Ti2AlMo is an intermetallic compound based on titanium with aluminum and molybdenum additions, belonging to the family of titanium aluminides—a class of lightweight, high-temperature structural materials. This material is primarily of research and development interest for aerospace and high-temperature engine applications where weight reduction and elevated-temperature strength are critical; titanium aluminides in general offer superior specific strength compared to conventional titanium alloys at temperatures above 600°C, though they typically exhibit lower room-temperature ductility, making processing and application design more challenging than mature alloy systems.
Compliance & Regulations
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Bulk Modulus(K) | 21,871.7 | ksi | — | ||
Poisson's Ratio(ν) | 0.3600 | - | — | ||
Shear Modulus(G) | 6,935.7 | ksi | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.2051 | lb/in³ | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Band Gap(Eg) | 0.000 | eV | — | ||
Magnetic Moment(μB) | 0.000 | µB | — | ||
Seebeck Coefficient(S) | 29.24 | µV/K | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Energy Above Hull(ΔEhull) | 0.000 | eV/atom | — | ||
Formation Energy(ΔHf) | -0.3159 | eV/atom | — |