Study of geometrically similar rockets of different sizes; essential difference between large and small missiles from standpoint of designer; it appears that rocket of 50 tons launching weight might have minimum proportion of deadweight; factors which will set limit to ultimate size of missiles. From paper before High Altitude and Satellite Rocket Symposium.


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    Title :

    Design problems of large rockets


    Additional title:

    Engineer


    Contributors:

    Published in:

    Engineer ; 204 , n 5295


    Publication date :

    1957


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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