EN 1.4962 Stainless Steel vs. N06230 Nickel
EN 1.4962 stainless steel belongs to the iron alloys classification, while N06230 nickel belongs to the nickel 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 EN 1.4962 stainless steel and the bottom bar is N06230 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 210 |
| Elongation at Break, % | 22 to 34 | |
| 38 to 48 |
| Fatigue Strength, MPa | 210 to 330 | |
| 250 to 360 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 83 |
| Shear Strength, MPa | 420 to 440 | |
| 420 to 600 |
| Tensile Strength: Ultimate (UTS), MPa | 630 to 690 | |
| 620 to 840 |
| Tensile Strength: Yield (Proof), MPa | 260 to 490 | |
| 330 to 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 310 |
| Maximum Temperature: Mechanical, °C | 910 | |
| 990 |
| Melting Completion (Liquidus), °C | 1480 | |
| 1370 |
| Melting Onset (Solidus), °C | 1440 | |
| 1300 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 420 |
| Thermal Conductivity, W/m-K | 14 | |
| 8.9 |
| Thermal Expansion, µm/m-K | 16 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 1.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 1.3 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 23 | |
| 85 |
| Density, g/cm3 | 8.1 | |
| 9.5 |
| Embodied Carbon, kg CO2/kg material | 4.1 | |
| 11 |
| Embodied Energy, MJ/kg | 59 | |
| 160 |
| Embodied Water, L/kg | 150 | |
| 290 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 170 | |
| 200 to 330 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 to 610 | |
| 250 to 380 |
| Stiffness to Weight: Axial, points | 14 | |
| 12 |
| Stiffness to Weight: Bending, points | 24 | |
| 21 |
| Strength to Weight: Axial, points | 21 to 24 | |
| 18 to 25 |
| Strength to Weight: Bending, points | 20 to 21 | |
| 17 to 21 |
| Thermal Diffusivity, mm2/s | 3.7 | |
| 2.3 |
| Thermal Shock Resistance, points | 14 to 16 | |
| 17 to 23 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.2 to 0.5 |
| Boron (B), % | 0.0015 to 0.0060 | |
| 0 to 0.015 |
| Carbon (C), % | 0.070 to 0.15 | |
| 0.050 to 0.15 |
| Chromium (Cr), % | 15.5 to 17.5 | |
| 20 to 24 |
| Cobalt (Co), % | 0 | |
| 0 to 5.0 |
| Iron (Fe), % | 62.1 to 69 | |
| 0 to 3.0 |
| Lanthanum (La), % | 0 | |
| 0.0050 to 0.050 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0.3 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 1.0 to 3.0 |
| Nickel (Ni), % | 12.5 to 14.5 | |
| 47.5 to 65.2 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 0.5 | |
| 0.25 to 0.75 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0.4 to 0.7 | |
| 0 |
| Tungsten (W), % | 2.5 to 3.0 | |
| 13 to 15 |