The purpose of this program is to research the methods and materials that will produce thermally stable AP and burning rate catalyst. They will be used with other thermally stable propellant ingredients to produce a solid propellant that is capable of withstanding a temperature environment of -75 to 350 F. With the present capability of aircraft to fly at supersonic speeds, a new requirement now exists for missiles which can be carried externally. The major development problem arises from the effects of aerodynamic heating, causing missile skin temperatures of several hundred degrees Fahrenheit. In addition, the external carry means that a missile in the airstream is exposed to temperatures of about 65 F. Missiles and missile components therefore are subject to temperatures from -65 F to well over 300 F. (Posamentier)


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    Titel :

    Thermally stable burning rate accelerators


    Weitere Titelangaben:

    Beschleunigung der thermostabilen Verbrennung von Festtreibstoffen


    Beteiligte:
    Miller, M. (Autor:in) / Willis, T.C. (Autor:in) / Stephens, W.D. (Autor:in) / Flanigan, D.A. (Autor:in) / Hightower, J.O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1971


    Format / Umfang :

    21 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




    Thermally Stable Burning Rate Accelerators

    W. D. Stephens / D. A. Flanigan / J. O. Hightower et al. | NTIS | 1971


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    Li, Chiping / Kailasanath, K. / Oran, Elaine S. | AIAA | 1996



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