C66900 Brass vs. EN AC-42200 Aluminum
C66900 brass belongs to the copper alloys classification, while EN AC-42200 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, 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 C66900 brass and the bottom bar is EN AC-42200 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 120 | |
| 70 |
| Elongation at Break, % | 1.1 to 26 | |
| 3.0 to 6.7 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 45 | |
| 26 |
| Tensile Strength: Ultimate (UTS), MPa | 460 to 770 | |
| 320 |
| Tensile Strength: Yield (Proof), MPa | 330 to 760 | |
| 240 to 260 |
Thermal Properties
| Latent Heat of Fusion, J/g | 190 | |
| 500 |
| Maximum Temperature: Mechanical, °C | 150 | |
| 170 |
| Melting Completion (Liquidus), °C | 860 | |
| 610 |
| Melting Onset (Solidus), °C | 850 | |
| 600 |
| Specific Heat Capacity, J/kg-K | 400 | |
| 910 |
| Thermal Expansion, µm/m-K | 20 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 3.4 | |
| 40 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 3.8 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 23 | |
| 9.5 |
| Density, g/cm3 | 8.2 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 8.0 |
| Embodied Energy, MJ/kg | 46 | |
| 150 |
| Embodied Water, L/kg | 310 | |
| 1110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 4.6 to 200 | |
| 9.0 to 20 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 2450 | |
| 410 to 490 |
| Stiffness to Weight: Axial, points | 8.1 | |
| 15 |
| Stiffness to Weight: Bending, points | 20 | |
| 53 |
| Strength to Weight: Axial, points | 15 to 26 | |
| 34 to 35 |
| Strength to Weight: Bending, points | 16 to 23 | |
| 40 to 41 |
| Thermal Shock Resistance, points | 14 to 23 | |
| 15 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 91 to 93.1 |
| Copper (Cu), % | 62.5 to 64.5 | |
| 0 to 0.050 |
| Iron (Fe), % | 0 to 0.25 | |
| 0 to 0.19 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.45 to 0.7 |
| Manganese (Mn), % | 11.5 to 12.5 | |
| 0 to 0.1 |
| Silicon (Si), % | 0 | |
| 6.5 to 7.5 |
| Titanium (Ti), % | 0 | |
| 0 to 0.25 |
| Zinc (Zn), % | 22.5 to 26 | |
| 0 to 0.070 |
| Residuals, % | 0 | |
| 0 to 0.1 |