| Property | Value |
|---|---|
| Mechanical Properties | |
| Ultimate tensile strength | 470 – 530 MPa |
| Yield strength | 390 – 460 MPa |
| Young’s modulus (modulus of elasticity) | 70 – 80 GPa |
| Elongation at break | 5 – 12 % |
| Physical Properties | |
| Corrosion resistance | Good |
| Magnetism | Non-magnetic |
| Weldability | Poor |
| Thermal Properties | |
| Thermal expansion coefficient | 23 – 25.4 × 10-6/ºC |
| Thermal conductivity | 153 W/(m⋅°C) |
| Electrical Properties | |
| Electrical resistivity | 4.4 μΩ*cm |
| Post Treatments | |
| Post-Processing | Cold working, Aging, Hardening |
| Anodizing compatibility | Not recommended – due to the high amount of zinc that the material contains, dark spots or corroded marks may be observed |
| Common Applications | |
| Fuselage frames | Bulkheads |
| Wing skins | Aerospace structures |
| Commercial & military aircraft applications | |
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