EN 1.4020 Stainless Steel vs. N06230 Nickel
EN 1.4020 stainless steel belongs to the iron alloys classification, while N06230 nickel belongs to the nickel alloys. They have a modest 22% of their average alloy composition in common, which, by itself, doesn't mean much. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is EN 1.4020 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, % | 13 to 34 | |
| 38 to 48 |
| Fatigue Strength, MPa | 340 to 540 | |
| 250 to 360 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 77 | |
| 83 |
| Shear Strength, MPa | 510 to 680 | |
| 420 to 600 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 1130 | |
| 620 to 840 |
| Tensile Strength: Yield (Proof), MPa | 430 to 950 | |
| 330 to 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 310 |
| Maximum Temperature: Mechanical, °C | 890 | |
| 990 |
| Melting Completion (Liquidus), °C | 1390 | |
| 1370 |
| Melting Onset (Solidus), °C | 1350 | |
| 1300 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 420 |
| Thermal Expansion, µm/m-K | 17 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 85 |
| Density, g/cm3 | 7.6 | |
| 9.5 |
| Embodied Carbon, kg CO2/kg material | 2.5 | |
| 11 |
| Embodied Energy, MJ/kg | 37 | |
| 160 |
| Embodied Water, L/kg | 150 | |
| 290 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 220 | |
| 200 to 330 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 2290 | |
| 250 to 380 |
| Stiffness to Weight: Axial, points | 14 | |
| 12 |
| Stiffness to Weight: Bending, points | 25 | |
| 21 |
| Strength to Weight: Axial, points | 28 to 41 | |
| 18 to 25 |
| Strength to Weight: Bending, points | 25 to 32 | |
| 17 to 21 |
| Thermal Shock Resistance, points | 16 to 23 | |
| 17 to 23 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0.2 to 0.5 |
| Boron (B), % | 0 | |
| 0 to 0.015 |
| Carbon (C), % | 0 to 0.15 | |
| 0.050 to 0.15 |
| Chromium (Cr), % | 16.5 to 19 | |
| 20 to 24 |
| Cobalt (Co), % | 0 | |
| 0 to 5.0 |
| Iron (Fe), % | 62.8 to 71.8 | |
| 0 to 3.0 |
| Lanthanum (La), % | 0 | |
| 0.0050 to 0.050 |
| Manganese (Mn), % | 11 to 14 | |
| 0.3 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 1.0 to 3.0 |
| Nickel (Ni), % | 0.5 to 2.5 | |
| 47.5 to 65.2 |
| Nitrogen (N), % | 0.2 to 0.45 | |
| 0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 to 0.030 |
| Silicon (Si), % | 0 to 1.0 | |
| 0.25 to 0.75 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |
| Tungsten (W), % | 0 | |
| 13 to 15 |