Aerospace Materials: 2219 EXTRUSION T8511
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) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2219 EXTRUSION T8511 ANY S T3 2 8 0d C1 | 70 | 10.5 | 10.8 | 87 | 113 | 69 | 84 | 43 | 43 | 33 | 58 | 56 | 42 | 39 | 4 | S | T8511 | 0.103 | 6 | 4 | Extruded shapes | 0.33 | AMS 4162 and AMS 4163a |
| 2219 EXTRUSION T8511 ANY S T3 2 8 0d C2 | 70 | 10.5 | 10.8 | 81 | 107 | 67 | 82 | 42 | 41 | 33 | 58 | 56 | 42 | 39 | 4 | S | T8511 | 0.103 | 6 | 4 | Extruded shapes | 0.33 | AMS 4162 and AMS 4163a |
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