This paper will address the trajectory correction maneuvers (TCMs) which enabled the successful completion of the circuitous VEEGA trajectory while providing for the first ever encounters with main-belt asteroids.


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    Title :

    (abstract) Maneuver Design for Galileo Asteroid Flybys


    Contributors:

    Publication date :

    1994-05-22


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English







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