Unconventional trajectory techniques for space missions in the Sun-Earth-Moon system, including libration-point orbits, gravity-assist maneuvers, and Earth-return trajectories are reviewed. The ISEE-3/ICE flight experience is used to illustrate the utility of libration-point orbits called halo-orbits. Five lunar gravity-assist maneuvers used by the ISEE-3/ICE spacecraft are discussed. The final lunar swingby sent the spacecraft into a heliocentric trajectory that will eventually intercept Comet Giacobini-Zinner. As an example of the Earth-return trajectory concept, a proposed mission that includes flybys of three comets and two asteroids is described.


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    Titel :

    Orbital acrobatics in the Sun-Earth-Moon system


    Beteiligte:
    Farquhar, Robert W. (Autor:in) / Dunham, D. W. (Autor:in) / Hsu, S. C. (Autor:in)


    Erscheinungsdatum :

    1986-12-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    R. W. Farquhar / D. W. Dunham / S. C. Hsu | NTIS | 1986


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