Aerospace Materials: CLAD 7075 SHEET T6 and 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) | 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 T6 AND T62 0.008-0.011 S | 70 | 10.3 | 10.2 | — | — | — | — | — | — | — | — | 68 | — | 58 | S | T6 and T62 | 0.101 | 5 | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.008-0.011 |
| CLAD 7075 SHEET T6 AND T62 0.012-0.039 A | 70 | 10.3 | 10.2 | 108 | 140 | 90 | 105 | 61 | 64 | 42 | 70 | 70 | 62 | 60 | A | T6 and T62 | 0.101 | 7 | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.012-0.039 |
| CLAD 7075 SHEET T6 AND T62 0.012-0.039 B | 70 | 10.3 | 10.2 | 115 | 148 | 94 | 110 | 64 | 67 | 44 | 74 | 74 | 65 | 63 | B | T6 and T62 | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.012-0.039 |
| CLAD 7075 SHEET T6 AND T62 0.040-0.062 A | 70 | 10.3 | 10.2 | 110 | 142 | 91 | 106 | 62 | 65 | 42 | 71 | 71 | 63 | 61 | A | T6 and T62 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.040-0.062 |
| CLAD 7075 SHEET T6 AND T62 0.040-0.062 B | 70 | 10.3 | 10.2 | 116 | 150 | 96 | 112 | 65 | 68 | 45 | 75 | 75 | 66 | 64 | B | T6 and T62 | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.040-0.062 |
| CLAD 7075 SHEET T6 AND T62 0.063-0.187 A | 70 | 10.3 | 10.2 | 113 | 146 | 94 | 110 | 64 | 67 | 44 | 73 | 73 | 65 | 63 | A | T6 and T62 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.063-0.187 |
| CLAD 7075 SHEET T6 AND T62 0.063-0.187 B | 70 | 10.3 | 10.2 | 119 | 154 | 100 | 117 | 68 | 71 | 46 | 77 | 77 | 69 | 67 | B | T6 and T62 | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.063-0.187 |
| CLAD 7075 SHEET T6 AND T62 0.188-0.249 A | 70 | 10.3 | 10.2 | 116 | 150 | 96 | 112 | 65 | 68 | 45 | 75 | 75 | 66 | 64 | A | T6 and T62 | 0.101 | 8 | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.188-0.249 |
| CLAD 7075 SHEET T6 AND T62 0.188-0.249 B | 70 | 10.3 | 10.2 | 119 | 154 | 99 | 115 | 67 | 70 | 46 | 77 | 77 | 68 | 66 | B | T6 and T62 | 0.101 | — | Sheet | 0.33 | AMS-QQ-A-250/13 | 0.188-0.249 |
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