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C19010 Copper vs. 5082 Aluminum

C19010 copper belongs to the copper alloys classification, while 5082 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 C19010 copper and the bottom bar is 5082 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
67
Elongation at Break, % 2.4 to 22
1.1
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
25
Shear Strength, MPa 210 to 360
210 to 230
Tensile Strength: Ultimate (UTS), MPa 330 to 640
380 to 400
Tensile Strength: Yield (Proof), MPa 260 to 620
300 to 340

Thermal Properties

Latent Heat of Fusion, J/g 210
400
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1060
640
Melting Onset (Solidus), °C 1010
560
Specific Heat Capacity, J/kg-K 390
910
Thermal Conductivity, W/m-K 260
130
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48 to 63
32
Electrical Conductivity: Equal Weight (Specific), % IACS 48 to 63
110

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.9
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 310
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.3 to 140
4.0 to 4.3
Resilience: Unit (Modulus of Resilience), kJ/m3 290 to 1680
670 to 870
Stiffness to Weight: Axial, points 7.3
14
Stiffness to Weight: Bending, points 18
51
Strength to Weight: Axial, points 10 to 20
39 to 41
Strength to Weight: Bending, points 12 to 18
43 to 45
Thermal Diffusivity, mm2/s 75
54
Thermal Shock Resistance, points 12 to 23
17 to 18

Alloy Composition


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Aluminum (Al), % 0
93.5 to 96
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 97.3 to 99.04
0 to 0.15
Iron (Fe), % 0
0 to 0.35
Magnesium (Mg), % 0
4.0 to 5.0
Manganese (Mn), % 0
0 to 0.15
Nickel (Ni), % 0.8 to 1.8
0
Phosphorus (P), % 0.010 to 0.050
0
Silicon (Si), % 0.15 to 0.35
0 to 0.2
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0 to 0.5
0 to 0.15