Injector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia


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    Title :

    Evaluation of Injector Principles in a 2400-pound-thrust Rocket Engine Using Liquid Oxygen and Liquid Ammonia


    Contributors:

    Publication date :

    1959-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English