Rocket engine performance is quoted in terms of frozen or shifting equilibrium nozzle expansion processes; experiments made with RP-1/oxygen propellant system consisted of measurement of flow rates, chamber pressure, nozzle pressure profile, and static gas temperature in large (30.1) expansion ratio nozzle; it is found that near frozen conditions exist at low (below 1.6) oxidizer to fuel (O/F) ratios, and near equilibrium conditions exist at higher (above 2.0) O/F ratios.


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    Title :

    Experiments on recombination effects in rocket nozzles


    Additional title:

    AIAA J


    Contributors:
    Hoglund, R. (author) / Carlson, D. (author) / Byron, S. (author)

    Published in:

    AIAA Journal ; 1 , n 2


    Publication date :

    1963


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    EXPERIMENTS ON RECOMBINATION EFFECTS IN ROCKET NOZZLES

    BYRON, S. / CARLSON, D. / HOGLUND, R. | AIAA | 1963


    Catalysis of hydrogen-atom recombination in rocket nozzles

    Lordi, J. A. / Mates, R. E. | TIBKAT | 1966


    Catalysis of Hydrogen-Atom Recombination in Rocket Nozzles

    J. A. Lordi / R. E. Mates | NTIS | 1965


    Catalysis of Hydrogen-Atom Recombination in Rocket Nozzles

    J. A. Lordi / R. E. Mates | NTIS | 1966


    Catalysis of hydrogen-atom recombination in rocket nozzles

    Lordi, J. A. / Mates, R. E. | NTRS | 1966