Techniques available which determine optimum sounding rocket capability as function of fuels and materials limitations, for types of multistaged rockets which are of greatest importance with respect to space flight; calculation results presented for two examples representing extreme altitude sounding to summit height of one earth diameter, and minimal lunar flight.


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    Title :

    Ultimate design of high altitude sounding rockets


    Additional title:

    Jet Propulsion


    Contributors:

    Published in:

    Jet Propulsion ; 27 , n 10


    Publication date :

    1957


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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