61–80 von 2,684 Ergebnissen
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    Wave intersection limits for focused compression of air in chemical equilibrium

    PEARSON, L. W. / SCHOELEN, F. J. | AIAA | 1965
    Verlag: The American Institute of Aeronautics and Astronautics

    Velocity defect laws for transpired turbulent boundary layers

    FRASER, M. D. / MASSACHUSETTS INST. OF TECH. / DEPT. OF CHEMICAL ENGINEERING et al. | AIAA | 1965
    Verlag: The American Institute of Aeronautics and Astronautics

    Performance of solid propellants containing metal additives

    Cheung, H. / Cohen, N.S. | Engineering Index Backfile | 1965
    studied although some combustion took place in nozzle; results indicate that condensation of oxide vapor can be described by first-order chemical ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Recent developments and current status of hybrid rocket propulsion

    Ordahl, D.D. / Rains, W.A. | Engineering Index Backfile | 1965
    Comparison of performance capabilities and growth history of hybrids with other forms of chemical propulsion systems is presented showing ...

    Arc-jet propulsion for attitude and orbit control of MORL

    tobias, I.I. / Kosson, R.L. | Engineering Index Backfile | 1965
    ; by comparison, stored-chemical propulsion system with specific impulse of 300 sec has mass of 11,790 lb maximum; this represents launch mass ...

    Characteristic calculation of flowfields with chemical reactions.

    GERBER, N. / SEDNEY, R. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Energetics and chemical kinetics of polystyrene surface degradation in inert and chemically reactive environments.

    HANSEL, J. G. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Comparison of chemical history and rates for the H sub 2 -air reaction.

    RUBINS, P. M. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Mechanical and chemical contributions to the erosion rates of graphite throats in rocket motor nozzles.

    GOWARIKER, V. R. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Instrumental determination of large amounts of fluorine in oxygen.

    DECKER, W. H. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Significance of nonequilibrium conductivity on plasma engine performance.

    DIMMOCK, T. H. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Thermal diffusivity of ammonium perchlorate.

    INAMI, S. H. / ROSSER, W. A. / WISE, H. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Shock tube ignition delay studies of endothermic fuels.

    HAWTHORN, R. D. / NIXON, A. C. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Effects of grain configuration upon the burning rate of a spinning rocket motor.

    MURPHY, J. M. / WALL, R. H. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    A new synthesis of o-nitrophenylacetaldehyde.

    Noland, W. E. / Sellstedt, J. H. | NTRS | 1966
    New synthesis of o-nigrophenylacetaldehyde ...
    Schlagwörter: CHEMICAL REACTION

    Ignition of ammonium perchlorate composite propellants by convectiveheating.

    BAER, A. D. / KELLER, J. A. / RYAN, N. W. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Ignition of simulated propellants based on ammonium perchlorate.

    FISHMAN, N. | AIAA | 1966
    Verlag: The American Institute of Aeronautics and Astronautics

    Nonacoustic instability of composite propellant combustion.

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

    A theory for ignition and deflagration of fuel drops.

    PESKIN, R. L. | 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