The trajectory profile that will be used by Japan's Sakigake spacecraft to accomplish its extended-mission objectives is described. Currently, Sakigake is following a heliocentric trajectory that will return to the earth's vicinity in January 1992. Four earth gravity-assist maneuvers are planned to redirect Sakigake to an encounter with Comet Honda-Mrkos-Pajdusakova (HMP) in February 1996. While carrying out the earth-swingby maneuvers, the spacecraft will make several passes through previously unexplored regions of the distant geomagnetic tail.


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    Titel :

    Trajectories for the Sakigake extended-mission phase


    Beteiligte:
    Farquhar, R. (Autor:in) / Dunham, D. (Autor:in) / Hsu, S. (Autor:in) / Uesugi, K. (Autor:in) / Kawaguchi, J. (Autor:in)

    Kongress:

    International Symposium on Space Technology and Science ; 1988 ; Sapporo, Japan


    Erscheinungsdatum :

    01.01.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    SAKIGAKE/SUSEI communications system

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