Effect is investigated for Hohmann type transfers; closed form solution of trajectory during thrusting is obtained by assuming that constant thrust is applied normal to focal radius and that change of radial position of rocket is small; example shows thrusting time, thrust level, propellant consumption, and conic trajectories following powered flight paths, etc, in comparison with ordinary impulsive thrust case; calculations of lead angle and time are introduced based on analysis presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effect of finite thrusting time in orbital maneuvers


    Weitere Titelangaben:

    AIAA J


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

    Erschienen in:

    AIAA Journal ; 1 , n 1


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Thrusting Trajectory Minimization Program for Orbital Transfer Maneuvers

    R. N. Green / L. H. Hoffman / G. R. Young | NTIS | 1971


    Thrusting trajectory minimization program for orbital transfer maneuvers

    Hoffmann, Lawrence H. / Green, Richard N. / Young, George R. | TIBKAT | 1971


    Asymptotic theory for thrusting, spinning-up spacecraft maneuvers

    Ayoubi, Mohammad A. | Online Contents | 2009


    Asymptotic theory for thrusting, spinning-up spacecraft maneuvers

    Ayoubi, Mohammad A. | Online Contents | 2009