Aerospace Materials: 7050 EXTRUSION T73511
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 7050 EXTRUSION T73511 1.001-2.000 S | 70 | 10.3 | 10.7 | 100 | 129 | 80 | 95 | 60 | 59 | 39 | 70 | 66 | 60 | 56 | 3.9 | S | T73511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4341 | 1.001-2.000 |
| 7050 EXTRUSION T73511 2.001-3.000 S | 70 | 10.3 | 10.7 | 96 | 124 | 78 | 93 | 60 | 58 | 38 | 70 | 65 | 60 | 55 | 3.9 | S | T73511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4341 | 2.001-3.000 |
| 7050 EXTRUSION T73511 3.001-4.000 S | 70 | 10.3 | 10.7 | 91 | 120 | 76 | 91 | 61 | 56 | 37 | 70 | 63 | 60 | 53 | 3.9 | S | T73511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4341 | 3.001-4.000 |
| 7050 EXTRUSION T73511 4.001-5.000 S | 70 | 10.3 | 10.7 | 87 | 115 | 74 | 88 | 61 | 55 | 36 | 70 | 62 | 60 | 52 | 3.9 | S | T73511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4341 | 4.001-5.000 |
| 7050 EXTRUSION T73511 LE1.000 S | 70 | 10.3 | 10.7 | 103 | 133 | 82 | 97 | 60 | 60 | 39 | 70 | 68 | 60 | 57 | 3.9 | S | T73511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4341 | <=1.000 |
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