N06255 Nickel vs. 6262A Aluminum
N06255 nickel belongs to the nickel alloys classification, while 6262A aluminum belongs to the aluminum 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 N06255 nickel and the bottom bar is 6262A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 210 | |
| 68 |
| Elongation at Break, % | 45 | |
| 4.5 to 11 |
| Fatigue Strength, MPa | 210 | |
| 94 to 110 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 81 | |
| 26 |
| Shear Strength, MPa | 460 | |
| 190 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 660 | |
| 310 to 410 |
| Tensile Strength: Yield (Proof), MPa | 250 | |
| 270 to 370 |
Thermal Properties
| Latent Heat of Fusion, J/g | 320 | |
| 400 |
| Maximum Temperature: Mechanical, °C | 1000 | |
| 160 |
| Melting Completion (Liquidus), °C | 1470 | |
| 640 |
| Melting Onset (Solidus), °C | 1420 | |
| 580 |
| Specific Heat Capacity, J/kg-K | 450 | |
| 890 |
| Thermal Expansion, µm/m-K | 13 | |
| 23 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 55 | |
| 11 |
| Density, g/cm3 | 8.5 | |
| 2.8 |
| Embodied Carbon, kg CO2/kg material | 9.4 | |
| 8.4 |
| Embodied Energy, MJ/kg | 130 | |
| 150 |
| Embodied Water, L/kg | 270 | |
| 1190 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 230 | |
| 17 to 34 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 150 | |
| 540 to 1000 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 23 | |
| 49 |
| Strength to Weight: Axial, points | 22 | |
| 31 to 41 |
| Strength to Weight: Bending, points | 20 | |
| 36 to 44 |
| Thermal Shock Resistance, points | 17 | |
| 14 to 18 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 94.2 to 97.8 |
| Bismuth (Bi), % | 0 | |
| 0.4 to 0.9 |
| Carbon (C), % | 0 to 0.030 | |
| 0 |
| Chromium (Cr), % | 23 to 26 | |
| 0.040 to 0.14 |
| Copper (Cu), % | 0 to 1.2 | |
| 0.15 to 0.4 |
| Iron (Fe), % | 6.0 to 24 | |
| 0 to 0.7 |
| Magnesium (Mg), % | 0 | |
| 0.8 to 1.2 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 0.15 |
| Molybdenum (Mo), % | 6.0 to 9.0 | |
| 0 |
| Nickel (Ni), % | 47 to 52 | |
| 0 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0.4 to 0.8 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0.4 to 1.0 |
| Titanium (Ti), % | 0 to 0.69 | |
| 0 to 0.1 |
| Tungsten (W), % | 0 to 3.0 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |