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242.0 Aluminum vs. C18600 Copper

242.0 aluminum belongs to the aluminum alloys classification, while C18600 copper belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 242.0 aluminum and the bottom bar is C18600 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
120
Elongation at Break, % 0.5 to 1.5
8.0 to 11
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 27
44
Shear Strength, MPa 150 to 240
310 to 340
Tensile Strength: Ultimate (UTS), MPa 180 to 290
520 to 580
Tensile Strength: Yield (Proof), MPa 120 to 220
500 to 520

Thermal Properties

Latent Heat of Fusion, J/g 390
210
Maximum Temperature: Mechanical, °C 210
200
Melting Completion (Liquidus), °C 640
1090
Melting Onset (Solidus), °C 530
1070
Specific Heat Capacity, J/kg-K 870
390
Thermal Conductivity, W/m-K 130 to 170
280
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
70
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
71

Otherwise Unclassified Properties

Base Metal Price, % relative 12
31
Density, g/cm3 3.1
8.9
Embodied Carbon, kg CO2/kg material 8.3
2.9
Embodied Energy, MJ/kg 150
46
Embodied Water, L/kg 1130
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
44 to 58
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
1060 to 1180
Stiffness to Weight: Axial, points 13
7.3
Stiffness to Weight: Bending, points 45
18
Strength to Weight: Axial, points 16 to 26
16 to 18
Strength to Weight: Bending, points 23 to 32
16 to 17
Thermal Diffusivity, mm2/s 50 to 62
81
Thermal Shock Resistance, points 8.0 to 13
19 to 20

Alloy Composition

Aluminum (Al), % 88.4 to 93.6
0
Chromium (Cr), % 0 to 0.25
0.1 to 1.0
Cobalt (Co), % 0
0 to 0.1
Copper (Cu), % 3.5 to 4.5
96.5 to 99.55
Iron (Fe), % 0 to 1.0
0.25 to 0.8
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0
Nickel (Ni), % 1.7 to 2.3
0 to 0.25
Silicon (Si), % 0 to 0.7
0
Titanium (Ti), % 0 to 0.25
0.050 to 0.5
Zinc (Zn), % 0 to 0.35
0
Zirconium (Zr), % 0
0.050 to 0.4
Residuals, % 0
0 to 0.5