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5052 Aluminum vs. C16200 Copper

5052 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 (2, 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 5052 aluminum and the bottom bar is C16200 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 1.1 to 22
2.0 to 56
Fatigue Strength, MPa 66 to 140
100 to 210
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 120 to 180
190 to 390
Tensile Strength: Ultimate (UTS), MPa 190 to 320
240 to 550
Tensile Strength: Yield (Proof), MPa 75 to 280
48 to 470

Thermal Properties

Latent Heat of Fusion, J/g 400
210
Maximum Temperature: Mechanical, °C 190
370
Melting Completion (Liquidus), °C 650
1080
Melting Onset (Solidus), °C 610
1030
Specific Heat Capacity, J/kg-K 900
380
Thermal Conductivity, W/m-K 140
360
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
90
Electrical Conductivity: Equal Weight (Specific), % IACS 120
90

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.7
9.0
Embodied Carbon, kg CO2/kg material 8.6
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1190
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.7 to 69
10 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 41 to 590
10 to 970
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 19 to 33
7.4 to 17
Strength to Weight: Bending, points 27 to 38
9.6 to 17
Thermal Diffusivity, mm2/s 57
100
Thermal Shock Resistance, points 8.3 to 14
8.7 to 20

Alloy Composition

Aluminum (Al), % 95.8 to 97.7
0
Cadmium (Cd), % 0
0.7 to 1.2
Chromium (Cr), % 0.15 to 0.35
0
Copper (Cu), % 0 to 0.1
98.6 to 99.3
Iron (Fe), % 0 to 0.4
0 to 0.2
Magnesium (Mg), % 2.2 to 2.8
0
Manganese (Mn), % 0 to 0.1
0
Silicon (Si), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0