Ti-6Al-2Sn-4Zr-2Mo

Verifiedmetal

Ti-6Al-2Sn-4Zr-2Mo is a near-alpha titanium alloy combining aluminum, tin, zirconium, and molybdenum additions for elevated temperature strength and creep resistance; used primarily in compressor and fastener applications in military and commercial jet engines operating up to ~600°C with good fatigue and stress-rupture performance.

aerospacestructural

Compliance & Regulations

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

Tempers & Conditions

PropertyValueUnitConditionsSource
Compressive Modulus(Ec)2 entries
Pa22°C · Sheet
Curve (17 pts)
Pa
Poisson's Ratio(ν)
-22°C
Shear Modulus(G)
Pa22°C · Sheet
Young's Modulus(E)
Pa22°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.
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
CTE vs Temperature(α(T))
Curve (15 pts)
1/K
Specific Heat vs Temperature(Cp(T))
Curve (17 pts)
J/(kg·K)
Thermal Conductivity vs Temperature(k(T))
Curve (17 pts)
W/(m·K)
Verified Unverified Low confidence (<80%) Link to source
PropertyValueUnitConditionsSource
Density(ρ)
kg/m³22°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.