Ti-15V-3Cr-3Sn-3Al
VerifiedmetalTi-15V-3Cr-3Sn-3Al is a metastable beta titanium alloy designed for high-strength aerospace applications requiring excellent damage tolerance and fatigue resistance. The alloy offers tensile strengths exceeding 150 ksi with good fracture toughness, making it suitable for aircraft fuselage structure, fasteners, and landing gear components.
aerospacestructural
Compliance & Regulations
?ITAR?EAR?ISO 10993?Conflict Free?RoHS?REACH?TSCA?Prop 65
Tempers & Conditions
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Compressive Modulus(Ec) | — | ksi | 22°C · Sheet | — | |
Young's Modulus(E) | — | ksi | 22°C · Sheet | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
CTE vs Temperature(α(T)) | Curve (16 pts) | µin/in·°F | — | — | |
Specific Heat vs Temperature(Cp(T)) | Curve (16 pts) | BTU/(lb·°F) | — | — | |
Thermal Conductivity vs Temperature(k(T)) | Curve (16 pts) | BTU/(hr·ft·°F) | — | — |
Verified Unverified Low confidence (<80%) Link to source
| Property | Value | Unit | Conditions | Source | |
|---|---|---|---|---|---|
Density(ρ) | — | lb/in³ | 22°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.