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C18600 Copper vs. 333.0 Aluminum

C18600 copper belongs to the copper alloys classification, while 333.0 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 C18600 copper and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
73
Elongation at Break, % 8.0 to 11
1.0 to 2.0
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 44
28
Shear Strength, MPa 310 to 340
190 to 230
Tensile Strength: Ultimate (UTS), MPa 520 to 580
230 to 280
Tensile Strength: Yield (Proof), MPa 500 to 520
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 210
520
Maximum Temperature: Mechanical, °C 200
170
Melting Completion (Liquidus), °C 1090
590
Melting Onset (Solidus), °C 1070
530
Specific Heat Capacity, J/kg-K 390
880
Thermal Conductivity, W/m-K 280
100 to 140
Thermal Expansion, µm/m-K 17
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 70
26 to 35
Electrical Conductivity: Equal Weight (Specific), % IACS 71
83 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 31
10
Density, g/cm3 8.9
2.8
Embodied Carbon, kg CO2/kg material 2.9
7.6
Embodied Energy, MJ/kg 46
140
Embodied Water, L/kg 310
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 44 to 58
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 1060 to 1180
120 to 290
Stiffness to Weight: Axial, points 7.3
14
Stiffness to Weight: Bending, points 18
49
Strength to Weight: Axial, points 16 to 18
22 to 27
Strength to Weight: Bending, points 16 to 17
29 to 34
Thermal Diffusivity, mm2/s 81
42 to 57
Thermal Shock Resistance, points 19 to 20
11 to 13

Alloy Composition

Aluminum (Al), % 0
81.8 to 89
Chromium (Cr), % 0.1 to 1.0
0
Cobalt (Co), % 0 to 0.1
0
Copper (Cu), % 96.5 to 99.55
3.0 to 4.0
Iron (Fe), % 0.25 to 0.8
0 to 1.0
Magnesium (Mg), % 0
0.050 to 0.5
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.25
0 to 0.5
Silicon (Si), % 0
8.0 to 10
Titanium (Ti), % 0.050 to 0.5
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Zirconium (Zr), % 0.050 to 0.4
0
Residuals, % 0
0 to 0.5