Aerospace Materials: TI-8AL-1MO-1V BAR 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).
| material id | temp f | E 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) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | elongation pct ST (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-8AL-1MO-1V BAR ANN 2.501-4.000 S | 70 | 17.5 | 18 | 120 | 120 | 120 | 110 | 110 | 110 | 6.7 | S | Duplex annealed | 0.158 | 10 | 10 | 8 | Bar | 0.32 | MIL-T-9047 | 2.501-4.000a |
| TI-8AL-1MO-1V BAR ANN LT2.500 S | 70 | 17.5 | 18 | 130 | 130 | — | 120 | 120 | — | 6.7 | S | Duplex annealed | 0.158 | 10 | 10 | — | Bar | 0.32 | MIL-T-9047 | < 2.500a |
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