Maximum range of rocket vehicle is discussed applying variational theory of optimum multistage processes; vector thrust may be controlled in magnitude and in direction, and two-stage vehicle considered is assumed flying in vacuum; it is shown that maximum range trajectory of two-stage rocket vehicle flying in vacuum is composed of three subarcs; staging conditions presented permit determination of fundamental function that makes it possible to detect type, sequence, and number of subarcs forming external arc; conclusions also apply to n-stage vehicles.


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    Titel :

    Optimization of multistage processes


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Cavoti, C.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Optimization of multistage processes

    CAVOTI, C. R. | AIAA | 1965



    On optimization of multistage rockets

    Hall, H.H. / Zambelli, E.D. | Engineering Index Backfile | 1958


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    Liao-McPherson, Dominic / Li, Huayi / Kolmanovsky, Ilya et al. | SAE Technical Papers | 2020