Aerospace Materials: 2024 EXTRUSION T3
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) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2024 EXTRUSION T3 3.000-4.499 B | 70 | 10.8 | 11 | 91 | 115 | 65 | 78 | 51 | 43 | 35 | 74 | 57 | 54 | 41 | 4.1 | B | T3, T3510, and T3511 | 0.1 | — | Extruded bar, rod, and shapes | 0.33 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | 3.000-4.499 |
| 2024 EXTRUSION T3 3.000-4.499 S | 70 | 10.8 | 11 | 84 | 106 | 57 | 69 | 45 | 38 | 32 | 68 | 52 | 48 | 36 | 4.1 | S | T3, T3510, and T3511 | 0.1 | 8 | Extruded bar, rod, and shapes | 0.33 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | 3.000-4.499 |
| 2024 EXTRUSION T3 LE0.249 A | 70 | 10.8 | 11 | 84 | 108 | 61 | 71 | 34 | 41 | 29 | 57 | 54 | 42 | 37 | 4.1 | A | T3, T3510, and T3511 | 0.1 | 12 | Extruded bar, rod, and shapes | 0.33 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | <=0.249 |
| 2024 EXTRUSION T3 LE0.249 B | 70 | 10.8 | 11 | 90 | 114 | 68 | 79 | 38 | 45 | 31 | 61 | 58 | 47 | 41 | 4.1 | B | T3, T3510, and T3511 | 0.1 | — | Extruded bar, rod, and shapes | 0.33 | AMS 4152, AMS 4164, AMS 4165, and AMS-QQ-A-200/3 | <=0.249 |
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