Conservation equations coupled with mass balance equation to produce method of computing transient burning rates in solid propellant motors


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    Titel :

    A theoretical study of combustion and quenching of solid propellant rocket motors during depressurization


    Beteiligte:
    Fletcher, E. A. (Autor:in) / Hiroki, T. (Autor:in)

    Erscheinungsdatum :

    15.01.1968


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rapid Depressurization Dynamics of Solid Propellant Rocket Motors

    Tahsini, Amir / Farshchi, Mohammad | AIAA | 2007


    Rapid Depressurization Dynamics of Solid Propellant Rocket Motors AIAA Paper

    Tahsini, A. / Farshchi, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007


    Quenching of solid rocket propellants by depressurization.

    Bunde, G. W. / Fletcher, E. A. / Hiroki, T. et al. | NTRS | 1966


    Combustion instability in solid propellant rocket motors

    Price, E.W. / Sofferis, J.W. | Engineering Index Backfile | 1958