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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    Titel :

    Ultimate design of high altitude sounding rockets


    Weitere Titelangaben:

    Jet Propulsion


    Beteiligte:
    Michelson, I. (Autor:in)

    Erschienen in:

    Jet Propulsion ; 27 , n 10


    Erscheinungsdatum :

    1957


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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