Aerospace Materials: TI-6AL-6V-2SN EXTRUSION 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) | 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) | RA pct (%) | RA pct LT (%) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-6AL-6V-2SN EXTRUSION ANN 2.000 A | 70 | 16 | 16.4 | 218 | 268 | 196 | 227 | 137 | 136 | 93 | 142 | 141 | 129 | 128 | 6.2 | 20 | 15 | A | Annealed | 0.164 | 10 | 8 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 2.000 |
| TI-6AL-6V-2SN EXTRUSION ANN 2.000 B | 70 | 16 | 16.4 | 229 | 281 | 203 | 235 | 144 | 142 | 97 | 148 | 148 | 135 | 135 | 6.2 | — | — | B | Annealed | 0.164 | — | — | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 2.000 |
| TI-6AL-6V-2SN EXTRUSION ANN 2.001-3.000 S | 70 | 16 | 16.4 | — | — | — | — | 140 | 140 | — | 145 | 145 | 135 | 135 | 6.2 | 20 | 15 | S | Annealed | 0.164 | 10 | 8 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 2.001-3.000 |
| TI-6AL-6V-2SN EXTRUSION ANN 3.001-4.000 S | 70 | 16 | 16.4 | — | — | — | — | 135 | 135 | — | 140 | 140 | 130 | 130 | 6.2 | 20 | 15 | S | Annealed | 0.164 | 10 | 8 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 3.001-4.000 |
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