA Space Flight Mechanics Meeting


    Publication date :

    2002-01-27


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English







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