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C18700 Copper vs. 355.0 Aluminum

C18700 copper belongs to the copper alloys classification, while 355.0 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 C18700 copper and the bottom bar is 355.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
71
Elongation at Break, % 9.0 to 9.6
1.5 to 2.6
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
27
Shear Strength, MPa 170 to 190
150 to 240
Tensile Strength: Ultimate (UTS), MPa 290 to 330
200 to 260
Tensile Strength: Yield (Proof), MPa 230 to 250
150 to 190

Thermal Properties

Latent Heat of Fusion, J/g 210
470
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1080
620
Melting Onset (Solidus), °C 950
560
Specific Heat Capacity, J/kg-K 380
890
Thermal Conductivity, W/m-K 380
150 to 170
Thermal Expansion, µm/m-K 17
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 98
38 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 99
120 to 140

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 9.0
2.7
Embodied Carbon, kg CO2/kg material 2.6
8.0
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 310
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 29
2.7 to 5.9
Resilience: Unit (Modulus of Resilience), kJ/m3 240 to 280
150 to 250
Stiffness to Weight: Axial, points 7.1
14
Stiffness to Weight: Bending, points 18
51
Strength to Weight: Axial, points 9.0 to 10
20 to 27
Strength to Weight: Bending, points 11 to 12
28 to 33
Thermal Diffusivity, mm2/s 110
60 to 69
Thermal Shock Resistance, points 10 to 12
9.1 to 12

Alloy Composition

Aluminum (Al), % 0
90.3 to 94.1
Chromium (Cr), % 0
0 to 0.25
Copper (Cu), % 98 to 99.2
1.0 to 1.5
Iron (Fe), % 0
0 to 0.6
Lead (Pb), % 0.8 to 1.5
0
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0
0 to 0.5
Silicon (Si), % 0
4.5 to 5.5
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15