Atmospheric reentry

Which are the composite materials used in advanced re-entry space vehicles like X-38? What are the mech.and thermal properties of alumina2014,C-C Composite and inconel 718 at elevated temp(at >700K)?

i expect Yield strengths,young's modulus,poisson's ratio specific heat etc. at high temperatures (at all available temperatures)

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Carbon fiber and the use of any or all heat resistance materials are utilized.