C/C composites are reinforced with carbon or graphite fibers and their fabrics. C/C composites are also advanced composites based on carbon or graphite. 

In fact, the C/C composite is a multiphase material composed of a single carbon element. The C/C composite not only inherits the light-weight, high temperature and corrosion resistance of graphite, but also has a series of excellent properties such as high strength, high modulus, thermal shock resistance, thermal stress resistance and crack propagation resistance.

So C/C composites have been used earlier in the field of aerospace. Such as the engine nozzle of the solid rocket, the end cap and the heat proof jacket of the strategic missile, the thermal protection system of the nasal vertebra cap and the front edge of the wing of the space shuttle, the aircraft brake disc, etc.

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