Aerospace Materials: 2219 SHEET UNK
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 | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2219 SHEET UNK 0.020-0.039 A | 70 | 10.5 | 10.8 | 99 | 126 | 83 | 96 | 52 | 55 | 36 | 63 | 64 | 51 | 52 | 4 | A | 0.103 | 5 | Sheet | 0.33 | AMS-QQ-A-250/30 | 0.020-0.039 |
| 2219 SHEET UNK 0.020-0.039 B | 70 | 10.5 | 10.8 | 100 | 128 | 85 | 98 | 53 | 56 | 37 | 64 | 65 | 52 | 53 | 4 | B | 0.103 | — | Sheet | 0.33 | AMS-QQ-A-250/30 | 0.020-0.039 |
| 2219 SHEET UNK 0.040-0.249 A | 70 | 10.5 | 10.8 | 99 | 126 | 83 | 96 | 52 | 55 | 36 | 63 | 64 | 51 | 52 | 4 | A | 0.103 | 6 | Sheet | 0.33 | AMS-QQ-A-250/30 | 0.040-0.249 |
| 2219 SHEET UNK 0.040-0.249 B | 70 | 10.5 | 10.8 | 100 | 128 | 85 | 98 | 53 | 56 | 37 | 64 | 65 | 52 | 53 | 4 | B | 0.103 | — | Sheet | 0.33 | AMS-QQ-A-250/30 | 0.040-0.249 |
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