Parametric study of vehicle size for direct-flight manned lunar mission; main parameter is take-off thrust which is influenced by many factors; close choice exists in second stage where conventional and high-energy propellants are compared; size of final stage is governed by method of approach to earth's surface.


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    Title :

    Rocket for manned lunar exploration


    Additional title:

    IRE -- Trans Space Electronics Telemetry


    Contributors:
    Rosen, M.W. (author) / Schwenk, F.C. (author)


    Publication date :

    1959


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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