EN 2.4878 Nickel vs. EN AC-21200 Aluminum
EN 2.4878 nickel belongs to the nickel alloys classification, while EN AC-21200 aluminum belongs to the aluminum alloys. There are 27 material properties with values for both materials. Properties with values for just one material (4, 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 2.4878 nickel and the bottom bar is EN AC-21200 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 71 |
| Elongation at Break, % | 13 to 17 | |
| 3.9 to 6.2 |
| Fatigue Strength, MPa | 400 to 410 | |
| 110 to 130 |
| Poisson's Ratio | 0.29 | |
| 0.33 |
| Shear Modulus, GPa | 78 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 1210 to 1250 | |
| 410 to 440 |
| Tensile Strength: Yield (Proof), MPa | 740 to 780 | |
| 270 to 360 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 390 |
| Maximum Temperature: Mechanical, °C | 1030 | |
| 170 |
| Melting Completion (Liquidus), °C | 1370 | |
| 660 |
| Melting Onset (Solidus), °C | 1320 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 460 | |
| 880 |
| Thermal Conductivity, W/m-K | 11 | |
| 130 |
| Thermal Expansion, µm/m-K | 12 | |
| 23 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 10 |
| Density, g/cm3 | 8.3 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 10 | |
| 8.0 |
| Embodied Energy, MJ/kg | 150 | |
| 150 |
| Embodied Water, L/kg | 370 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 180 | |
| 16 to 22 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1370 to 1540 | |
| 500 to 930 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 24 | |
| 46 |
| Strength to Weight: Axial, points | 41 to 42 | |
| 38 to 40 |
| Strength to Weight: Bending, points | 31 | |
| 41 to 43 |
| Thermal Diffusivity, mm2/s | 2.8 | |
| 49 |
| Thermal Shock Resistance, points | 37 to 39 | |
| 18 to 19 |
Alloy Composition
| Aluminum (Al), % | 1.2 to 1.6 | |
| 93.3 to 95.7 |
| Boron (B), % | 0.010 to 0.015 | |
| 0 |
| Carbon (C), % | 0.030 to 0.070 | |
| 0 |
| Chromium (Cr), % | 23 to 25 | |
| 0 |
| Cobalt (Co), % | 19 to 21 | |
| 0 |
| Copper (Cu), % | 0 to 0.2 | |
| 4.0 to 5.0 |
| Iron (Fe), % | 0 to 1.0 | |
| 0 to 0.2 |
| Lead (Pb), % | 0 | |
| 0 to 0.030 |
| Magnesium (Mg), % | 0 | |
| 0.15 to 0.5 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0.2 to 0.5 |
| Molybdenum (Mo), % | 1.0 to 2.0 | |
| 0 |
| Nickel (Ni), % | 43.6 to 52.2 | |
| 0 to 0.050 |
| Niobium (Nb), % | 0.7 to 1.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.010 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.1 |
| Sulfur (S), % | 0 to 0.0070 | |
| 0 |
| Tantalum (Ta), % | 0 to 0.050 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0 to 0.030 |
| Titanium (Ti), % | 2.8 to 3.2 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 0 to 0.1 |
| Zirconium (Zr), % | 0.030 to 0.070 | |
| 0 |
| Residuals, % | 0 | |
| 0 to 0.1 |