The concept of the effective ejection velocity of a rocket engine is explained and the magnitude of the attainable ejection velocity theoretically and experimentally investigated. Velocities above 3000 meters per second (6700 mph) are actually measured and the possibilities of further increases shown.


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    Titel :

    Recent Results in Rocket Flight Technique


    Beteiligte:
    Sanger, Eugen (Autor:in)

    Erscheinungsdatum :

    01.04.1942


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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