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C19800 Copper vs. 333.0 Aluminum

C19800 copper belongs to the copper alloys classification, while 333.0 aluminum belongs to the aluminum alloys. There are 29 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 C19800 copper and the bottom bar is 333.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
73
Elongation at Break, % 9.0 to 12
1.0 to 2.0
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 43
28
Shear Strength, MPa 260 to 330
190 to 230
Tensile Strength: Ultimate (UTS), MPa 430 to 550
230 to 280
Tensile Strength: Yield (Proof), MPa 420 to 550
130 to 210

Thermal Properties

Latent Heat of Fusion, J/g 210
520
Maximum Temperature: Mechanical, °C 200
170
Melting Completion (Liquidus), °C 1070
590
Melting Onset (Solidus), °C 1050
530
Specific Heat Capacity, J/kg-K 390
880
Thermal Conductivity, W/m-K 260
100 to 140
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61
26 to 35
Electrical Conductivity: Equal Weight (Specific), % IACS 62
83 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 30
10
Density, g/cm3 8.9
2.8
Embodied Carbon, kg CO2/kg material 2.8
7.6
Embodied Energy, MJ/kg 43
140
Embodied Water, L/kg 320
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 49 to 52
2.1 to 4.6
Resilience: Unit (Modulus of Resilience), kJ/m3 770 to 1320
120 to 290
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 18
49
Strength to Weight: Axial, points 14 to 17
22 to 27
Strength to Weight: Bending, points 14 to 17
29 to 34
Thermal Diffusivity, mm2/s 75
42 to 57
Thermal Shock Resistance, points 15 to 20
11 to 13

Alloy Composition

Aluminum (Al), % 0
81.8 to 89
Copper (Cu), % 95.7 to 99.47
3.0 to 4.0
Iron (Fe), % 0.020 to 0.5
0 to 1.0
Magnesium (Mg), % 0.1 to 1.0
0.050 to 0.5
Manganese (Mn), % 0
0 to 0.5
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0.010 to 0.1
0
Silicon (Si), % 0
8.0 to 10
Tin (Sn), % 0.1 to 1.0
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0.3 to 1.5
0 to 1.0
Residuals, % 0
0 to 0.5