A program was conducted in which the response and failure charactersitcs of solid propellant rocket motors when subjected to transient thermal conditions representing air launch operational environments were recorded and analyzed. Future Air Force mission profiles were used. The Maverick motor, AGM-65A, was used as a test bed on the program. (Author)


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    Titel :

    Simulated Air Launch Environment, Volume II. Aeroheat Data Summary


    Beteiligte:
    O. R. Pritts (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    317 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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