Problem of placing artificial satellite by means of 2 rockets into elliptical orbit, with maximum payload to initial weight ratio, was studied previously; rockets are idealized as impulses and effect of aerodynamic force is neglected; with assumption that both rockets have same specific impulse, it was found that optimum transfer trajectory is of Hohmann type; in general, specific impulses of 2 rockets may be quite different; in present paper optimum launching problem is investigated without restricting ratio of specific impulses of 2 rockets to unity.


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    Titel :

    Optimum launching of satellite by two impulses of unequal specific impulse


    Weitere Titelangaben:

    Astronautica Acta


    Beteiligte:
    Ting, L. (Autor:in) / Pierucci, M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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