Nozzle insert evaluation and gas cooling concept in storable liquid propellant rocket engine


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    Title :

    Evaluation of 7.8-inch-throat-diameter inserts and a unique cooling concept in a storable- propellant rocket engine


    Contributors:

    Publication date :

    1969-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English