Aerospace Materials: 7150 PLATE T7751
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) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 7150 PLATE T7751 0.250-0.499 S | 70 | 10.3 | 10.7 | 119 | 154 | 102 | 117 | 74 | 77 | 46 | 80 | 80 | — | 74 | 74 | — | 3.9 | S | T7751 | 0.102 | 8 | 8 | Plate | 0.33 | AMS 4252 | 0.250-0.499 |
| 7150 PLATE T7751 0.500-0.749 S | 70 | 10.3 | 10.7 | 124 | 160 | 105 | 120 | 76 | 79 | 47 | 83 | 83 | — | 77 | 76 | — | 3.9 | S | T7751 | 0.102 | 8 | 8 | Plate | 0.33 | AMS 4252 | 0.500-0.749 |
| 7150 PLATE T7751 0.750-1.500 S | 70 | 10.3 | 10.7 | 125 | 162 | 106 | 121 | 77 | 81 | 48 | 84 | 84 | — | 78 | 77 | — | 3.9 | S | T7751 | 0.102 | 8 | 8 | Plate | 0.33 | AMS 4252 | 0.750-1.500 |
| 7150 PLATE T7751 1.501-3.000 A | 70 | 10.3 | 10.7 | 122 | 158 | 104 | 118 | 75 | 79 | 47 | 82 | 82 | 77 | 76 | 75 | 67 | 3.9 | A | T7751 | 0.102 | 7 | 6 | Plate | 0.33 | AMS 4252 | 1.501-3.000 |
| 7150 PLATE T7751 1.501-3.000 B | 70 | 10.3 | 10.7 | 125 | 162 | 108 | 123 | 77 | 82 | 48 | 84 | 84 | 81 | 78 | 77 | 71 | 3.9 | B | T7751 | 0.102 | 6 | 1 | Plate | 0.33 | AMS 4252 | 1.501-3.000 |
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