Material Specifications
2.4375 is a nickel-cobalt-based superalloy combining high strength at elevated temperatures with outstanding corrosion resistance. Used in demanding aerospace, marine, and industrial applications worldwide.
| Element | Composition % | Property | Value |
|---|---|---|---|
| Cobalt (Co) | 15.7 - 17.1 | Density | 8.74 g/cm³ |
| Chromium (Cr) | 4.3 - 5.2 | Melting Point | 1350°C |
| Aluminum (Al) | 5.8 - 6.7 | Yield Strength (RT) | 950 - 1200 MPa |
| Titanium (Ti) | 0.8 - 1.2 | Tensile Strength (RT) | 1200 - 1500 MPa |
| Molybdenum (Mo) | 3.0 - 3.7 | Service Temperature | -100°C to +700°C |