Irregular mixture ratio (O/F) distribution across face of injector can result from unequal hydraulic resistances to injector elements and by chamber cooling requirements; degree to which O/F distribution will influence specific impulse depends upon propellant system and operating conditions, extent of O/F deviations, and degree of turbulent mixing in combustion chamber; how these effects can be taken into account in rocket thrust chamber designs by use of stream-tube analysis is shown; evaluations of three rocket thrust systems and experimental results.


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    Title :

    Mixture ratio distribution -- Its impact on rocket thrust chamber performance


    Additional title:

    J Spacecraft Rockets


    Contributors:
    Pieper, J.L. (author) / Dean, L.E. (author) / Valentine, R.S. (author)

    Published in:

    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Mixture ratio distribution - Its impact on rocket thrust chamber performance.

    DEAN, L. E. / PIEPER, J. L. / VALENTINE, R. S. | AIAA | 1967



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