Aerospace Materials: 2014 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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2014 PLATE T62 0.250-0.499 A | 70 | 10.7 | 10.9 | 100 | 127 | 84 | 99 | 59 | 60 | 37 | 65 | 67 | 57 | 59 | 4 | A | T62b | 7 | Platea | 0.33 | AMS 4028 | 0.250-0.499 |
| 2014 PLATE T62 0.250-0.499 B | 70 | 10.7 | 10.9 | 103 | 131 | 87 | 103 | 61 | 62 | 39 | 67 | 69 | 59 | 61 | 4 | B | T62b | — | Platea | 0.33 | AMS 4028 | 0.250-0.499 |
| 2014 PLATE T62 0.500-1.000 A | 70 | 10.7 | 10.9 | 100 | 127 | 84 | 99 | 59 | 60 | 37 | 65 | 67 | 57 | 59 | 4 | A | T62b | 6 | Platea | 0.33 | AMS 4028 | 0.500-1.000 |
| 2014 PLATE T62 0.500-1.000 B | 70 | 10.7 | 10.9 | 103 | 131 | 87 | 103 | 61 | 62 | 39 | 67 | 69 | 59 | 61 | 4 | B | T62b | — | Platea | 0.33 | AMS 4028 | 0.500-1.000 |
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