The results are presented of a study to show the effect on flyback trajectories of constant inertial attitude during the fuel dissipation phase of a return-to-launch-site abort. It is shown that the value of the constant inertial attitude can be chosen to shape the flyback trajectory. (Author)


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    Title :

    Return-to-Launch-Site Trajectory Shaping


    Contributors:
    R. L. Bown (author)

    Publication date :

    1975


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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