EN 2.4952 Nickel vs. EN 1.4418 Stainless Steel
EN 2.4952 nickel belongs to the nickel alloys classification, while EN 1.4418 stainless steel belongs to the iron alloys. They have a modest 23% of their average alloy composition in common, which, by itself, doesn't mean much. There are 31 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 2.4952 nickel and the bottom bar is EN 1.4418 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Elongation at Break, % | 17 | |
| 16 to 20 |
| Fatigue Strength, MPa | 370 | |
| 350 to 480 |
| Impact Strength: V-Notched Charpy, J | 22 | |
| 62 to 90 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 74 | |
| 77 |
| Shear Strength, MPa | 700 | |
| 530 to 620 |
| Tensile Strength: Ultimate (UTS), MPa | 1150 | |
| 860 to 1000 |
| Tensile Strength: Yield (Proof), MPa | 670 | |
| 540 to 790 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 980 | |
| 870 |
| Melting Completion (Liquidus), °C | 1350 | |
| 1450 |
| Melting Onset (Solidus), °C | 1300 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 12 | |
| 15 |
| Thermal Expansion, µm/m-K | 13 | |
| 10 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 2.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.5 | |
| 2.5 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 55 | |
| 13 |
| Density, g/cm3 | 8.3 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 9.8 | |
| 2.8 |
| Embodied Energy, MJ/kg | 140 | |
| 39 |
| Embodied Water, L/kg | 290 | |
| 130 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 170 | |
| 130 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1180 | |
| 730 to 1590 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 25 |
| Strength to Weight: Axial, points | 38 | |
| 31 to 36 |
| Strength to Weight: Bending, points | 29 | |
| 26 to 28 |
| Thermal Diffusivity, mm2/s | 3.1 | |
| 4.0 |
| Thermal Shock Resistance, points | 33 | |
| 31 to 36 |
Alloy Composition
| Aluminum (Al), % | 1.0 to 1.8 | |
| 0 |
| Boron (B), % | 0 to 0.0080 | |
| 0 |
| Carbon (C), % | 0.040 to 0.1 | |
| 0 to 0.060 |
| Chromium (Cr), % | 18 to 21 | |
| 15 to 17 |
| Cobalt (Co), % | 0 to 1.0 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 0 |
| Iron (Fe), % | 0 to 1.5 | |
| 73.2 to 80.2 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.5 |
| Molybdenum (Mo), % | 0 | |
| 0.8 to 1.5 |
| Nickel (Ni), % | 65 to 79.2 | |
| 4.0 to 6.0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.020 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Titanium (Ti), % | 1.8 to 2.7 | |
| 0 |