Aerospace Materials: 5083 EXTRUSION H111
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) | Fbry ksi (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 5083 EXTRUSION H111 0.501-5.000 S | 70 | 10.2 | 10.4 | 16 | 24 | 16 | 24 | 3.35 | S | H111 | 0.096 | Extrusion | 0.33 | AMS-QQ-A-200/4 | 0.501-5.000a |
| 5083 EXTRUSION H111 LT0.500 S | 70 | 10.2 | 10.4 | — | 32 | — | 40 | 3.35 | S | H111 | 0.096 | Extrusion | 0.33 | AMS-QQ-A-200/4 | <0.500a |
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