Two alternative mission profiles are presented for the WIND mission whose baseline design includes two years in a double lunar swingby (DLS) orbit followed by one year in a Lissajous orbit about the sun-earth L1 libration point. The first alternative uses a half-month high-inclination transfer orbit between two lunar gravity assists to change the initial sunward DLS orbit to a DLS orbit in the geomagnetic tail region. The second alternative uses a direct insertion from launch into a large-amplitude Lissajous orbit followed by a sunward DLS orbit.


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    Titel :

    Double lunar swingby and Lissajous trajectory design for the WIND mission


    Beteiligte:
    Sharer, P. J. (Autor:in) / Dunham, D. W. (Autor:in) / Jen, S. (Autor:in) / Roberts, C. E. (Autor:in) / Seacord, A. W., II (Autor:in) / Folta, D. C. (Autor:in)

    Erscheinungsdatum :

    01.08.1992


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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