Aerospace Materials: MG-ZK60A EXTRUSION T5 5.000-9.999 ALL
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) | Fcy 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-ZK60A EXTRUSION T5 5.000-9.999 ALL S | 70 | 6.5 | 6.5 | 23 | 45 | 34 | 2.4 | S | T5 | 0.0659 | 6 | Extruded rod, bar, and solid shapes | 0.35 | AMS 4352 | 5.000-9.999; All |
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