Aerospace Materials: 7075 PLATE T7351
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 | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 7075 PLATE T7351 2.501-3.000 B | 70 | 10.3 | 10.6 | 103 | 132 | 81 | 96 | 51 | 55 | 55 | 39 | 65 | 66 | 62 | 53 | 53 | 50 | 3.9 | B | T7351 | 0.101 | — | Plate | 0.33 | AMS 4078 and AMS-QQ-A-250/12 | 2.501-3.000 |
| 7075 PLATE T7351 3.001-3.500 S | 70 | 10.3 | 10.6 | 99 | 127 | 76 | 89 | 47 | 51 | 50 | 38 | 62 | 63 | 59 | 49 | 49 | 47 | 3.9 | S | T7351 | 0.101 | 6 | Plate | 0.33 | AMS 4078 and AMS-QQ-A-250/12 | 3.001-3.500 |
| 7075 PLATE T7351 3.501-4.000 S | 70 | 10.3 | 10.6 | 96 | 124 | 76 | 88 | 45 | 50 | 48 | 37 | 60 | 61 | 57 | 48 | 48 | 46 | 3.9 | S | T7351 | 0.101 | 6 | Plate | 0.33 | AMS 4078 and AMS-QQ-A-250/12 | 3.501-4.000 |
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