N06230 Nickel vs. S13800 Stainless Steel
N06230 nickel belongs to the nickel alloys classification, while S13800 stainless steel belongs to the iron alloys. They have a modest 25% of their average alloy composition in common, which, by itself, doesn't mean much. There are 30 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 N06230 nickel and the bottom bar is S13800 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 200 |
| Elongation at Break, % | 38 to 48 | |
| 11 to 18 |
| Fatigue Strength, MPa | 250 to 360 | |
| 410 to 870 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 83 | |
| 77 |
| Shear Strength, MPa | 420 to 600 | |
| 610 to 1030 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 980 to 1730 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 660 to 1580 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 810 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1450 |
| Melting Onset (Solidus), °C | 1300 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 470 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 16 |
| Thermal Expansion, µm/m-K | 13 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.3 | |
| 2.6 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 15 |
| Density, g/cm3 | 9.5 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 3.4 |
| Embodied Energy, MJ/kg | 160 | |
| 46 |
| Embodied Water, L/kg | 290 | |
| 140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 150 to 190 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 1090 to 5490 |
| Stiffness to Weight: Axial, points | 12 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 25 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 35 to 61 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 28 to 41 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 4.3 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 33 to 58 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 0.9 to 1.4 |
| Boron (B), % | 0 to 0.015 | |
| 0 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0 to 0.050 |
| Chromium (Cr), % | 20 to 24 | |
| 12.3 to 13.2 |
| Cobalt (Co), % | 0 to 5.0 | |
| 0 |
| Iron (Fe), % | 0 to 3.0 | |
| 73.6 to 77.3 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 to 0.2 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 2.0 to 3.0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 7.5 to 8.5 |
| Nitrogen (N), % | 0 | |
| 0 to 0.010 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.010 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.0080 |
| Tungsten (W), % | 13 to 15 | |
| 0 |