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
01.01.1992
Sonstige
Keine Angabe
Englisch
Tema Archiv | 1986
|Secondary Bonding of Carbon/Carbon Composites
AIAA | 1979
|Oxidation model for carbon-carbon composites
AIAA | 1992
|Recent developments in carbon-carbon composites
Tema Archiv | 1998
|Secondary bonding of carbon/carbon composites
AIAA | 1978
|