Aerospace Materials: TI-5AL-2.5SN 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) | Ftu ksi (ksi) | Fty ksi (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| TI-5AL-2.5SN EXTRUSION ANN 0.188-1.000 S | 70 | 15.5 | 15.5 | 120 | 115 | S | Annealed | 0.162 | 10 | Extruded bars and shapes | AMS-T-81556, Comp. A-1 | 0.188-1.000 |
| TI-5AL-2.5SN EXTRUSION ANN 1.001-2.000 S | 70 | 15.5 | 15.5 | 115 | 110 | S | Annealed | 0.162 | 10 | Extruded bars and shapes | AMS-T-81556, Comp. A-1 | 1.001-2.000 |
| TI-5AL-2.5SN EXTRUSION ANN 2.001-3.000 S | 70 | 15.5 | 15.5 | 115 | 110 | S | Annealed | 0.162 | 8 | Extruded bars and shapes | AMS-T-81556, Comp. A-1 | 2.001-3.000 |
| TI-5AL-2.5SN EXTRUSION ANN 3.001-4.000 S | 70 | 15.5 | 15.5 | 115 | 110 | S | Annealed | 0.162 | 6 | Extruded bars and shapes | AMS-T-81556, Comp. A-1 | 3.001-4.000 |
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