Aerospace Materials: 2219 SHEET 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 | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2219 SHEET T62 0.020-2.000 A | 70 | 10.5 | 10.8 | 84 | 107 | 62 | 79 | 37 | 37 | 31 | 54 | 54 | 36 | 36 | 4 | A | T62a | 0.103 | Sheet and plate | 0.33 | AMS 4031 & AMS-QQ-A-250/30 | 0.020-2.000 |
| 2219 SHEET T62 0.020-2.000 B | 70 | 10.5 | 10.8 | 85 | 109 | 64 | 81 | 39 | 38 | 32 | 55 | 55 | 37 | 37 | 4 | B | T62a | 0.103 | Sheet and plate | 0.33 | AMS 4031 & AMS-QQ-A-250/30 | 0.020-2.000 |
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