Several examples are calculated of optimum utilization of low-thrust propulsion systems (electrical propulsion) and high-thrust propulsion systems (chemical or nuclear rockets); use of both systems in combination will often result in performance superior to that obtainable with either system alone; preliminary theories for optimizing staging and trajectories of such dual-thrust vehicles in field-free space and in central force field.


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    Titel :

    Use of high- and low-thrust propulsion in combination for space missions


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Edelbaum, T.N. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :