Ti-15V-3Cr-3Sn-3Al STA (1000°F/8 Hrs.)
VerifiedmetalTi-15V-3Cr-3Sn-3Al is a near-beta titanium alloy designed for high-strength applications requiring excellent damage tolerance and formability, with applications in aerospace fasteners, springs, and structural components. The STA (solution treated and aged at 1000°F for 8 hours) condition provides optimized strength and ductility balance, typically yielding tensile strengths in the 140-160 ksi range with good fatigue resistance and fracture toughness retention.
aerospacestructural
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e/D Ratio
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| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru)2 entries | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · t=≤0.125 in · e/D=1.5 | — | |
| ↳ | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · t=≤0.125 in · e/D=2 | — | |
Bearing Yield Strength(Fbry)2 entries | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · t=≤0.125 in · e/D=1.5 | — | |
| ↳ | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · t=≤0.125 in · e/D=2 | — | |
Compressive Modulus(Ec) | — | Pa | 22°C · Sheet | — | |
Compressive Yield Strength(Fcy)2 entries | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · L · t=≤0.125 in | — | |
| ↳ | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · LT · t=≤0.125 in | — | |
Elongation at Break(εf)2 entries | — | - | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · L · t=≤0.125 in | — | |
| ↳ | — | - | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · LT · t=≤0.125 in | — | |
Ultimate Shear Strength(Fsu) | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · t=≤0.125 in | — | |
Ultimate Tensile Strength(σUTS)2 entries | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · L · t=≤0.125 in | — | |
| ↳ | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · LT · t=≤0.125 in | — | |
Yield Strength (0.2% offset)(σy)2 entries | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · L · t=≤0.125 in | — | |
| ↳ | — | Pa | 22°C · Sheet · STA (1000°F/8 Hrs.) · AMS 4914 · LT · t=≤0.125 in | — | |
Young's Modulus(E) | — | Pa | 22°C · Sheet | — |
N entriesMultiple entries per property — large groups are collapsed; click a summary row to expand. Use filters above to narrow by form / heat treatment / basis.
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (16 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) | — | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | kg/m³ | 22°C | — |
Rows with are inherited from the base material
Verified Unverified Low confidence (<80%) Link to source
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RoHS, REACH, and Prop 65 statuses are validated against official substance lists (ECHA SVHC Candidate List, OEHHA Prop 65, RoHS Annex II). Other regulations are estimated from composition and material classification. All screening is a starting point for due diligence — always verify with your supplier before making compliance decisions.