Aerospace Materials: 5086 EXTRUSION 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) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 5086 EXTRUSION UNK LE5.000 S T3 5 3 0b C12 | 70 | 10.2 | 10.4 | 35 | 14 | 3.85 | S | 0.096 | 14 | Extrusion | 0.33 | AMS-QQ-A-200/5 | <=5.000a |
| 5086 EXTRUSION UNK LE5.000 S T3 5 3 0b C13 | 70 | 10.2 | 10.4 | 36 | 21 | 3.85 | S | 0.096 | 12 | Extrusion | 0.33 | AMS-QQ-A-200/5 | <=5.000a |
| 5086 EXTRUSION UNK LE5.000 S T3 5 3 0b C14 | 70 | 10.2 | 10.4 | 35 | 14 | 3.85 | S | 0.096 | 12 | Extrusion | 0.33 | AMS-QQ-A-200/5 | <=5.000a |
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