6110 Aluminum vs. C73100 Nickel Silver
6110 aluminum belongs to the aluminum alloys classification, while C73100 nickel silver belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (1, 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 6110 aluminum and the bottom bar is C73100 nickel silver.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 2.2 | |
| 3.4 to 8.0 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 26 | |
| 43 |
| Shear Strength, MPa | 290 | |
| 260 to 370 |
| Tensile Strength: Ultimate (UTS), MPa | 500 | |
| 450 to 640 |
| Tensile Strength: Yield (Proof), MPa | 500 | |
| 420 to 590 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 190 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 170 |
| Melting Completion (Liquidus), °C | 640 | |
| 1030 |
| Melting Onset (Solidus), °C | 600 | |
| 1000 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 390 |
| Thermal Conductivity, W/m-K | 170 | |
| 35 |
| Thermal Expansion, µm/m-K | 23 | |
| 19 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 42 | |
| 7.5 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 8.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 28 |
| Density, g/cm3 | 2.8 | |
| 8.4 |
| Embodied Carbon, kg CO2/kg material | 8.2 | |
| 3.0 |
| Embodied Energy, MJ/kg | 150 | |
| 49 |
| Embodied Water, L/kg | 1170 | |
| 310 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 11 | |
| 21 to 35 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1770 | |
| 790 to 1560 |
| Stiffness to Weight: Axial, points | 14 | |
| 7.5 |
| Stiffness to Weight: Bending, points | 50 | |
| 19 |
| Strength to Weight: Axial, points | 51 | |
| 15 to 21 |
| Strength to Weight: Bending, points | 51 | |
| 15 to 20 |
| Thermal Diffusivity, mm2/s | 67 | |
| 11 |
| Thermal Shock Resistance, points | 22 | |
| 15 to 21 |
Alloy Composition
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| Aluminum (Al), % | 94.4 to 98.4 | |
| 0 |
| Chromium (Cr), % | 0.040 to 0.25 | |
| 0 |
| Copper (Cu), % | 0.2 to 0.7 | |
| 70.8 to 78 |
| Iron (Fe), % | 0 to 0.8 | |
| 0 to 0.1 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Magnesium (Mg), % | 0.5 to 1.1 | |
| 0 |
| Manganese (Mn), % | 0.2 to 0.7 | |
| 0 to 0.5 |
| Nickel (Ni), % | 0 | |
| 4.0 to 6.0 |
| Silicon (Si), % | 0.7 to 1.5 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0 to 0.1 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 0 to 0.3 | |
| 18 to 22 |
| Residuals, % | 0 to 0.15 | |
| 0 to 0.5 |