EN 2.4650 Nickel vs. 201.0 Aluminum
EN 2.4650 nickel belongs to the nickel alloys classification, while 201.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 EN 2.4650 nickel and the bottom bar is 201.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 71 |
| Elongation at Break, % | 34 | |
| 4.4 to 20 |
| Fatigue Strength, MPa | 480 | |
| 120 to 150 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 80 | |
| 27 |
| Shear Strength, MPa | 730 | |
| 290 |
| Tensile Strength: Ultimate (UTS), MPa | 1090 | |
| 370 to 470 |
| Tensile Strength: Yield (Proof), MPa | 650 | |
| 220 to 400 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 1010 | |
| 170 |
| Melting Completion (Liquidus), °C | 1400 | |
| 650 |
| Melting Onset (Solidus), °C | 1350 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 870 |
| Thermal Conductivity, W/m-K | 12 | |
| 120 |
| Thermal Expansion, µm/m-K | 11 | |
| 19 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.5 | |
| 30 to 33 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.6 | |
| 87 to 97 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 38 |
| Density, g/cm3 | 8.5 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 8.7 |
| Embodied Energy, MJ/kg | 140 | |
| 160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 320 | |
| 19 to 63 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1030 | |
| 330 to 1160 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 23 | |
| 45 |
| Strength to Weight: Axial, points | 36 | |
| 33 to 42 |
| Strength to Weight: Bending, points | 28 | |
| 37 to 44 |
| Thermal Diffusivity, mm2/s | 3.1 | |
| 45 |
| Thermal Shock Resistance, points | 33 | |
| 19 to 25 |
Alloy Composition
| Aluminum (Al), % | 0.3 to 0.6 | |
| 92.1 to 95.1 |
| Boron (B), % | 0 to 0.0050 | |
| 0 |
| Carbon (C), % | 0.040 to 0.080 | |
| 0 |
| Chromium (Cr), % | 19 to 21 | |
| 0 |
| Cobalt (Co), % | 19 to 21 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 4.0 to 5.2 |
| Iron (Fe), % | 0 to 0.7 | |
| 0 to 0.15 |
| Magnesium (Mg), % | 0 | |
| 0.15 to 0.55 |
| Manganese (Mn), % | 0 to 0.6 | |
| 0.2 to 0.5 |
| Molybdenum (Mo), % | 5.6 to 6.1 | |
| 0 |
| Nickel (Ni), % | 46.9 to 54.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 0.4 | |
| 0 to 0.1 |
| Silver (Ag), % | 0 | |
| 0.4 to 1.0 |
| Sulfur (S), % | 0 to 0.0070 | |
| 0 |
| Titanium (Ti), % | 1.9 to 2.4 | |
| 0.15 to 0.35 |
| Residuals, % | 0 | |
| 0 to 0.1 |