Aerospace Materials: TI-6AL-6V-2SN EXTRUSION 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).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Fcy ksi (ksi) | Fcy ksi LT (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 STA 0.188-0.500 S | 70 | 16 | 16.4 | 165 | 165 | 170 | 170 | 160 | 160 | 6.2 | 15 | 12 | S | Solution treated and aged | 0.164 | 8 | 6 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 0.188-0.500 |
| TI-6AL-6V-2SN EXTRUSION STA 0.501-1.500 S | 70 | 16 | 16.4 | 160 | 160 | 165 | 165 | 155 | 155 | 6.2 | 15 | 12 | S | Solution treated and aged | 0.164 | 8 | 6 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 0.501-1.500 |
| TI-6AL-6V-2SN EXTRUSION STA 1.501-2.500 S | 70 | 16 | 16.4 | 155 | 155 | 160 | 160 | 150 | 150 | 6.2 | 15 | 12 | S | Solution treated and aged | 0.164 | 8 | 6 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 1.501-2.500 |
| TI-6AL-6V-2SN EXTRUSION STA 2.501-4.000 S | 70 | 16 | 16.4 | 145 | 145 | 150 | 150 | 140 | 140 | 6.2 | 15 | 12 | S | Solution treated and aged | 0.164 | 8 | 6 | Extruded bar and shapes | 0.31 | MIL-T-81556 & AMS-T-81556, Comp. AB-3 | 2.501-4.000 |
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