THE significant design parameters of an ion-propellant rocket engine are developed in terms of three independent parameters. These are: the ratio of the acceleration voltage to atomic or molecular weight of the propellant, gross weight of the vehicle, and thrust-to-weight ratio.Engineering trends are presented which will lead toward advanced study of ion thrust chambers, power generation systems, and propellants.This paper received the 1958 Manley Memorial Award.


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    Titel :

    The ION ROCKET ENGINE


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Boden, R. H. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1959-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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