N06230 Nickel vs. EN 2.4878 Nickel
Both N06230 nickel and EN 2.4878 nickel are nickel alloys. They have 75% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is N06230 nickel and the bottom bar is EN 2.4878 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 200 |
| Elongation at Break, % | 38 to 48 | |
| 13 to 17 |
| Fatigue Strength, MPa | 250 to 360 | |
| 400 to 410 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 83 | |
| 78 |
| Shear Strength, MPa | 420 to 600 | |
| 750 to 760 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 1210 to 1250 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 740 to 780 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 330 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 1030 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1370 |
| Melting Onset (Solidus), °C | 1300 | |
| 1320 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 460 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 11 |
| Thermal Expansion, µm/m-K | 13 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 80 |
| Density, g/cm3 | 9.5 | |
| 8.3 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 10 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 290 | |
| 370 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 150 to 180 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 1370 to 1540 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 21 | |
| 24 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 41 to 42 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 31 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 2.8 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 37 to 39 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 1.2 to 1.6 |
| Boron (B), % | 0 to 0.015 | |
| 0.010 to 0.015 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0.030 to 0.070 |
| Chromium (Cr), % | 20 to 24 | |
| 23 to 25 |
| Cobalt (Co), % | 0 to 5.0 | |
| 19 to 21 |
| Copper (Cu), % | 0 | |
| 0 to 0.2 |
| Iron (Fe), % | 0 to 3.0 | |
| 0 to 1.0 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 1.0 to 2.0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 43.6 to 52.2 |
| Niobium (Nb), % | 0 | |
| 0.7 to 1.2 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.010 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.0070 |
| Tantalum (Ta), % | 0 | |
| 0 to 0.050 |
| Titanium (Ti), % | 0 | |
| 2.8 to 3.2 |
| Tungsten (W), % | 13 to 15 | |
| 0 |
| Zirconium (Zr), % | 0 | |
| 0.030 to 0.070 |