The current applications of C-C composites extend to aircraft brakes, rocket nozzles, missile nosetips, and leading edges of the Space Shuttle. More advanced, secondary and even primary structure applications in cyclic, high-temperature oxidizing environments depend on effective oxidation protection for repeated missions. Accounts are presently given of state-of-the-art methods in substrate fabrication, carbon deposition, and SiC and Si3N4 protective coatings. Attention is given to current levels of high temperature oxidation protection for various mission and vehicle types, as well as to performance projections for C-C composites used by a representative National Aerospace Plane airframe structure. Future technology requirements in C-C composites are projected.
Carbon-carbon composites
1992-01-01
Miscellaneous
No indication
English
Tema Archive | 1986
|Secondary Bonding of Carbon/Carbon Composites
AIAA | 1979
|Oxidation model for carbon-carbon composites
AIAA | 1992
|Joint Structures of Carbon-Carbon Composites
British Library Conference Proceedings | 1996
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