| CMC Material Systems & Applications |
| |
| Material |
MI SiC-SiC Hi Per-Comp® |
CVI C/SiC (Novoltex)® |
CVI C/SiC (T-300)® |
| Primary Application |
Turbine Engine Hot Section - Aviation & Stationary |
Rocket Propulsion Hot Gas Path |
RLV/SOV Airframe |
| Typical Components |
Vanes Blades Shrouds Liners |
Hot gas valves Exit nozzles |
Control surfaces TPS panels |
| Temperature |
2200° - 2400° F |
3500° - 4500° F |
2800°° - 3000° F |
| Life Requirements |
Up to 48,000 hrs |
10-1000 sec |
100+ hrs |
| Density |
175 lb/ft3 |
135 lb/ft3 |
135 lb/ft3 |
| Benefits |
Temperature capability super alloys Light weight Thermally conductive |
Erosion resistant Light weight Complex features |
High specific strength Environmental durability |
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| Materials for a wide range of extreme environments |