C66200 Brass vs. 7050 Aluminum
C66200 brass belongs to the copper alloys classification, while 7050 aluminum belongs to the aluminum 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 C66200 brass and the bottom bar is 7050 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 70 |
| Elongation at Break, % | 8.0 to 15 | |
| 2.2 to 12 |
| Poisson's Ratio | 0.33 | |
| 0.32 |
| Shear Modulus, GPa | 42 | |
| 26 |
| Shear Strength, MPa | 270 to 300 | |
| 280 to 330 |
| Tensile Strength: Ultimate (UTS), MPa | 450 to 520 | |
| 490 to 570 |
| Tensile Strength: Yield (Proof), MPa | 410 to 480 | |
| 390 to 500 |
Thermal Properties
| Latent Heat of Fusion, J/g | 200 | |
| 370 |
| Maximum Temperature: Mechanical, °C | 180 | |
| 190 |
| Melting Completion (Liquidus), °C | 1070 | |
| 630 |
| Melting Onset (Solidus), °C | 1030 | |
| 490 |
| Specific Heat Capacity, J/kg-K | 390 | |
| 860 |
| Thermal Conductivity, W/m-K | 150 | |
| 140 |
| Thermal Expansion, µm/m-K | 18 | |
| 24 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 35 | |
| 35 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 36 | |
| 100 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 29 | |
| 10 |
| Density, g/cm3 | 8.7 | |
| 3.1 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 8.2 |
| Embodied Energy, MJ/kg | 43 | |
| 150 |
| Embodied Water, L/kg | 320 | |
| 1120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 40 to 66 | |
| 10 to 55 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 760 to 1030 | |
| 1110 to 1760 |
| Stiffness to Weight: Axial, points | 7.2 | |
| 13 |
| Stiffness to Weight: Bending, points | 19 | |
| 45 |
| Strength to Weight: Axial, points | 14 to 17 | |
| 45 to 51 |
| Strength to Weight: Bending, points | 15 to 16 | |
| 45 to 50 |
| Thermal Diffusivity, mm2/s | 45 | |
| 54 |
| Thermal Shock Resistance, points | 16 to 18 | |
| 21 to 25 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 87.3 to 92.1 |
| Chromium (Cr), % | 0 | |
| 0 to 0.040 |
| Copper (Cu), % | 86.6 to 91 | |
| 2.0 to 2.6 |
| Iron (Fe), % | 0 to 0.050 | |
| 0 to 0.15 |
| Lead (Pb), % | 0 to 0.050 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 1.9 to 2.6 |
| 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 0.12 |
| Tin (Sn), % | 0.2 to 0.7 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.060 |
| Zinc (Zn), % | 6.5 to 12.9 | |
| 5.7 to 6.7 |
| Zirconium (Zr), % | 0 | |
| 0.080 to 0.15 |
| Residuals, % | 0 | |
| 0 to 0.15 |