Aerospace Materials: TI-8AL-1MO-1V PLATE 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 PLATE ANN 0.501-1.000 S | 70 | 17.5 | 18 | 140 | 140 | — | 130 | 130 | — | 6.7 | S | Single Annealed | 0.158 | 10 | 10 | — | Plate | 0.32 | AMS 4915, AMS-T-9046, and Comp A-4 | 0.501-1.000 |
| TI-8AL-1MO-1V PLATE ANN 1.001-2.500 S | 70 | 17.5 | 18 | 130 | 130 | — | 120 | 120 | — | 6.7 | S | Single Annealed | 0.158 | 10 | 10 | — | Plate | 0.32 | AMS 4915, AMS-T-9046, and Comp A-4 | 1.001-2.500 |
| TI-8AL-1MO-1V PLATE ANN 2.501-4.000 S | 70 | 17.5 | 18 | 120 | 120 | 120 | 110 | 110 | 110 | 6.7 | S | Single Annealed | 0.158 | 8 | 8 | 8 | Plate | 0.32 | AMS 4915, AMS-T-9046, and Comp A-4 | 2.501-4.000 |
| TI-8AL-1MO-1V PLATE ANN ANY S T5 3 2 0b2 C4 | 70 | 17.5 | 18 | 130 | 130 | — | 120 | 120 | — | 6.7 | S | Duplex Annealed | 0.158 | 10 | 10 | — | Plate | 0.32 | AMS 4916, AMS-T-9046, and Comp. A-4 | — |
| TI-8AL-1MO-1V PLATE ANN ANY S T5 3 2 0b2 C5 | 70 | 17.5 | 18 | 125 | 125 | — | 115 | 115 | — | 6.7 | S | Duplex Annealed | 0.158 | 10 | 10 | — | Plate | 0.32 | AMS 4916, AMS-T-9046, and Comp. A-4 | — |
| TI-8AL-1MO-1V PLATE ANN ANY S T5 3 2 0b2 C6 | 70 | 17.5 | 18 | 120 | 120 | — | 110 | 110 | — | 6.7 | S | Duplex Annealed | 0.158 | 8 | 8 | — | Plate | 0.32 | AMS 4916, AMS-T-9046, and Comp. A-4 | — |
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