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


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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 :

    1969-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    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