Characteristics of ballistic missile and design of nose cone primary purpose of which is to provide thermal protection for payload; factors considered in study of Missile and Space Vehicle Dept of General Electric Co selecting material to protect Atlas re-entry nose cone at ICBM ranges; flight test program and method of obtaining data with copper heat sink re-entry vehicle over range of re-entry conditions.


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    Titel :

    Nose cones -- Case for heat sink


    Weitere Titelangaben:

    Missiles Rockets


    Beteiligte:
    Stewart, J.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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