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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:

    Published in:

    D ; 5324


    Publication date :

    1969


    Size :

    III, 34 S


    Remarks:

    Ill., graph. Darst


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English






    Improved Throat Inserts for Ablative Thrust Chambers

    D. N. Crump / H. H. Henderson / K. J. Smith | NTIS | 1967


    Improved throat inserts for ablative thrust chambers

    Crump, D. N. / Henderson, H. H. / Smith, K. J. | NTRS | 1967