Combustion instability -- departures from normal steady-state operating pressure -- has been major problem in solid propellant rocket motor design since early in World War II; experimental work and present state of art are briefly summarized; various theories discussed, with special attention to McClure theory.


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    Title :

    Combustion instability in solid propellant rocket motors -- Review


    Additional title:

    Fuel Soc J


    Contributors:
    Sotter, G. (author)

    Published in:

    Publication date :

    1963


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Combustion instability in solid propellant rocket motors

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




    Combustion Instability and the Design of Solid Propellant Rocket Motors

    A. K. Roberts / W. G. Brownlee / F. Jackson | NTIS | 1970