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Carbon based materials are generally known for high temperature withstanding properties which remain unaffected up to 2300 °C. The carboncarbon composite can be synthesized using compaction of carbon or multiple impregnations of porous frames with liquid carboniser precursors and subsequent pyrolization or through chemical vapor deposition of pyrolytic carbon [14]. These composites can retain their temperature stability upto 2400 °C along with dimensional stability and thus make them the oblivious choice in space research, military and aeronautics. The components which are regularly exposed to higher temperature and responsible for demands of high standard performance generally utilize carbon-carbon composites [15].