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C16500 Copper vs. 6016 Aluminum

C16500 copper belongs to the copper alloys classification, while 6016 aluminum belongs to the aluminum alloys. There are 29 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 C16500 copper and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
69
Elongation at Break, % 1.5 to 53
11 to 27
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
26
Shear Strength, MPa 200 to 310
130 to 170
Tensile Strength: Ultimate (UTS), MPa 280 to 530
200 to 280
Tensile Strength: Yield (Proof), MPa 97 to 520
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 210
410
Maximum Temperature: Mechanical, °C 340
160
Melting Completion (Liquidus), °C 1070
660
Melting Onset (Solidus), °C 1010
610
Specific Heat Capacity, J/kg-K 380
900
Thermal Conductivity, W/m-K 250
190 to 210
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 60
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 61
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 2.6
8.2
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 320
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.8 to 110
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 41 to 1160
82 to 340
Stiffness to Weight: Axial, points 7.1
14
Stiffness to Weight: Bending, points 18
51
Strength to Weight: Axial, points 8.6 to 17
21 to 29
Strength to Weight: Bending, points 11 to 16
29 to 35
Thermal Diffusivity, mm2/s 74
77 to 86
Thermal Shock Resistance, points 9.8 to 19
9.1 to 12

Alloy Composition


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Aluminum (Al), % 0
96.4 to 98.8
Cadmium (Cd), % 0.6 to 1.0
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 97.8 to 98.9
0 to 0.2
Iron (Fe), % 0 to 0.020
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0
0 to 0.2
Silicon (Si), % 0
1.0 to 1.5
Tin (Sn), % 0.5 to 0.7
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0 to 0.5
0 to 0.15