Ti-6Al-6V-2Sn

Verifiedmetal

Ti-6Al-6V-2Sn is a near-alpha titanium alloy containing 6% aluminum, 6% vanadium, and 2% tin, designed for elevated-temperature aerospace applications requiring moderate strength and creep resistance up to approximately 600°C. The alloy offers good fatigue performance and weldability with moderate density, making it suitable for jet engine components, airframes, and other high-temperature structural applications.

aerospacestructural

Compliance & Regulations

?ITAR?EAR?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65

Tempers & Conditions

Filter by
Form
PropertyValueUnitConditionsSource
Compressive Modulus(Ec)
ksi22°C · Sheet/Strip/Plate
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)2 entries
ksi22°C · Bar/Extrusion
ksi22°C · Sheet/Strip/Plate
S–N Curve (Wöhler)(S–N)
ksi9 entriesClick to expand
Young's Modulus(E)
ksi22°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.
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (17 pts)
µin/in·°F
Specific Heat vs Temperature(Cp(T))
Curve (17 pts)
BTU/(lb·°F)
Thermal Conductivity vs Temperature(k(T))
Curve (17 pts)
BTU/(hr·ft·°F)
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
lb/in³22°C
Verified Unverified Low confidence (<80%) Link to source

Regulatory Screening

Environmental

Export Control

Safety & Biocompatibility

Quality & Standards

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.