Maneuvers in which orbital plane of earth satellite is changed by means of aerodynamic forces during one or more skips into and out of atmosphere are analyzed; characteristic velocities required of rockets to deflect vehicle into atmosphere and to reaccelerate it to orbital speed after leaving atmosphere are calculated as functions of change in inclination lift-drag ratio, and entry angle, and compared with characteristic velocities required for purely extra-atmospheric rocket maneuvers.


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    Titel :

    Change of satellite orbit plane by aerodynamic maneuvering


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    London, H.S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :