Launch windows of few hours daily are obtained for highly eccentric orbits in order that lunar and solar perturbations will not lower perigee into atmosphere for specified period after launch, usually year; characteristics of perturbations, methods employed in numerically integrating perturbations, construction of launch window map, and characteristics of launch window map are considered.


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    Titel :

    Launch windows for highly eccentric orbits


    Weitere Titelangaben:

    Progress Astronautics Aeronautics -- Celestial Mechanics Astrodynamics


    Beteiligte:
    Shute, B.E. (Autor:in)


    Erscheinungsdatum :

    1964


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Launch Windows for Highly Eccentric Orbits

    Szebehely, Victor G. | AIAA | 1964


    Highly Eccentric Satellite Orbits

    Wnuk, E. | Online Contents | 1997


    Highly Eccentric Satellite Orbits

    Wnuk, E. / Committee on Space Research; Technical Panel on Satellite Dynamics | British Library Conference Proceedings | 1997