N08120 Nickel vs. EN 1.4568 Stainless Steel
N08120 nickel belongs to the nickel alloys classification, while EN 1.4568 stainless steel belongs to the iron alloys. They have 56% of their average alloy composition in common. There are 29 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 N08120 nickel and the bottom bar is EN 1.4568 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 34 | |
| 2.3 to 21 |
| Fatigue Strength, MPa | 230 | |
| 220 to 670 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 76 |
| Shear Strength, MPa | 470 | |
| 520 to 930 |
| Tensile Strength: Ultimate (UTS), MPa | 700 | |
| 830 to 1620 |
| Tensile Strength: Yield (Proof), MPa | 310 | |
| 330 to 1490 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 890 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1420 |
| Melting Onset (Solidus), °C | 1370 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 11 | |
| 16 |
| Thermal Expansion, µm/m-K | 14 | |
| 13 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 45 | |
| 13 |
| Density, g/cm3 | 8.2 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 7.2 | |
| 2.8 |
| Embodied Energy, MJ/kg | 100 | |
| 40 |
| Embodied Water, L/kg | 240 | |
| 140 |
Common Calculations
| PREN (Pitting Resistance) | 35 | |
| 17 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 | |
| 36 to 140 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 | |
| 290 to 5710 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 | |
| 30 to 58 |
| Strength to Weight: Bending, points | 21 | |
| 25 to 40 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 4.3 |
| Thermal Shock Resistance, points | 17 | |
| 23 to 46 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.4 | |
| 0.7 to 1.5 |
| Boron (B), % | 0 to 0.010 | |
| 0 |
| Carbon (C), % | 0.020 to 0.1 | |
| 0 to 0.090 |
| Chromium (Cr), % | 23 to 27 | |
| 16 to 18 |
| Cobalt (Co), % | 0 to 3.0 | |
| 0 |
| Copper (Cu), % | 0 to 0.5 | |
| 0 |
| Iron (Fe), % | 21 to 41.4 | |
| 70.9 to 76.8 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 to 2.5 | |
| 0 |
| Nickel (Ni), % | 35 to 39 | |
| 6.5 to 7.8 |
| Niobium (Nb), % | 0.4 to 0.9 | |
| 0 |
| Nitrogen (N), % | 0.15 to 0.3 | |
| 0 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.7 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Tungsten (W), % | 0 to 2.5 | |
| 0 |