The application of heat pipe technology to the design of rocket engine thrust chambers is discussed. Subjects presented are: (1) evaporator wick development, (2) specific heat pipe designs and test results, (3) injector design, fabrication, and cold flow testing, and (4) preliminary thrust chamber design. (Author)


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    Title :

    Heat Pipe Technology for Advanced Rocket Thrust Chambers


    Contributors:

    Publication date :

    1971


    Size :

    224 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Advanced tube-bundle rocket thrust chambers

    KAZAROFF, JOHN M. / PAVLI, ALBERT J. | AIAA | 1992


    Advanced tube-bundle rocket thrust chambers

    Kazaroff, John M. / Pavli, Albert J. | NTRS | 1992