The Nozomi spacecraft is the first to achieve an Earth-Mars transfer orbit without a direct hyperbolic insertion maneuver.


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    Title :

    Nozomi CIS-Lunar Phase Orbit Determination


    Contributors:
    Criddle, K. (author) / Ryne, M. (author)

    Publication date :

    1999-08-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Nozomi Cis-Lunar Phase Orbit Determination

    Criddle, K. / Ryne, M. | NTRS | 1999


    Nozomi Cis-lunar Phase Orbit Determination (AAS 99-329)

    Ryne, M. / Criddle, K. / American Astronautical Society et al. | British Library Conference Proceedings | 2000


    NOZOMI Orbit Determination

    Ohnishi, T. / Ishibashi, S. / Yoshikawa, M. et al. | British Library Conference Proceedings | 2002


    Nozomi Earth swingby orbit determination

    Nandi, Sumita / Ryne, Mark | NTRS | 2004


    NOZOMI Orbit Determination in the Earth Swingby Phase

    Yoshikawa, M. / Kato, T. / Ichikawa, T. et al. | British Library Conference Proceedings | 2004