6025 Aluminum vs. N06210 Nickel
6025 aluminum belongs to the aluminum alloys classification, while N06210 nickel belongs to the nickel alloys. There are 26 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 6025 aluminum and the bottom bar is N06210 nickel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 220 |
| Elongation at Break, % | 2.8 to 10 | |
| 51 |
| Fatigue Strength, MPa | 67 to 110 | |
| 320 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 26 | |
| 85 |
| Shear Strength, MPa | 110 to 140 | |
| 560 |
| Tensile Strength: Ultimate (UTS), MPa | 190 to 240 | |
| 780 |
| Tensile Strength: Yield (Proof), MPa | 68 to 210 | |
| 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 330 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 980 |
| Melting Completion (Liquidus), °C | 650 | |
| 1570 |
| Melting Onset (Solidus), °C | 550 | |
| 1510 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 420 |
| Thermal Expansion, µm/m-K | 23 | |
| 12 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 85 |
| Density, g/cm3 | 2.8 | |
| 9.0 |
| Embodied Carbon, kg CO2/kg material | 8.5 | |
| 17 |
| Embodied Energy, MJ/kg | 150 | |
| 250 |
| Embodied Water, L/kg | 1160 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 6.0 to 15 | |
| 320 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 33 to 310 | |
| 280 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 50 | |
| 22 |
| Strength to Weight: Axial, points | 19 to 24 | |
| 24 |
| Strength to Weight: Bending, points | 26 to 31 | |
| 21 |
| Thermal Shock Resistance, points | 8.2 to 10 | |
| 22 |
Alloy Composition
| Aluminum (Al), % | 91.7 to 96.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0 to 0.015 |
| Chromium (Cr), % | 0 to 0.2 | |
| 18 to 20 |
| Cobalt (Co), % | 0 | |
| 0 to 1.0 |
| Copper (Cu), % | 0.2 to 0.7 | |
| 0 |
| Iron (Fe), % | 0 to 0.7 | |
| 0 to 1.0 |
| Magnesium (Mg), % | 2.1 to 3.0 | |
| 0 |
| Manganese (Mn), % | 0.6 to 1.4 | |
| 0 to 0.5 |
| Molybdenum (Mo), % | 0 | |
| 18 to 20 |
| Nickel (Ni), % | 0 | |
| 54.8 to 62.5 |
| Phosphorus (P), % | 0 | |
| 0 to 0.020 |
| Silicon (Si), % | 0.8 to 1.5 | |
| 0 to 0.080 |
| Sulfur (S), % | 0 | |
| 0 to 0.020 |
| Tantalum (Ta), % | 0 | |
| 1.5 to 2.2 |
| Titanium (Ti), % | 0 to 0.2 | |
| 0 |
| Vanadium (V), % | 0 | |
| 0 to 0.35 |
| Zinc (Zn), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 to 0.15 | |
| 0 |