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Aerospace Materials: TI-6AL-2SN-4ZR-2MO BAR STA

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial id: TI-6AL-2SN-4ZR-2MO BAR STA2 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Ftu ksi (ksi)Ftu ksi LT (ksi)Ftu ksi ST (ksi)Fty ksi (ksi)Fty ksi LT (ksi)Fty ksi ST (ksi)G Msi (Msi)RA pct (%)RA pct LT (%)RA pct ST (%)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)elongation pct ST (%)formpoisson ratiospecification
TI-6AL-2SN-4ZR-2MO BAR STA ANY A7016.5181301301301201201206.2252525ASTA (Duplex annealed)0.164101010Bar0.32AMS 4975
TI-6AL-2SN-4ZR-2MO BAR STA ANY B7016.5181441316.2BSTA (Duplex annealed)0.164Bar0.32AMS 4975

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