C46200 Brass vs. 7108A Aluminum
C46200 brass belongs to the copper alloys classification, while 7108A aluminum belongs to the aluminum alloys. There are 27 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 C46200 brass and the bottom bar is 7108A aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 69 |
| Elongation at Break, % | 17 to 34 | |
| 11 to 13 |
| Poisson's Ratio | 0.31 | |
| 0.33 |
| Shear Modulus, GPa | 40 | |
| 26 |
| Shear Strength, MPa | 240 to 290 | |
| 210 |
| Tensile Strength: Ultimate (UTS), MPa | 370 to 480 | |
| 350 |
| Tensile Strength: Yield (Proof), MPa | 120 to 290 | |
| 290 to 300 |
Thermal Properties
| Latent Heat of Fusion, J/g | 170 | |
| 380 |
| Maximum Temperature: Mechanical, °C | 120 | |
| 210 |
| Melting Completion (Liquidus), °C | 840 | |
| 630 |
| Melting Onset (Solidus), °C | 800 | |
| 520 |
| Specific Heat Capacity, J/kg-K | 380 | |
| 870 |
| Thermal Conductivity, W/m-K | 110 | |
| 150 |
| Thermal Expansion, µm/m-K | 20 | |
| 24 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 24 | |
| 10 |
| Density, g/cm3 | 8.1 | |
| 2.9 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 8.3 |
| Embodied Energy, MJ/kg | 46 | |
| 150 |
| Embodied Water, L/kg | 330 | |
| 1150 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 69 to 100 | |
| 38 to 44 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 72 to 400 | |
| 610 to 640 |
| Stiffness to Weight: Axial, points | 7.2 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 47 |
| Strength to Weight: Axial, points | 13 to 16 | |
| 33 to 34 |
| Strength to Weight: Bending, points | 14 to 17 | |
| 38 |
| Thermal Diffusivity, mm2/s | 35 | |
| 59 |
| Thermal Shock Resistance, points | 12 to 16 | |
| 15 to 16 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 91.6 to 94.4 |
| Chromium (Cr), % | 0 | |
| 0 to 0.040 |
| Copper (Cu), % | 62 to 65 | |
| 0 to 0.050 |
| Gallium (Ga), % | 0 | |
| 0 to 0.030 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.3 |
| Lead (Pb), % | 0 to 0.2 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.7 to 1.5 |
| Manganese (Mn), % | 0 | |
| 0 to 0.050 |
| Silicon (Si), % | 0 | |
| 0 to 0.2 |
| Tin (Sn), % | 0.5 to 1.0 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.030 |
| Zinc (Zn), % | 33.3 to 37.5 | |
| 4.8 to 5.8 |
| Zirconium (Zr), % | 0 | |
| 0.15 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |