This paper describes the Jet Propulsion Laboratory effort to navigate Nozomi, in conjunction with Japan's Institute of Space and Astronauticaal Science, past two Earth swingbys using differential tracking techniques to successfully place the spacecraft on a trajectory reaching Mars in December 2003.


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    Title :

    Nozomi Earth swingby orbit determination


    Contributors:
    Nandi, Sumita (author) / Ryne, Mark (author)

    Publication date :

    2004-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English



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