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2218 Aluminum vs. C16200 Copper

2218 aluminum belongs to the aluminum alloys classification, while C16200 copper belongs to the copper alloys. There are 30 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 2218 aluminum and the bottom bar is C16200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
120
Elongation at Break, % 6.8 to 10
2.0 to 56
Fatigue Strength, MPa 110
100 to 210
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 27
43
Shear Strength, MPa 210 to 250
190 to 390
Tensile Strength: Ultimate (UTS), MPa 330 to 430
240 to 550
Tensile Strength: Yield (Proof), MPa 260 to 310
48 to 470

Thermal Properties

Latent Heat of Fusion, J/g 390
210
Maximum Temperature: Mechanical, °C 220
370
Melting Completion (Liquidus), °C 640
1080
Melting Onset (Solidus), °C 510
1030
Specific Heat Capacity, J/kg-K 870
380
Thermal Conductivity, W/m-K 140
360
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
90
Electrical Conductivity: Equal Weight (Specific), % IACS 110
90

Otherwise Unclassified Properties

Base Metal Price, % relative 11
30
Density, g/cm3 3.1
9.0
Embodied Carbon, kg CO2/kg material 8.2
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1130
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
10 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
10 to 970
Stiffness to Weight: Axial, points 13
7.2
Stiffness to Weight: Bending, points 45
18
Strength to Weight: Axial, points 30 to 39
7.4 to 17
Strength to Weight: Bending, points 34 to 41
9.6 to 17
Thermal Diffusivity, mm2/s 52
100
Thermal Shock Resistance, points 15 to 19
8.7 to 20

Alloy Composition

Aluminum (Al), % 88.8 to 93.6
0
Cadmium (Cd), % 0
0.7 to 1.2
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 3.5 to 4.5
98.6 to 99.3
Iron (Fe), % 0 to 1.0
0 to 0.2
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
0
Nickel (Ni), % 1.7 to 2.3
0
Silicon (Si), % 0 to 0.9
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0