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5086 Aluminum vs. C16200 Copper

5086 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 (3, 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 5086 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, % 1.7 to 20
2.0 to 56
Fatigue Strength, MPa 88 to 180
100 to 210
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 160 to 230
190 to 390
Tensile Strength: Ultimate (UTS), MPa 270 to 390
240 to 550
Tensile Strength: Yield (Proof), MPa 110 to 320
48 to 470

Thermal Properties

Latent Heat of Fusion, J/g 400
210
Maximum Temperature: Mechanical, °C 190
370
Melting Completion (Liquidus), °C 640
1080
Melting Onset (Solidus), °C 590
1030
Specific Heat Capacity, J/kg-K 900
380
Thermal Conductivity, W/m-K 130
360
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
90
Electrical Conductivity: Equal Weight (Specific), % IACS 100
90

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.7
9.0
Embodied Carbon, kg CO2/kg material 8.8
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1180
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.8 to 42
10 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 86 to 770
10 to 970
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 28 to 40
7.4 to 17
Strength to Weight: Bending, points 34 to 44
9.6 to 17
Thermal Diffusivity, mm2/s 52
100
Thermal Shock Resistance, points 12 to 17
8.7 to 20

Alloy Composition

Aluminum (Al), % 93 to 96.3
0
Cadmium (Cd), % 0
0.7 to 1.2
Chromium (Cr), % 0.050 to 0.25
0
Copper (Cu), % 0 to 0.1
98.6 to 99.3
Iron (Fe), % 0 to 0.5
0 to 0.2
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0.2 to 0.7
0
Silicon (Si), % 0 to 0.4
0
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0