Aerospace Materials: 7075-T6 PLATE
-65 to 300
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) | Fbru ksi (ksi) | Fcy ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | elongation pct (%) | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|
| 7075-T6 PLATE | -65 | 10.5 | 152 | 73 | 49 | 84 | 73 | 10 | QQ-A-250/13 | 0.250-2.000 in |
| 7075-T6 PLATE | 70 | 10.4 | 142 | 68 | 46 | 78 | 68 | 8 | QQ-A-250/13 | 0.250-2.000 in |
| 7075-T6 PLATE | 212 | 9.9 | 122 | 55 | 39 | 68 | 55 | 9 | QQ-A-250/13 | 0.250-2.000 in |
| 7075-T6 PLATE | 250 | 9.7 | 112 | 47 | 35 | 62 | 47 | 9 | QQ-A-250/13 | 0.250-2.000 in |
| 7075-T6 PLATE | 300 | 9.3 | 80 | 30 | 25 | 44 | 30 | 12 | QQ-A-250/13 | 0.250-2.000 in |
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