N06230 Nickel vs. AISI 321 Stainless Steel
N06230 nickel belongs to the nickel alloys classification, while AISI 321 stainless steel belongs to the iron alloys. They have a modest 31% 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 (3, in this case) are not shown.
For each property being compared, the top bar is N06230 nickel and the bottom bar is AISI 321 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 200 |
| Elongation at Break, % | 38 to 48 | |
| 34 to 50 |
| Fatigue Strength, MPa | 250 to 360 | |
| 220 to 270 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Shear Modulus, GPa | 83 | |
| 77 |
| Shear Strength, MPa | 420 to 600 | |
| 420 to 460 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 590 to 690 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 220 to 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 870 |
| Melting Completion (Liquidus), °C | 1370 | |
| 1430 |
| Melting Onset (Solidus), °C | 1300 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 480 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 16 |
| Thermal Expansion, µm/m-K | 13 | |
| 17 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 2.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.3 | |
| 2.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 16 |
| Density, g/cm3 | 9.5 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 3.2 |
| Embodied Energy, MJ/kg | 160 | |
| 45 |
| Embodied Water, L/kg | 290 | |
| 140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 190 to 230 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 130 to 310 |
| Stiffness to Weight: Axial, points | 12 | |
| 14 |
| Stiffness to Weight: Bending, points | 21 | |
| 25 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 21 to 25 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 20 to 22 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 4.1 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 13 to 15 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 0 |
| Boron (B), % | 0 to 0.015 | |
| 0 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0 to 0.080 |
| Chromium (Cr), % | 20 to 24 | |
| 17 to 19 |
| Cobalt (Co), % | 0 to 5.0 | |
| 0 |
| Iron (Fe), % | 0 to 3.0 | |
| 65.3 to 74 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 to 2.0 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 9.0 to 12 |
| Nitrogen (N), % | 0 | |
| 0 to 0.1 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.045 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0 to 0.75 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 | |
| 0 to 0.7 |
| Tungsten (W), % | 13 to 15 | |
| 0 |