Reference is made to previous work by first author considering problem of scheduling direction of constant momentum thrust of rocket, which loses mass at constant rate, so that it transfers to known earth satellite orbit in minimum time after launching; method is extended to solve problem of orbital transfer of such rocket with minimum fuel consumption.


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    Titel :

    Orbital transfer with minimum fuel


    Weitere Titelangaben:

    U S Naval Postgraduate School -- Research Paper


    Beteiligte:
    Bleick, W.E. (Autor:in) / Faulkner, F.D. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Orbital transfer with minimum fuel

    BLEICK, W. E. / FAULKNER, F. D. | AIAA | 1964


    Low Thrust Minimum-Fuel Orbital Transfer: A Homotopic Approach

    T. Haberkorn / P. Martinon / J. Gergaud | AIAA | 2004



    ORBITAL TRANSFER IN MINIMUM TIME

    BLEICK, W. E. | AIAA | 1963


    Low-thrust, minimum-fuel, orbital transfers

    Brusch, R. G. / Vincent, T. L. | NTRS | 1971