Methods for determining optimum stage-weight distribution and ascending trajectory of multistage rockets have individually been described; these two problems are inherently inseparable and are not independent of each other; unified numerical method integrating these two optimization problems for satellite laucching vehicles is explained; also, numerical examples concerning finding of optimum vehicle to place 150 kg weight satellite into circular orbit at height of 1000 km are given. (In Japanese with English abstract) (Rec'd 1968)


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    Titel :

    Optimization of staging and trajectory for satellite launching vehicles


    Weitere Titelangaben:

    Mitsubishi Heavy Industries, Ltd -- Tech Bul


    Beteiligte:
    Matsubara, H. (Autor:in) / Yamada, Y. (Autor:in) / Nakanishi, H. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Japanisch


    Schlagwörter :


    Optimization of staging and trajectory for satellite launching vehicles

    Matsubara, Hideo / Yamada, Yuji / Nakanishi, Hideki | TIBKAT | 1966


    Method of weight prediction of satellite launching vehicles

    Ball, K.J. / Heyes, C.T. | Engineering Index Backfile | 1967




    MSAT satellite launching

    Online Contents | 1995