N12160 Nickel vs. EN 1.4310 Stainless Steel
N12160 nickel belongs to the nickel alloys classification, while EN 1.4310 stainless steel belongs to the iron 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 (5, in this case) are not shown.
For each property being compared, the top bar is N12160 nickel and the bottom bar is EN 1.4310 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 200 |
| Elongation at Break, % | 45 | |
| 14 to 45 |
| Fatigue Strength, MPa | 230 | |
| 240 to 330 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 80 | |
| 77 |
| Shear Strength, MPa | 500 | |
| 510 to 550 |
| Tensile Strength: Ultimate (UTS), MPa | 710 | |
| 730 to 900 |
| Tensile Strength: Yield (Proof), MPa | 270 | |
| 260 to 570 |
Thermal Properties
| Latent Heat of Fusion, J/g | 360 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 1060 | |
| 910 |
| Melting Completion (Liquidus), °C | 1330 | |
| 1420 |
| Melting Onset (Solidus), °C | 1280 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 11 | |
| 15 |
| Thermal Expansion, µm/m-K | 13 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 90 | |
| 14 |
| Density, g/cm3 | 8.2 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 8.5 | |
| 2.9 |
| Embodied Energy, MJ/kg | 120 | |
| 42 |
| Embodied Water, L/kg | 400 | |
| 140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 260 | |
| 110 to 260 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 180 | |
| 170 to 830 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 | |
| 26 to 32 |
| Strength to Weight: Bending, points | 22 | |
| 23 to 27 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 4.0 |
| Thermal Shock Resistance, points | 19 | |
| 15 to 18 |
Alloy Composition
| Carbon (C), % | 0 to 0.15 | |
| 0.050 to 0.15 |
| Chromium (Cr), % | 26 to 30 | |
| 16 to 19 |
| Cobalt (Co), % | 27 to 33 | |
| 0 |
| Iron (Fe), % | 0 to 3.5 | |
| 66.4 to 78 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 2.0 |
| Molybdenum (Mo), % | 0 to 1.0 | |
| 0 to 0.8 |
| Nickel (Ni), % | 25 to 44.4 | |
| 6.0 to 9.5 |
| Niobium (Nb), % | 0 to 1.0 | |
| 0 |
| Nitrogen (N), % | 0 | |
| 0 to 0.1 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.045 |
| Silicon (Si), % | 2.4 to 3.0 | |
| 0 to 2.0 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0.2 to 0.8 | |
| 0 |
| Tungsten (W), % | 0 to 1.0 | |
| 0 |