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    Title :

    Thermal radiation of heterogeneous combustion products at the nozzle exit of the rocket microengine


    Contributors:

    Published in:

    Publication date :

    2016




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    Local classification TIB:    770/7040/8000
    BKL:    55.50 Luftfahrzeugtechnik



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    Micro-Heat Engines, Gas Turbines, and Rocket Engines - The MIT Microengine Project -

    Epstein, A. H. / Senturia, S. D. / Al-Midani, O. et al. | British Library Conference Proceedings | 1997


    Micro-heat engines, gas turbines, and rocket engines - The MIT microengine project

    Epstein, A. / Senturia, S. / Al-Midani, O. et al. | AIAA | 1997



    Use of Discontinuous Exit Flows to Reduce Rocket Nozzle Length

    Rao, G. V. R. / Beck, J. E. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1994