The Galileo mission has been reprogrammed to use a direct earth-Jupiter trajectory with a May 1986 launch date and with arrival at Jupiter occurring in mid-1988. Within the constraints of Shuttle/Centaur launch vehicle capability and total spacecraft mass and performance, optimal broken-plane trajectories are generated, and the region of positive propellant margin in the launch/arrival space is determined. Mission constraints are used to define a launch/arrival strategy. It is also shown that a close flyby of any one of several asteroids or a comet is possible on the interplanetary transfer with minimal impact on mission performance.


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    Titel :

    Interplanetary trajectory design for the Galileo mission


    Beteiligte:
    Damario, L. A. (Autor:in) / Byrnes, D. V. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1983 ; Reno, NV


    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Interplanetary trajectory design for the Galileo mission

    DAMARIO, L. / BYRNES, D. | AIAA | 1983




    Interplanetary Trajectory Optimization with Application to Galileo

    Louis A. DAmario / Dennis V. Byrnes / Richard H. Stanford | AIAA | 1982


    Europa Clipper Mission Design: Interplanetary Trajectory Navigation Analysis

    Goodson, Troy / Boone, Dylan / French, Andrew et al. | Springer Verlag | 2025