Ti5Re24 is a titanium-rhenium alloy containing approximately 5% titanium and 24% rhenium, representing a high-density refractory metal composite designed for extreme-temperature applications. This alloy is primarily investigated for aerospace and defense applications where conventional superalloys reach their performance limits, particularly in rocket engines, hypersonic vehicle structures, and next-generation jet propulsion systems where exceptional strength retention at elevated temperatures is critical. The rhenium addition significantly improves high-temperature creep resistance and ductility compared to pure refractory metals, making it notable for engineers working on materials that must perform in the 1200–1600°C range where nickel superalloys become inadequate.
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 17.30 | kg/m³ | DFT · OptB88vdW |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Band Gap(Eg) | 0.000 | eV | DFT · OptB88vdW | ||
Magnetic Moment(μB) | 0.000 | µB | DFT · OptB88vdW |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Energy Above Hull(ΔEhull) | 0.000 | eV/atom | DFT · OptB88vdW | ||
Formation Energy(ΔHf) | -0.2231 | eV/atom | DFT · OptB88vdW |
Reference data from cited sources. Not verified or certified by MatWorld Inc. Verify against the source before use in design. Terms: engineering data