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C70260 Copper vs. 6066 Aluminum

C70260 copper belongs to the copper alloys classification, while 6066 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 C70260 copper and the bottom bar is 6066 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 9.5 to 19
7.8 to 17
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 44
26
Shear Strength, MPa 320 to 450
95 to 240
Tensile Strength: Ultimate (UTS), MPa 520 to 760
160 to 400
Tensile Strength: Yield (Proof), MPa 410 to 650
93 to 360

Thermal Properties

Latent Heat of Fusion, J/g 220
410
Maximum Temperature: Mechanical, °C 200
170
Melting Completion (Liquidus), °C 1060
650
Melting Onset (Solidus), °C 1040
560
Specific Heat Capacity, J/kg-K 390
890
Thermal Conductivity, W/m-K 160
150
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40 to 50
40
Electrical Conductivity: Equal Weight (Specific), % IACS 40 to 51
130

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.9
2.8
Embodied Carbon, kg CO2/kg material 2.7
8.3
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 310
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 46 to 140
23 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 1810
61 to 920
Stiffness to Weight: Axial, points 7.3
14
Stiffness to Weight: Bending, points 18
49
Strength to Weight: Axial, points 16 to 24
16 to 39
Strength to Weight: Bending, points 16 to 21
23 to 43
Thermal Diffusivity, mm2/s 45
61
Thermal Shock Resistance, points 18 to 27
6.9 to 17

Alloy Composition


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Aluminum (Al), % 0
93 to 97
Chromium (Cr), % 0
0 to 0.4
Copper (Cu), % 95.8 to 98.8
0.7 to 1.2
Iron (Fe), % 0
0 to 0.5
Magnesium (Mg), % 0
0.8 to 1.4
Manganese (Mn), % 0
0.6 to 1.1
Nickel (Ni), % 1.0 to 3.0
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0.2 to 0.7
0.9 to 1.8
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0 to 0.5
0 to 0.15