C66200 Brass vs. 712.0 Aluminum
C66200 brass belongs to the copper alloys classification, while 712.0 aluminum belongs to the aluminum 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 C66200 brass and the bottom bar is 712.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 70 |
| Elongation at Break, % | 8.0 to 15 | |
| 4.5 to 4.7 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 42 | |
| 27 |
| Shear Strength, MPa | 270 to 300 | |
| 180 |
| Tensile Strength: Ultimate (UTS), MPa | 450 to 520 | |
| 250 to 260 |
| Tensile Strength: Yield (Proof), MPa | 410 to 480 | |
| 180 to 200 |
Thermal Properties
| Latent Heat of Fusion, J/g | 200 | |
| 380 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 190 |
| Melting Completion (Liquidus), °C | 1070 | |
| 640 |
| Melting Onset (Solidus), °C | 1030 | |
| 610 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 870 |
| Thermal Conductivity, W/m-K | 150 | |
| 160 |
| Thermal Expansion, µm/m-K | 18 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 40 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 36 | |
| 120 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 29 | |
| 9.5 |
| Density, g/cm3 | 8.7 | |
| 3.0 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 8.0 |
| Embodied Energy, MJ/kg | 43 | |
| 150 |
| Embodied Water, L/kg | 320 | |
| 1140 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 40 to 66 | |
| 11 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 760 to 1030 | |
| 240 to 270 |
| Stiffness to Weight: Axial, points | 7.2 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 46 |
| Strength to Weight: Axial, points | 14 to 17 | |
| 24 to 25 |
| Strength to Weight: Bending, points | 15 to 16 | |
| 30 to 31 |
| Thermal Diffusivity, mm2/s | 45 | |
| 62 |
| Thermal Shock Resistance, points | 16 to 18 | |
| 11 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 90.7 to 94 |
| Chromium (Cr), % | 0 | |
| 0.4 to 0.6 |
| Copper (Cu), % | 86.6 to 91 | |
| 0 to 0.25 |
| Iron (Fe), % | 0 to 0.050 | |
| 0 to 0.5 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.5 to 0.65 |
| Manganese (Mn), % | 0 | |
| 0 to 0.1 |
| Nickel (Ni), % | 0.3 to 1.0 | |
| 0 |
| Phosphorus (P), % | 0.050 to 0.2 | |
| 0 |
| Silicon (Si), % | 0 | |
| 0 to 0.3 |
| Tin (Sn), % | 0.2 to 0.7 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0.15 to 0.25 |
| Zinc (Zn), % | 6.5 to 12.9 | |
| 5.0 to 6.5 |
| Residuals, % | 0 | |
| 0 to 0.2 |