Analysis of escape trajectory of solar sail from original circular satellite orbit oriented perpendicular to planet sun line subject to steering program that provides maximum time rate of energy increase; general solution is obtained, independent of vehicle dimensions, choice of planet, and starting conditions; although resulting trajectory is not optimum with respect to escape time and restricted by assumptions, it is useful as means of rapidly estimating solar sail escape performance in preliminary design studies.


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    Titel :

    Generalized three-dimensional trajectory analysis of planetary escape by solar sail


    Weitere Titelangaben:

    ARS J


    Beteiligte:
    Fimple, W.R. (Autor:in)

    Erschienen in:

    ARS Journal ; 32 , n 6


    Erscheinungsdatum :

    1962


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Optimal solar sail spiral to escape

    Sackett, L. L. / Edelbaum, T. N. | NTRS | 1977


    Solar Sail Three-Body Transfer Trajectory Design

    Gong, Shengping / Baoyin, Hexi / Li, Jengfeng | AIAA | 2010


    Inverse Solar Sail Trajectory Problem

    Colin R. McInnes | AIAA | 2003