N06230 Nickel vs. EN 1.4962 Stainless Steel
N06230 nickel belongs to the nickel alloys classification, while EN 1.4962 stainless steel belongs to the iron alloys. They have a modest 35% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is N06230 nickel and the bottom bar is EN 1.4962 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 200 |
| Elongation at Break, % | 38 to 48 | |
| 22 to 34 |
| Fatigue Strength, MPa | 250 to 360 | |
| 210 to 330 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 83 | |
| 77 |
| Shear Strength, MPa | 420 to 600 | |
| 420 to 440 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 630 to 690 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 260 to 490 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 910 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1480 |
| Melting Onset (Solidus), °C | 1300 | |
| 1440 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 470 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 14 |
| Thermal Expansion, µm/m-K | 13 | |
| 16 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.3 | |
| 2.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 23 |
| Density, g/cm3 | 9.5 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 4.1 |
| Embodied Energy, MJ/kg | 160 | |
| 59 |
| Embodied Water, L/kg | 290 | |
| 150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 140 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 170 to 610 |
| Stiffness to Weight: Axial, points | 12 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 24 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 21 to 24 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 20 to 21 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 3.7 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 14 to 16 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 0 |
| Boron (B), % | 0 to 0.015 | |
| 0.0015 to 0.0060 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0.070 to 0.15 |
| Chromium (Cr), % | 20 to 24 | |
| 15.5 to 17.5 |
| Cobalt (Co), % | 0 to 5.0 | |
| 0 |
| Iron (Fe), % | 0 to 3.0 | |
| 62.1 to 69 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 12.5 to 14.5 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.035 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 | |
| 0.4 to 0.7 |
| Tungsten (W), % | 13 to 15 | |
| 2.5 to 3.0 |