6065 Aluminum vs. C69300 Brass
6065 aluminum belongs to the aluminum alloys classification, while C69300 brass belongs to the copper 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 6065 aluminum and the bottom bar is C69300 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
110 |
Elongation at Break, % | 4.5 to 11 | |
8.5 to 15 |
Poisson's Ratio | 0.33 | |
0.32 |
Shear Modulus, GPa | 26 | |
41 |
Shear Strength, MPa | 190 to 230 | |
330 to 370 |
Tensile Strength: Ultimate (UTS), MPa | 310 to 400 | |
550 to 630 |
Tensile Strength: Yield (Proof), MPa | 270 to 380 | |
300 to 390 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
240 |
Maximum Temperature: Mechanical, °C | 180 | |
160 |
Melting Completion (Liquidus), °C | 640 | |
880 |
Melting Onset (Solidus), °C | 590 | |
860 |
Specific Heat Capacity, J/kg-K | 890 | |
400 |
Thermal Conductivity, W/m-K | 170 | |
38 |
Thermal Expansion, µm/m-K | 23 | |
19 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 43 | |
8.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
8.8 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 11 | |
26 |
Density, g/cm3 | 2.8 | |
8.2 |
Embodied Carbon, kg CO2/kg material | 8.4 | |
2.7 |
Embodied Energy, MJ/kg | 150 | |
45 |
Embodied Water, L/kg | 1200 | |
310 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 17 to 34 | |
47 to 70 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 540 to 1040 | |
400 to 700 |
Stiffness to Weight: Axial, points | 14 | |
7.4 |
Stiffness to Weight: Bending, points | 49 | |
19 |
Strength to Weight: Axial, points | 31 to 40 | |
19 to 21 |
Strength to Weight: Bending, points | 36 to 43 | |
18 to 20 |
Thermal Diffusivity, mm2/s | 67 | |
12 |
Thermal Shock Resistance, points | 14 to 18 | |
19 to 22 |
Alloy Composition
Aluminum (Al), % | 94.4 to 98.2 | |
0 |
Bismuth (Bi), % | 0.5 to 1.5 | |
0 |
Chromium (Cr), % | 0 to 0.15 | |
0 |
Copper (Cu), % | 0.15 to 0.4 | |
73 to 77 |
Iron (Fe), % | 0 to 0.7 | |
0 to 0.1 |
Lead (Pb), % | 0 to 0.050 | |
0 to 0.090 |
Magnesium (Mg), % | 0.8 to 1.2 | |
0 |
Manganese (Mn), % | 0 to 0.15 | |
0 to 0.1 |
Nickel (Ni), % | 0 | |
0 to 0.1 |
Phosphorus (P), % | 0 | |
0.040 to 0.15 |
Silicon (Si), % | 0.4 to 0.8 | |
2.7 to 3.4 |
Tin (Sn), % | 0 | |
0 to 0.2 |
Titanium (Ti), % | 0 to 0.1 | |
0 |
Zinc (Zn), % | 0 to 0.25 | |
18.4 to 24.3 |
Zirconium (Zr), % | 0 to 0.15 | |
0 |
Residuals, % | 0 | |
0 to 0.5 |