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Aerospace Materials: TI-8AL-1MO-1V SHEET ANN

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-8AL-1MO-1V SHEET ANN5 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fcy ksi LT (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)elongation pct LT (%)formpoisson ratiospecificationthickness range
TI-8AL-1MO-1V SHEET ANN 0.1875-0.500 S7017.5181451451351356.7SSingle Annealed0.1581010Sheet0.32AMS 4915, AMS-T-9046, and Comp A-40.1875-0.500
TI-8AL-1MO-1V SHEET ANN ANY S T5 3 2 0b2 C17017.518223269174191126126841351351201206.7SDuplex Annealed0.15888Sheet0.32AMS 4916, AMS-T-9046, and Comp. A-4
TI-8AL-1MO-1V SHEET ANN ANY S T5 3 2 0b2 C27017.518223269174191126126841351351201206.7SDuplex Annealed0.1581010Sheet0.32AMS 4916, AMS-T-9046, and Comp. A-4
TI-8AL-1MO-1V SHEET ANN ANY S T5 3 2 0b2 C37017.5181301301201206.7SDuplex Annealed0.1581010Sheet0.32AMS 4916, AMS-T-9046, and Comp. A-4
TI-8AL-1MO-1V SHEET ANN LT0.1875 S7017.518239294196214144149931451451351356.7SSingle Annealed0.158Sheet0.32AMS 4915, AMS-T-9046, and Comp A-4< 0.1875

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