Ti-6Al-6V-2Sn Annealed
VerifiedmetalTi-6Al-6V-2Sn is a near-alpha titanium alloy combining aluminum and vanadium for strength with tin for elevated-temperature stability, commonly used in gas turbine engines and airframes requiring sustained performance to approximately 600°C. The annealed condition provides a stable microstructure with moderate strength and good ductility, suitable for components requiring damage tolerance and fracture toughness over maximum strength.
aerospacestructural
Compliance & Regulations
?ITAR?EAR?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
Property OverviewNormalized to typical max values
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Specification
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Ultimate Bearing Strength(Fbru) | 218 – 317 | ksi | 14 entriesClick to expand | ||
Bearing Yield Strength(Fbry) | 193 – 240 | ksi | 14 entriesClick to expand | ||
Compressive Modulus(Ec) | 16,400 | ksi | 22°C · Sheet/Strip/Plate | ||
Compressive Tangent Modulus vs Stress(Etn(σ)) | Curve (12 pts) | ksi | 21°C · L | ||
Compressive Yield Strength(Fcy) | 135 – 151 | ksi | 18 entriesClick to expand | ||
Elongation at Break(εf) | 6.000 – 10.00 | - | 28 entriesClick to expand | ||
Poisson's Ratio(ν) | 0.3100 | - | 22°C | ||
Reduction of Area(RA) | 15.00 – 20.00 | - | 16 entriesClick to expand | ||
Shear Modulus(G) | 6,000 | ksi | 22°C · Bar/Extrusion | ||
Ultimate Shear Strength(Fsu) | 91.00 – 97.00 | ksi | 8 entriesClick to expand | ||
S–N Curve (Wöhler)(S–N) | — | ksi | 9 entriesClick to expand | ||
Stress–Strain Curve(σ–ε)2 entries | Curve (18 pts) | ksi | 21°C · L | ||
| ↳ | Curve (18 pts) | ksi | 21°C · LT | ||
Stress–Strain Curve (buckling region, ≤ 2% strain)(σ–ε (low-strain))2 entries | Curve (9 pts) | ksi | 21°C · L | ||
| ↳ | Curve (9 pts) | ksi | 21°C · L | ||
Ultimate Tensile Strength(σUTS) | 136 – 160 | ksi | 40 entriesClick to expand | ||
Yield Strength (0.2% offset)(σy) | 123 – 154 | ksi | 40 entriesClick to expand | ||
Young's Modulus(E) | 16,000 | ksi | 22°C · Sheet/Strip/Plate | ||
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 (7 pts) | µin/in·°F | — | ||
Specific Heat vs Temperature(Cp(T)) | Curve (4 pts) | BTU/(lb·°F) | — | ||
Thermal Conductivity vs Temperature(k(T)) | Curve (5 pts) | BTU/(hr·ft·°F) | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | 0.1640 | lb/in³ | 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.