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    Title :

    Design of injectors and ablative thrust chambers for a flox-propane rocket engine with a 1.2-inch throat diameter


    Contributors:


    Publication date :

    1969


    Size :

    III, 34 S


    Remarks:

    Ill., graph. Darst
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English