Aerospace Materials: CLAD 7075 SHEET T76
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) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 7075 SHEET T76 0.040-0.062 S | 70 | 10 | 10.3 | 103 | 133 | 80 | 92 | 55 | 59 | 41 | 66 | 67 | 56 | 56 | S | T76 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/25 | 0.040-0.062 |
| CLAD 7075 SHEET T76 0.063-0.187 S | 70 | 10 | 10.3 | 104 | 135 | 81 | 94 | 56 | 60 | 40 | 67 | 68 | 57 | 57 | S | T76 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/25 | 0.063-0.187 |
| CLAD 7075 SHEET T76 0.188-0.249 S | 70 | 10 | 10.3 | 107 | 139 | 84 | 97 | 58 | 62 | 40 | 69 | 70 | 59 | 59 | S | T76 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/25 | 0.188-0.249 |
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