This paper describes the methods used to estimate the statistical delta V and propellant requirements for propulsive maneuvers necessary to deliver the two Rovers while ensuring that planetary protection requirements are satisfied.


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    Title :

    Flight path control strategies for the 2003 Mars Exploration Rover (MER) mission


    Contributors:
    Raofi, B. (author) / Bhat, R. S. (author) / D'Amario, L. A. (author)

    Conference:

    AIAA/AAS Astrodynamics Specialist Conference


    Publication date :

    2002-08-05


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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