Aerospace Materials: CLAD 7075 PLATE T62
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) | Fcy ksi ST (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 | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 7075 PLATE T62 3.001-3.500 A | 70 | 10 | 10.3 | 104 | 128 | 86 | 100 | 53 | 55 | 57 | 40 | 66 | 69 | 65 | 50 | 56 | 54 | 3.9 | A | T62a | 5 | Plate | 0.33 | AMS-QQ-A-250/13 | 3.001-3.500b |
| CLAD 7075 PLATE T62 3.001-3.500 B | 70 | 10 | 10.3 | 107 | 132 | 89 | 104 | 55 | 57 | 59 | 42 | 68 | 71 | 67 | 52 | 58 | 55 | 3.9 | B | T62a | — | Plate | 0.33 | AMS-QQ-A-250/13 | 3.001-3.500b |
| CLAD 7075 PLATE T62 3.501-4.000 A | 70 | 10 | 10.3 | 98 | 121 | 80 | 93 | 48 | 50 | 53 | 38 | 62 | 65 | 61 | 46 | 52 | 50 | 3.9 | A | T62a | 3 | Plate | 0.33 | AMS-QQ-A-250/13 | 3.501-4.000b |
| CLAD 7075 PLATE T62 3.501-4.000 B | 70 | 10 | 10.3 | 101 | 124 | 84 | 97 | 50 | 52 | 55 | 39 | 64 | 67 | 63 | 48 | 54 | 52 | 3.9 | B | T62a | — | Plate | 0.33 | AMS-QQ-A-250/13 | 3.501-4.000b |
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