EN 2.4856 Nickel vs. 7049 Aluminum
EN 2.4856 nickel belongs to the nickel alloys classification, while 7049 aluminum belongs to the aluminum alloys. 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 2.4856 nickel and the bottom bar is 7049 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 210 | |
| 140 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 70 |
| Elongation at Break, % | 28 | |
| 6.2 to 7.0 |
| Fatigue Strength, MPa | 280 | |
| 160 to 170 |
| Poisson's Ratio | 0.29 | |
| 0.32 |
| Shear Modulus, GPa | 79 | |
| 27 |
| Shear Strength, MPa | 570 | |
| 300 to 310 |
| Tensile Strength: Ultimate (UTS), MPa | 880 | |
| 510 to 530 |
| Tensile Strength: Yield (Proof), MPa | 430 | |
| 420 to 450 |
Thermal Properties
| Latent Heat of Fusion, J/g | 330 | |
| 370 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 180 |
| Melting Completion (Liquidus), °C | 1480 | |
| 640 |
| Melting Onset (Solidus), °C | 1430 | |
| 480 |
| Specific Heat Capacity, J/kg-K | 440 | |
| 860 |
| Thermal Conductivity, W/m-K | 10 | |
| 130 |
| Thermal Expansion, µm/m-K | 11 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.3 | |
| 36 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.4 | |
| 110 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 80 | |
| 10 |
| Density, g/cm3 | 8.6 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 14 | |
| 8.1 |
| Embodied Energy, MJ/kg | 190 | |
| 140 |
| Embodied Water, L/kg | 290 | |
| 1110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 200 | |
| 31 to 34 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 440 | |
| 1270 to 1440 |
| Stiffness to Weight: Axial, points | 13 | |
| 13 |
| Stiffness to Weight: Bending, points | 23 | |
| 45 |
| Strength to Weight: Axial, points | 28 | |
| 46 to 47 |
| Strength to Weight: Bending, points | 24 | |
| 46 to 47 |
| Thermal Diffusivity, mm2/s | 2.7 | |
| 51 |
| Thermal Shock Resistance, points | 29 | |
| 22 to 23 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.4 | |
| 85.7 to 89.5 |
| Carbon (C), % | 0.030 to 0.1 | |
| 0 |
| Chromium (Cr), % | 20 to 23 | |
| 0.1 to 0.22 |
| Cobalt (Co), % | 0 to 1.0 | |
| 0 |
| Copper (Cu), % | 0 to 0.5 | |
| 1.2 to 1.9 |
| Iron (Fe), % | 0 to 5.0 | |
| 0 to 0.35 |
| Magnesium (Mg), % | 0 | |
| 2.0 to 2.9 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 0.2 |
| Molybdenum (Mo), % | 8.0 to 10 | |
| 0 |
| Nickel (Ni), % | 58 to 68.8 | |
| 0 |
| Niobium (Nb), % | 3.2 to 4.2 | |
| 0 |
| Phosphorus (P), % | 0 to 0.020 | |
| 0 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 0.25 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0 to 0.4 | |
| 0 to 0.1 |
| Zinc (Zn), % | 0 | |
| 7.2 to 8.2 |
| Residuals, % | 0 | |
| 0 to 0.15 |