Aerospace Materials: CP-TI 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) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CP-TI EXTRUSION ANN 0.188-3.000 S T5 2 1 0c C1 | 70 | 15.5 | 16 | 40 | 30 | 6.5 | S | Annealed | 0.163 | Extruded bars and shapes | AMS-T-81556 | 0.188-3.000 |
| CP-TI EXTRUSION ANN 0.188-3.000 S T5 2 1 0c C2 | 70 | 15.5 | 16 | 50 | 40 | 6.5 | S | Annealed | 0.163 | Extruded bars and shapes | AMS-T-81556 | 0.188-3.000 |
| CP-TI EXTRUSION ANN 0.188-3.000 S T5 2 1 0c C3 | 70 | 15.5 | 16 | 65 | 55 | 6.5 | S | Annealed | 0.163 | Extruded bars and shapes | AMS-T-81556 | 0.188-3.000 |
| CP-TI EXTRUSION ANN 0.188-3.000 S T5 2 1 0c C4 | 70 | 15.5 | 16 | 80 | 70 | 6.5 | S | Annealed | 0.163 | Extruded bars and shapes | AMS-T-81556 | 0.188-3.000 |
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