6070 Aluminum vs. C43400 Brass
6070 aluminum belongs to the aluminum alloys classification, while C43400 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 6070 aluminum and the bottom bar is C43400 brass.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 70 | |
| 110 |
| Elongation at Break, % | 5.6 to 8.6 | |
| 3.0 to 49 |
| Poisson's Ratio | 0.33 | |
| 0.33 |
| Shear Modulus, GPa | 26 | |
| 42 |
| Shear Strength, MPa | 220 to 240 | |
| 250 to 390 |
| Tensile Strength: Ultimate (UTS), MPa | 370 to 380 | |
| 310 to 690 |
| Tensile Strength: Yield (Proof), MPa | 350 | |
| 110 to 560 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 190 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 170 |
| Melting Completion (Liquidus), °C | 650 | |
| 1020 |
| Melting Onset (Solidus), °C | 570 | |
| 990 |
| Specific Heat Capacity, J/kg-K | 900 | |
| 380 |
| Thermal Conductivity, W/m-K | 160 | |
| 140 |
| Thermal Expansion, µm/m-K | 23 | |
| 19 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 41 | |
| 31 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
| 32 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 28 |
| Density, g/cm3 | 2.7 | |
| 8.6 |
| Embodied Carbon, kg CO2/kg material | 8.3 | |
| 2.7 |
| Embodied Energy, MJ/kg | 150 | |
| 44 |
| Embodied Water, L/kg | 1170 | |
| 320 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 20 to 32 | |
| 19 to 120 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 880 to 900 | |
| 57 to 1420 |
| Stiffness to Weight: Axial, points | 14 | |
| 7.2 |
| Stiffness to Weight: Bending, points | 50 | |
| 19 |
| Strength to Weight: Axial, points | 38 | |
| 10 to 22 |
| Strength to Weight: Bending, points | 42 to 43 | |
| 12 to 20 |
| Thermal Diffusivity, mm2/s | 65 | |
| 41 |
| Thermal Shock Resistance, points | 16 to 17 | |
| 11 to 24 |
Alloy Composition
| Aluminum (Al), % | 94.6 to 98 | |
| 0 |
| Chromium (Cr), % | 0 to 0.1 | |
| 0 |
| Copper (Cu), % | 0.15 to 0.4 | |
| 84 to 87 |
| Iron (Fe), % | 0 to 0.5 | |
| 0 to 0.050 |
| Lead (Pb), % | 0 | |
| 0 to 0.050 |
| Magnesium (Mg), % | 0.5 to 1.2 | |
| 0 |
| Manganese (Mn), % | 0.4 to 1.0 | |
| 0 |
| Silicon (Si), % | 1.0 to 1.7 | |
| 0 |
| Tin (Sn), % | 0 | |
| 0.4 to 1.0 |
| Titanium (Ti), % | 0 to 0.15 | |
| 0 |
| Zinc (Zn), % | 0 to 0.25 | |
| 11.4 to 15.6 |
| Residuals, % | 0 | |
| 0 to 0.5 |