1–20 of 38 hits
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    Low-burning-rate solid propellants in acceleration fields

    BRUNDIGE, W. / CAVENY, L. | AIAA | 1981

    Pressure transients of solid rockets with slow gas phase reaction times

    CAVENY, L. / BATTISTA, R. / SUMMERFIELD, M. | AIAA | 1973

    Thrust and ignition transients of the Space Shuttle solid rocket motor

    CAVENY, L. / KUO, K. / SHACKELFORD, B. | AIAA | 1979

    Propellant burning rate uniformity identified by ultrasonic acousticemissions

    CAVENY, L. / SABER, A. / SUMMERFIELD, M. | AIAA | 1976

    Aluminized solid propellants burning in a rocket motor flow field

    GANY, A. / CAVENY, L. / SUMMERFIELD, M. | AIAA | 1977

    Transition to nonlinear instability in solid propellant rocket motors

    GLICK, R. / MICCI, M. / CAVENY, L. | AIAA | 1981

    Effect of acceleration on the burning rate of composite propellants

    CAVENY, L. / GLICK, R. / HODGE, B. | AIAA | 1967