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Carbon fiber reinforced carbon composites (C/C) composites were first developed by the American Chance Vought Airline in 1958 and successfully applied to solid rocket motor nozzles in the 1970s. In general, C/C composite consists of three components: carbon fibre yarns, carbon matrix and fiber yarn-matrix interface. C/C composites have become one of the ideal materials for thermal structures due to the advantages of high strength, low density and high temperature resistance.
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