Aerospace Materials: 7150 EXTRUSION T61511
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 7150 EXTRUSION T61511 0.250-0.499 S | 70 | 10.4 | 11 | 119 | 152 | 100 | 118 | 80 | 80 | 44 | 87 | 80 | 82 | 73 | 4 | S | T61511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4307 | 0.250-0.499 |
| 7150 EXTRUSION T61511 0.500-0.749 S | 70 | 10.4 | 11 | 120 | 153 | 100 | 120 | 81 | 80 | 45 | 88 | 79 | 83 | 73 | 4 | S | T61511 | 0.102 | 9 | Extrusion | 0.33 | AMS 4307 | 0.500-0.749 |
| 7150 EXTRUSION T61511 0.750-0.999 S | 70 | 10.4 | 11 | 120 | 154 | 100 | 120 | 82 | 80 | 45 | 89 | 79 | 84 | 73 | 4 | S | T61511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4307 | 0.750-0.999 |
| 7150 EXTRUSION T61511 1.000-1.499 A | 70 | 10.4 | 11 | 118 | 152 | 96 | 117 | 82 | 77 | 44 | 89 | 85 | 83 | 77 | 4 | A | T61511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4307 | 1.000-1.499 |
| 7150 EXTRUSION T61511 1.500-2.000 S | 70 | 10.4 | 11 | 116 | 150 | 94 | 117 | 84 | 75 | 42 | 89 | 74 | 84 | 68 | 4 | S | T61511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4307 | 1.500-2.000 |
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