One effective method of increasing composite propellant burning rate is by addition of numerous short, nonreactive, metal fibers to basic propellant; analytical studies were directed at thermal processes that occur as single short fibers oriented normal to propellant surface are consumed; characteristics of model were determined by perturbation of important variables about those for 0.8×5×125 mil aluminum fiber in high base rate propellant (1.5 ips); trends predicted agree with those observed experimentally showing that intrinsic ability for burning rate enhancement depends upon thermal diffusivity and melting temperature.


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    Titel :

    Influence of embedded metal fibers on solid-propellant burning rate


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Caveny, L.H. (Autor:in) / Glick, R.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Influence of Thermal Radiation on Solid Propellant Burning Rate

    LEONARD H. CAVENY / THOMAS J. OHLEMILLER / MARTIN SUMMERFIELD | AIAA | 1975



    Uncertainty of Solid Propellant Burning Rate Measurements

    Evans, John / Penton, Ashley / Frederick, Robert | AIAA | 2009