Aerospace Materials: 2219 SHEET T851
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) | Ftu ksi LT (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2219 SHEET T851 5.001-6.000 A | 70 | 10.5 | 10.8 | 57 | 42 | 4 | A | T851 | 0.103 | 4 | Sheet and plate | 0.33 | AMS-QQ-A-250/30 | 5.001-6.000 |
| 2219 SHEET T851 5.001-6.000 B | 70 | 10.5 | 10.8 | 58 | 43 | 4 | B | T851 | 0.103 | — | Sheet and plate | 0.33 | AMS-QQ-A-250/30 | 5.001-6.000 |
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