Ti10Si6C2 is a titanium-based ceramic composite or intermetallic compound containing silicon and carbon phases, likely developed for high-temperature structural applications. This material family bridges traditional titanium alloys and ceramic matrix composites, targeting environments where conventional Ti alloys lose strength but monolithic ceramics prove brittle. Research compounds of this type are primarily investigated for aerospace propulsion components, thermal protection systems, and high-temperature wear-resistant applications where weight savings and thermal stability are critical.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Band Gap(Eg) | 0.00120 | eV | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Formation Energy(ΔHf) | -0.7900 | eV/atom | — |