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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    Titel :

    Heat Pipe Technology for Advanced Rocket Thrust Chambers


    Beteiligte:
    D. C. Rousar (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    224 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    Advanced tube-bundle rocket thrust chambers

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