N08120 Nickel vs. S35000 Stainless Steel
N08120 nickel belongs to the nickel alloys classification, while S35000 stainless steel belongs to the iron alloys. They have 55% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is N08120 nickel and the bottom bar is S35000 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 34 | |
| 2.3 to 14 |
| Fatigue Strength, MPa | 230 | |
| 380 to 520 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 78 |
| Shear Strength, MPa | 470 | |
| 740 to 950 |
| Tensile Strength: Ultimate (UTS), MPa | 700 | |
| 1300 to 1570 |
| Tensile Strength: Yield (Proof), MPa | 310 | |
| 660 to 1160 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 900 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1460 |
| Melting Onset (Solidus), °C | 1370 | |
| 1410 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Conductivity, W/m-K | 11 | |
| 16 |
| Thermal Expansion, µm/m-K | 14 | |
| 11 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 45 | |
| 14 |
| Density, g/cm3 | 8.2 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 7.2 | |
| 3.2 |
| Embodied Energy, MJ/kg | 100 | |
| 44 |
| Embodied Water, L/kg | 240 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 35 | |
| 28 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 | |
| 28 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 | |
| 1070 to 3360 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 | |
| 46 to 56 |
| Strength to Weight: Bending, points | 21 | |
| 34 to 38 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 4.4 |
| Thermal Shock Resistance, points | 17 | |
| 42 to 51 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.4 | |
| 0 |
| Boron (B), % | 0 to 0.010 | |
| 0 |
| Carbon (C), % | 0.020 to 0.1 | |
| 0.070 to 0.11 |
| Chromium (Cr), % | 23 to 27 | |
| 16 to 17 |
| Cobalt (Co), % | 0 to 3.0 | |
| 0 |
| Copper (Cu), % | 0 to 0.5 | |
| 0 |
| Iron (Fe), % | 21 to 41.4 | |
| 72.7 to 76.9 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0.5 to 1.3 |
| Molybdenum (Mo), % | 0 to 2.5 | |
| 2.5 to 3.2 |
| Nickel (Ni), % | 35 to 39 | |
| 4.0 to 5.0 |
| Niobium (Nb), % | 0.4 to 0.9 | |
| 0 |
| Nitrogen (N), % | 0.15 to 0.3 | |
| 0.070 to 0.13 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Tungsten (W), % | 0 to 2.5 | |
| 0 |