Investigation of limiting conditions for ramjet propulsion set by pressure and temperature of gaseous flow within propulsion duct and in environment of missile; results are plotted as functions of flight altitude and flight Mach number; known types of ramjet propelled missiles and aircraft in test or production stage are included; proposals made relating to research and development of ramjet engines within feasible application ranges.


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    Title :

    Application ranges of ramjet propulsion


    Additional title:

    Anwendungsbereiche der Staustrahlantriebe


    Contributors:


    Publication date :

    1961


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Application ranges of ramjet propulsion

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