High temperature C/C–SiC composite by liquid silicon infiltration: a literature review. PATEL, M., SAURABH, K., PRASAD, V. V. B., & SUBRAHMANYAM, J. Bulletin of Materials Science, 35(1):63–73, February, 2012.
doi  abstract   bibtex   
The ceramic matrix carbon fibre (CMC) reinforced composite has received great attention for use in aerospace engineering. In aerospace, the atmosphere is highly oxidative and experiences very high temperature. In addition to this, the materials require high thermal stability and high abrasion resistance in that atmosphere. The C/C–SiC composite meets with these requirements. In this paper, the C/C–SiC composite by liquid silicon infiltration is reviewed thoroughly.
@article{patel_high_2012,
	title = {High temperature {C}/{C}–{SiC} composite by liquid silicon infiltration: a literature review},
	volume = {35},
	issn = {0973-7669},
	doi = {10.1007/s12034-011-0247-5},
	abstract = {The ceramic matrix carbon fibre (CMC) reinforced composite has received great attention for use in aerospace engineering. In aerospace, the atmosphere is highly oxidative and experiences very high temperature. In addition to this, the materials require high thermal stability and high abrasion resistance in that atmosphere. The C/C–SiC composite meets with these requirements. In this paper, the C/C–SiC composite by liquid silicon infiltration is reviewed thoroughly.},
	number = {1},
	journal = {Bulletin of Materials Science},
	author = {PATEL, MANISH and SAURABH, KUMAR and PRASAD, V. V. BHANU and SUBRAHMANYAM, J.},
	month = feb,
	year = {2012},
	pages = {63--73},
}

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