81–100 von 1,837 Ergebnissen
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    Nonacoustic instability of composite propellant combustion.

    BAER, A. D. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Failure behavior of composite hydrocarbon fuel binder propellants.

    JONES, T. M. / KRUSE, R. B. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Effect of liquid nitrogen dilution on LOX IMPACT sensitivity.

    GAYLE, J. B. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Including re-entry heating in rocket engine thermal analyses.

    FINEMAN, S. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Temperature distribution within a particle during evaporation.

    ABLOW, C. M. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Chemical stabilization of beach sand

    C. V. Brouillette Part I. X-72 Diamine modification of the aniline-furfural method of beach sand stabilization. Part II. Operational procedure for preparation of stabilized beach sand roadway. Naval Civil Engineering Lab. Port Hueneme, Calif.
    Elsevier | 1967

    Computer experiments related to chemical propulsion.

    SICHEL, M. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Chemical relaxation phenomena behind normal shock waves in a dissociated freestream.

    CARLSON, L. A. / HARTSEL, J. E. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    A simplified technique for evaluating vibrational and/or chemical relaxation behind shock waves.

    ADAMS, D. M. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Temperature sensitivity of solid propellant burning rate.

    GLICK, R. L. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Influence of embedded metal fibers on solid- propellant burning rate.

    CAVENY, L. H. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Development of a fundamental model of hypergolic ignition in space-ambient engines.

    AGOSTA, V. D. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Catalyzed thermal decomposition of ammonium perchlorate.

    DAUERMAN, L. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Control of pressure deflagration limits of composite solid propellants.

    MCDONALD, A. J. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Internal ballistics of slotted-tube, solid- propellant rocket motors.

    CAVENY, L. H. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Application of the hydraulic analogy to axisymmetric nonideal compressible gas systems.

    ADAMS, D. M. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Dynamics of heterogeneous reaction at a stagnation point.

    SCHMITZ, R. A. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Effect of specific-heat ratio on mass flow for swirling nozzle flow.

    GLICK, R. L. / KILGORE, M. S. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Characterization of volatilized species from solid propellants.

    DAUERMAN, L. / SALSER, G. E. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics

    Development of airframe heat protection for a high-performance sounding rocket.

    OVERMIER, D. K. | AIAA | 1967
    Verlag: The American Institute of Aeronautics and Astronautics