Iridium-coated rhenium combustion chamber withstands operating temperatures up to 2,200 degrees C. Chamber designed to replace older silicide-coated combustion chamber in small rocket engine. Modified versions of newer chamber could be designed for use on Earth in gas turbines, ramjets, and scramjets.


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    Title :

    Iridium-Coated Rhenium Combustion Chamber



    Published in:

    Publication date :

    1994-08-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :



    DESIGN, ANALYSIS, AND FABRICATION OF OXIDE-COATED IRIDIUM/RHENIUM COMBUSTION CHAMBERS

    Jang, Q. / Tuffias, R. H. / La Ferla, R. et al. | British Library Conference Proceedings | 1993


    Iridium coated rhenium rocket chambers produced by electroforming

    Toenshoff, D. / Lanam, R. / Ragaini, J. et al. | AIAA | 2000


    Iridium/rhenium combustion chambers - From concept to reality

    Tuffias, R. / Kaplan, R. / Williams, B. et al. | AIAA | 1996


    Iridium/Rhenium Combustion Chambers: From Concept to Reality

    Tuffias, R. H. / Kaplan, R. B. / Williams, B. E. et al. | British Library Conference Proceedings | 1996