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242.0 Aluminum vs. C16500 Copper

242.0 aluminum belongs to the aluminum alloys classification, while C16500 copper belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 242.0 aluminum and the bottom bar is C16500 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
110
Elongation at Break, % 0.5 to 1.5
1.5 to 53
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 27
43
Shear Strength, MPa 150 to 240
200 to 310
Tensile Strength: Ultimate (UTS), MPa 180 to 290
280 to 530
Tensile Strength: Yield (Proof), MPa 120 to 220
97 to 520

Thermal Properties

Latent Heat of Fusion, J/g 390
210
Maximum Temperature: Mechanical, °C 210
340
Melting Completion (Liquidus), °C 640
1070
Melting Onset (Solidus), °C 530
1010
Specific Heat Capacity, J/kg-K 870
380
Thermal Conductivity, W/m-K 130 to 170
250
Thermal Expansion, µm/m-K 22
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 44
60
Electrical Conductivity: Equal Weight (Specific), % IACS 96 to 130
61

Otherwise Unclassified Properties

Base Metal Price, % relative 12
31
Density, g/cm3 3.1
8.9
Embodied Carbon, kg CO2/kg material 8.3
2.6
Embodied Energy, MJ/kg 150
42
Embodied Water, L/kg 1130
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 3.4
7.8 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 340
41 to 1160
Stiffness to Weight: Axial, points 13
7.1
Stiffness to Weight: Bending, points 45
18
Strength to Weight: Axial, points 16 to 26
8.6 to 17
Strength to Weight: Bending, points 23 to 32
11 to 16
Thermal Diffusivity, mm2/s 50 to 62
74
Thermal Shock Resistance, points 8.0 to 13
9.8 to 19

Alloy Composition


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Aluminum (Al), % 88.4 to 93.6
0
Cadmium (Cd), % 0
0.6 to 1.0
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 3.5 to 4.5
97.8 to 98.9
Iron (Fe), % 0 to 1.0
0 to 0.020
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.35
0
Nickel (Ni), % 1.7 to 2.3
0
Silicon (Si), % 0 to 0.7
0
Tin (Sn), % 0
0.5 to 0.7
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0 to 0.5