N06230 Nickel vs. 712.0 Aluminum
N06230 nickel belongs to the nickel alloys classification, while 712.0 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is N06230 nickel and the bottom bar is 712.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 70 |
| Elongation at Break, % | 38 to 48 | |
| 4.5 to 4.7 |
| Fatigue Strength, MPa | 250 to 360 | |
| 140 to 180 |
| Poisson's Ratio | 0.28 | |
| 0.32 |
| Shear Modulus, GPa | 83 | |
| 27 |
| Shear Strength, MPa | 420 to 600 | |
| 180 |
| Tensile Strength: Ultimate (UTS), MPa | 620 to 840 | |
| 250 to 260 |
| Tensile Strength: Yield (Proof), MPa | 330 to 400 | |
| 180 to 200 |
Thermal Properties
| Latent Heat of Fusion, J/g | 310 | |
| 380 |
| Maximum Temperature: Mechanical, °C | 990 | |
| 190 |
| Melting Completion (Liquidus), °C | 1370 | |
| 640 |
| Melting Onset (Solidus), °C | 1300 | |
| 610 |
| Specific Heat Capacity, J/kg-K | 420 | |
| 870 |
| Thermal Conductivity, W/m-K | 8.9 | |
| 160 |
| Thermal Expansion, µm/m-K | 13 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.4 | |
| 40 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.3 | |
| 120 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 85 | |
| 9.5 |
| Density, g/cm3 | 9.5 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 11 | |
| 8.0 |
| Embodied Energy, MJ/kg | 160 | |
| 150 |
| Embodied Water, L/kg | 290 | |
| 1140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 to 330 | |
| 11 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 380 | |
| 240 to 270 |
| Stiffness to Weight: Axial, points | 12 | |
| 13 |
| Stiffness to Weight: Bending, points | 21 | |
| 46 |
| Strength to Weight: Axial, points | 18 to 25 | |
| 24 to 25 |
| Strength to Weight: Bending, points | 17 to 21 | |
| 30 to 31 |
| Thermal Diffusivity, mm2/s | 2.3 | |
| 62 |
| Thermal Shock Resistance, points | 17 to 23 | |
| 11 |
Alloy Composition
| Aluminum (Al), % | 0.2 to 0.5 | |
| 90.7 to 94 |
| Boron (B), % | 0 to 0.015 | |
| 0 |
| Carbon (C), % | 0.050 to 0.15 | |
| 0 |
| Chromium (Cr), % | 20 to 24 | |
| 0.4 to 0.6 |
| Cobalt (Co), % | 0 to 5.0 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0 to 0.25 |
| Iron (Fe), % | 0 to 3.0 | |
| 0 to 0.5 |
| Lanthanum (La), % | 0.0050 to 0.050 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.5 to 0.65 |
| Manganese (Mn), % | 0.3 to 1.0 | |
| 0 to 0.1 |
| Molybdenum (Mo), % | 1.0 to 3.0 | |
| 0 |
| Nickel (Ni), % | 47.5 to 65.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0.25 to 0.75 | |
| 0 to 0.3 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0.15 to 0.25 |
| Tungsten (W), % | 13 to 15 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 5.0 to 6.5 |
| Residuals, % | 0 | |
| 0 to 0.2 |