EN 1.4567 Stainless Steel vs. N06058 Nickel
EN 1.4567 stainless steel belongs to the iron alloys classification, while N06058 nickel belongs to the nickel alloys. They have a modest 29% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is EN 1.4567 stainless steel and the bottom bar is N06058 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 220 |
| Elongation at Break, % | 22 to 51 | |
| 45 |
| Fatigue Strength, MPa | 190 to 260 | |
| 350 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 76 | |
| 86 |
| Shear Strength, MPa | 390 to 490 | |
| 600 |
| Tensile Strength: Ultimate (UTS), MPa | 550 to 780 | |
| 860 |
| Tensile Strength: Yield (Proof), MPa | 200 to 390 | |
| 410 |
Thermal Properties
| Latent Heat of Fusion, J/g | 290 | |
| 330 |
| Maximum Temperature: Mechanical, °C | 930 | |
| 980 |
| Melting Completion (Liquidus), °C | 1410 | |
| 1540 |
| Melting Onset (Solidus), °C | 1370 | |
| 1490 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 420 |
| Thermal Conductivity, W/m-K | 11 | |
| 9.8 |
| Thermal Expansion, µm/m-K | 17 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 16 | |
| 70 |
| Density, g/cm3 | 7.8 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 3.1 | |
| 13 |
| Embodied Energy, MJ/kg | 43 | |
| 170 |
| Embodied Water, L/kg | 150 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 220 | |
| 320 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 100 to 400 | |
| 370 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 23 |
| Strength to Weight: Axial, points | 19 to 27 | |
| 27 |
| Strength to Weight: Bending, points | 19 to 24 | |
| 23 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 2.6 |
| Thermal Shock Resistance, points | 12 to 17 | |
| 23 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.4 |
| Carbon (C), % | 0 to 0.040 | |
| 0 to 0.010 |
| Chromium (Cr), % | 17 to 19 | |
| 20 to 23 |
| Cobalt (Co), % | 0 | |
| 0 to 0.3 |
| Copper (Cu), % | 3.0 to 4.0 | |
| 0 to 0.5 |
| Iron (Fe), % | 63.3 to 71.5 | |
| 0 to 1.5 |
| Manganese (Mn), % | 0 to 2.0 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0 | |
| 19 to 21 |
| Nickel (Ni), % | 8.5 to 10.5 | |
| 52.2 to 61 |
| Nitrogen (N), % | 0 to 0.1 | |
| 0.020 to 0.15 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 to 0.015 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.010 |
| Tungsten (W), % | 0 | |
| 0 to 0.3 |