SiC/SiC CMC (ceramic matrix composite) with Hi-Nicalon S fibers reinforced by chemical vapor infiltration (CVI) is an advanced ceramic composite that combines silicon carbide fibers within a silicon carbide matrix, engineered to retain strength and damage tolerance at extreme temperatures where monolithic ceramics fail. This material is used in aerospace propulsion (jet engine hot sections, combustor liners), industrial gas turbines, and thermal protection systems where lightweight performance and thermal cycling resistance are critical; it outperforms traditional superalloys and unreinforced ceramics by maintaining structural integrity under thermal shock and providing graceful failure modes rather than brittle fracture.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Tensile Strength(σUTS)2 entries | 44.96 | ksi | 20°C | ||
| ↳ | 42.06 | ksi | 1000°C | ||
Young's Modulus(E) | 36,259.4 | ksi | 20°C |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Thermal Conductivity(k)2 entries | 8.667 | BTU/(hr·ft·°F) | 20°C | ||
| ↳ | 4.622 | BTU/(hr·ft·°F) | 1000°C |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data