Study was carried out of process in which solid-propellant combustion is terminated by rapid drop in pressure; experimentally, propellant burning in small rocket motor was subjected to rapid pressure drop when auxiliary nozzle was suddenly opened; results were compared to predictions of theoretical model, based on assumption that extinction occurs when heat absorption by solid propellant exceeds heat transfer to solid propellant from combustion gas; theoretical predictions agreed well with experimental results gathered in program and those by other investigators.


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    Titel :

    Depressurization induced extinction of burning solid propellant


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Horton, M.D. (Autor:in) / Bruno, P.S. (Autor:in) / Graesser, E.C. (Autor:in)

    Erschienen in:

    AIAA Journal ; 6 , n 2 ; p 292-297


    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :