Aerospace Materials: MG-AZ61A EXTRUSION F
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) | Fsu ksi (ksi) | Ftu ksi (ksi) | Fty ksi (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MG-AZ61A EXTRUSION F 0.250-2.499 S | 70 | 6.3 | 6.3 | 45 | 55 | 28 | 32 | 14 | 19 | 40 | 24 | 2.4 | S | F | 0.0647 | 9 | Extruded bar, rod, and solid shapes | 0.31 | AMS 4350 | 0.250-2.499 |
| MG-AZ61A EXTRUSION F 2.500-4.499 S | 70 | 6.3 | 6.3 | — | — | — | — | 14 | — | 40 | 22 | 2.4 | S | F | 0.0647 | 7 | Extruded bar, rod, and solid shapes | 0.31 | AMS 4350 | 2.500-4.499a |
| MG-AZ61A EXTRUSION F LE0.249 S | 70 | 6.3 | 6.3 | 45 | 55 | 28 | 32 | 14 | 19 | 38 | 21 | 2.4 | S | F | 0.0647 | 8 | Extruded bar, rod, and solid shapes | 0.31 | AMS 4350 | <=0.249 |
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