Report on study to determine exhaust velocity which would result in maximum payload mass fraction for possible combinations of vehicle characteristics and mission requirements; equation giving optimum exhaust velocity was derived by maximizing ratio of payload mass to take-off mass and used in study of 3 rockets; results are shown.


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    Title :

    Analyzing exhaust velocity requirements for electrically powered rockets


    Additional title:

    Gen Motors Eng J


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :