C69300 Brass vs. 6070 Aluminum
C69300 brass belongs to the copper alloys classification, while 6070 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 C69300 brass and the bottom bar is 6070 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 110 | |
| 70 |
| Elongation at Break, % | 8.5 to 15 | |
| 5.6 to 8.6 |
| Poisson's Ratio | 0.32 | |
| 0.33 |
| Shear Modulus, GPa | 41 | |
| 26 |
| Shear Strength, MPa | 330 to 370 | |
| 220 to 240 |
| Tensile Strength: Ultimate (UTS), MPa | 550 to 630 | |
| 370 to 380 |
| Tensile Strength: Yield (Proof), MPa | 300 to 390 | |
| 350 |
Thermal Properties
| Latent Heat of Fusion, J/g | 240 | |
| 410 |
| Maximum Temperature: Mechanical, °C | 160 | |
| 160 |
| Melting Completion (Liquidus), °C | 880 | |
| 650 |
| Melting Onset (Solidus), °C | 860 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 400 | |
| 900 |
| Thermal Conductivity, W/m-K | 38 | |
| 160 |
| Thermal Expansion, µm/m-K | 19 | |
| 23 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 8.0 | |
| 41 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 8.8 | |
| 140 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 26 | |
| 9.5 |
| Density, g/cm3 | 8.2 | |
| 2.7 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 8.3 |
| Embodied Energy, MJ/kg | 45 | |
| 150 |
| Embodied Water, L/kg | 310 | |
| 1170 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 47 to 70 | |
| 20 to 32 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 400 to 700 | |
| 880 to 900 |
| Stiffness to Weight: Axial, points | 7.4 | |
| 14 |
| Stiffness to Weight: Bending, points | 19 | |
| 50 |
| Strength to Weight: Axial, points | 19 to 21 | |
| 38 |
| Strength to Weight: Bending, points | 18 to 20 | |
| 42 to 43 |
| Thermal Diffusivity, mm2/s | 12 | |
| 65 |
| Thermal Shock Resistance, points | 19 to 22 | |
| 16 to 17 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 94.6 to 98 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 73 to 77 | |
| 0.15 to 0.4 |
| Iron (Fe), % | 0 to 0.1 | |
| 0 to 0.5 |
| Lead (Pb), % | 0 to 0.090 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 0.5 to 1.2 |
| Manganese (Mn), % | 0 to 0.1 | |
| 0.4 to 1.0 |
| Nickel (Ni), % | 0 to 0.1 | |
| 0 |
| Phosphorus (P), % | 0.040 to 0.15 | |
| 0 |
| Silicon (Si), % | 2.7 to 3.4 | |
| 1.0 to 1.7 |
| Tin (Sn), % | 0 to 0.2 | |
| 0 |
| Titanium (Ti), % | 0 | |
| 0 to 0.15 |
| Zinc (Zn), % | 18.4 to 24.3 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |