Problems encountered and solved successfully in design of Viking RTV-N-12a with reaction motors XLR 10-RM-2 liquid oxygen and alcohol rocket engine producing 21,000 lb thrust at sea level for research at altitudes between 100 and 200 mi.


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    Title :

    Aerodynamic design of high-altitude rocket


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1955


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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