Aerospace Materials: 7150 EXTRUSION T77511
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 T77511 0.250-0.499 A | 70 | 10.4 | 10.9 | 124 | 161 | 105 | 124 | 82 | 80 | 45 | 87 | 82 | 82 | 76 | 4 | A | T77511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4345 | 0.250-0.499 |
| 7150 EXTRUSION T77511 0.250-0.499 B | 70 | 10.4 | 10.9 | 127 | 165 | 108 | 127 | 85 | 82 | 46 | 89 | 86 | 84 | 79 | 4 | B | T77511 | 0.102 | — | Extrusion | 0.33 | AMS 4345 | 0.250-0.499 |
| 7150 EXTRUSION T77511 0.500-0.749 S | 70 | 10.4 | 10.9 | 125 | 162 | 106 | 125 | 83 | 81 | 46 | 88 | 83 | 83 | 79 | 4 | S | T77511 | 0.102 | 9 | Extrusion | 0.33 | AMS 4345 | 0.500-0.749 |
| 7150 EXTRUSION T77511 0.750-2.000 S | 70 | 10.4 | 10.9 | 123 | 159 | 108 | 127 | 84 | 82 | 46 | 89 | 83 | 84 | 78 | 4 | S | T77511 | 0.102 | 8 | Extrusion | 0.33 | AMS 4345 | 0.750-2.000 |
| 7150 EXTRUSION T77511 LE0.249 A | 70 | 10.4 | 10.9 | 122 | 158 | 100 | 118 | 78 | 76 | 44 | 85 | 81 | 78 | 74 | 4 | A | T77511 | 0.102 | 7 | Extrusion | 0.33 | AMS 4345 | <=0.249 |
| 7150 EXTRUSION T77511 LE0.249 B | 70 | 10.4 | 10.9 | 126 | 163 | 106 | 125 | 82 | 81 | 46 | 88 | 84 | 83 | 79 | 4 | B | T77511 | 0.102 | — | Extrusion | 0.33 | AMS 4345 | <=0.249 |
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