Effect of various dimensions on performance of system was studied both theoretically and experimentally; theory employing nonviscous fluid mechanics is developed showing good agreement with experiments; results show that pumping fluid leaving nozzle can evacuate its own environment to minimum value of 0.025 atm.


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    Title :

    Performance investigation of nonpumping rocket-ejector system for altitude simulation


    Additional title:

    NASA -- Tech Note


    Contributors:
    Fortini, A. (author)


    Publication date :

    1959


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :