Ti-15V-3Cr-3Sn-3Al STA is a metastable beta titanium alloy in solution-treated and aged condition, combining high strength (typically 1200-1400 MPa tensile strength) with excellent fracture toughness and damage tolerance for aerospace fasteners and structural components. The STA condition provides optimized strength-toughness balance through controlled precipitation hardening while maintaining good fatigue resistance and low-temperature impact properties required in critical airframe applications.
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6 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | 105.5 | GPa | 22°C · Sheet | ||
Compressive Tangent Modulus vs Stress(Etn(σ))2 entries | Curve (15 pts) | Pa | 21°C · L | ||
| ↳ | Curve (18 pts) | Pa | 21°C · LT | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))4 entries | Curve (16 pts) | Pa | 21°C · L | ||
| ↳ | Curve (15 pts) | Pa | 21°C · L | ||
| ↳ | Curve (16 pts) | Pa | 21°C · LT | ||
| ↳ | Curve (16 pts) | Pa | 21°C · LT | ||
Young's Modulus(E) | 104.8 | GPa | 22°C · Sheet |
3 interactive curves for this material
Stress-strain, S-N fatigue and environmental knockdown curves are free with an account.
Create free account| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (9 pts) | 1/K | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (16 pts) | J/(kg·K) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (16 pts) | W/(m·K) | — |
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 4.761 | kg/m³ | 22°C |