N08120 Nickel vs. AISI 316L Stainless Steel
N08120 nickel belongs to the nickel alloys classification, while AISI 316L stainless steel belongs to the iron alloys. They have 63% of their average alloy composition in common. There are 29 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 N08120 nickel and the bottom bar is AISI 316L stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 34 | |
| 9.0 to 50 |
| Fatigue Strength, MPa | 230 | |
| 170 to 450 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 79 | |
| 78 |
| Shear Strength, MPa | 470 | |
| 370 to 690 |
| Tensile Strength: Ultimate (UTS), MPa | 700 | |
| 530 to 1160 |
| Tensile Strength: Yield (Proof), MPa | 310 | |
| 190 to 870 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 870 |
| Melting Completion (Liquidus), °C | 1420 | |
| 1400 |
| Melting Onset (Solidus), °C | 1370 | |
| 1380 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Conductivity, W/m-K | 11 | |
| 15 |
| Thermal Expansion, µm/m-K | 14 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 45 | |
| 19 |
| Density, g/cm3 | 8.2 | |
| 7.9 |
| Embodied Carbon, kg CO2/kg material | 7.2 | |
| 3.9 |
| Embodied Energy, MJ/kg | 100 | |
| 53 |
| Embodied Water, L/kg | 240 | |
| 150 |
Common Calculations
| PREN (Pitting Resistance) | 35 | |
| 26 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 190 | |
| 77 to 230 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 240 | |
| 93 to 1880 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 25 |
| Strength to Weight: Axial, points | 24 | |
| 19 to 41 |
| Strength to Weight: Bending, points | 21 | |
| 18 to 31 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 4.1 |
| Thermal Shock Resistance, points | 17 | |
| 12 to 25 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.4 | |
| 0 |
| Boron (B), % | 0 to 0.010 | |
| 0 |
| Carbon (C), % | 0.020 to 0.1 | |
| 0 to 0.030 |
| 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 | |
| 62 to 72 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 2.0 |
| Molybdenum (Mo), % | 0 to 2.5 | |
| 2.0 to 3.0 |
| Nickel (Ni), % | 35 to 39 | |
| 10 to 14 |
| Niobium (Nb), % | 0.4 to 0.9 | |
| 0 |
| Nitrogen (N), % | 0.15 to 0.3 | |
| 0 to 0.1 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.045 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Tungsten (W), % | 0 to 2.5 | |
| 0 |