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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    Titel :

    Design problems of large rockets


    Weitere Titelangaben:

    Engineer


    Beteiligte:
    Bossart, K.J. (Autor:in)

    Erschienen in:

    Engineer ; 204 , n 5295


    Erscheinungsdatum :

    1957


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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