Rocket engine injector orifice to accommodate changes in density, velocity, and pressure, thereby maintaining constant mass flow rate of propellant into rocket combustion chamber


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    Title :

    Rocket engine injector Patent


    Contributors:
    Stein, S. (author)

    Publication date :

    1968-11-05


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Rocket engine injector Patent

    Stein, S. | NTRS | 1964


    Rocket propellant injector Patent

    Mantler, R. L. | NTRS | 1960



    Rocket engine Patent

    Dangle, E. E. / Richley, E. A. / Wear, J. D. | NTRS | 1964