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6182 Aluminum vs. C19010 Copper

6182 aluminum belongs to the aluminum alloys classification, while C19010 copper belongs to the copper 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 6182 aluminum and the bottom bar is C19010 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
120
Elongation at Break, % 6.8 to 13
2.4 to 22
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 140 to 190
210 to 360
Tensile Strength: Ultimate (UTS), MPa 230 to 320
330 to 640
Tensile Strength: Yield (Proof), MPa 130 to 270
260 to 620

Thermal Properties

Latent Heat of Fusion, J/g 410
210
Maximum Temperature: Mechanical, °C 190
200
Melting Completion (Liquidus), °C 640
1060
Melting Onset (Solidus), °C 600
1010
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 160
260
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
48 to 63
Electrical Conductivity: Equal Weight (Specific), % IACS 130
48 to 63

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.9
Embodied Carbon, kg CO2/kg material 8.4
2.7
Embodied Energy, MJ/kg 150
42
Embodied Water, L/kg 1170
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 21 to 26
7.3 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 520
290 to 1680
Stiffness to Weight: Axial, points 14
7.3
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 23 to 32
10 to 20
Strength to Weight: Bending, points 30 to 38
12 to 18
Thermal Diffusivity, mm2/s 65
75
Thermal Shock Resistance, points 10 to 14
12 to 23

Alloy Composition

Aluminum (Al), % 95 to 97.9
0
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.1
97.3 to 99.04
Iron (Fe), % 0 to 0.5
0
Magnesium (Mg), % 0.7 to 1.2
0
Manganese (Mn), % 0.5 to 1.0
0
Nickel (Ni), % 0
0.8 to 1.8
Phosphorus (P), % 0
0.010 to 0.050
Silicon (Si), % 0.9 to 1.3
0.15 to 0.35
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.050 to 0.2
0
Residuals, % 0
0 to 0.5