A viewgraph presentation outlines NASA's goals for the Second and Third Generation Reusable Launch Vehicles, placing emphasis on improving safety and decreasing the cost of transporting payloads to orbit. The use of ceramic matrix composite (CMC) technology is discussed. The development of CMC components, such as the Simplex CMC Blisk, cooled CMC nozzle ramps, cooled CMC thrust chambers, and CMC gas generators, are described, including challenges, test results, and likely future developments.


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    Title :

    Fabrication and Testing of Ceramic Matrix Composite Propulsion Components


    Contributors:
    M. R. Effinger (author) / R. G. Clinton (author) / J. Dennis (author) / S. Elam (author) / G. Genge (author)

    Publication date :

    2000


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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