Second order nonlinear differential equation of motion in case of rocket in drag-free vertical powered flight under constant thrust is solved by series expansion containing 9 terms; coefficients in series are in terms of given boundary conditions; truncation error of series is estimated, hence accuracy for practical problem based on analysis in paper could be well established; immediate applications are lunar landing and launching; case of constant thrust acceleration is also solved.


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    Titel :

    Rocket in drag-free vertical powered flight under constant thrust


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Zee, C.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :