Scale model compressed air tests of 260-inch solid rocket with submerged nozzle to determine exhaust flow velocity and direction in annular channel


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    Title :

    Investigation of a submerged nozzle for solid rockets


    Contributors:

    Publication date :

    1967-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    INVESTIGATION OF A SUBMERGED NOZZLE FOR SOLID ROCKETS

    SALMI, REINO / PELOUC, JR., JAMES | AIAA | 1967


    Investigation of a submerged nozzle for solid rockets.

    Pelouch, J. J., Jr. / Salmi, R. J. | NTRS | 1967


    Effect of nozzle submergence upon stability of solid rockets

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