Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for bipropellant rockets


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    Title :

    Exploring in aerospace rocketry. 7 - Liquid propellant rocket systems


    Contributors:

    Conference:

    LEWIS AEROSPACE EXPLORERS ; 1966 , 1967 ; CLEVELAND


    Publication date :

    1968-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English