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C19010 Copper vs. 7475 Aluminum

C19010 copper belongs to the copper alloys classification, while 7475 aluminum belongs to the aluminum 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 C19010 copper and the bottom bar is 7475 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 2.4 to 22
10 to 12
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 43
26
Shear Strength, MPa 210 to 360
320 to 350
Tensile Strength: Ultimate (UTS), MPa 330 to 640
530 to 590
Tensile Strength: Yield (Proof), MPa 260 to 620
440 to 520

Thermal Properties

Latent Heat of Fusion, J/g 210
380
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1060
640
Melting Onset (Solidus), °C 1010
480
Specific Heat Capacity, J/kg-K 390
870
Thermal Conductivity, W/m-K 260
140 to 160
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 48 to 63
33 to 42
Electrical Conductivity: Equal Weight (Specific), % IACS 48 to 63
98 to 120

Otherwise Unclassified Properties

Base Metal Price, % relative 31
10
Density, g/cm3 8.9
3.0
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 42
150
Embodied Water, L/kg 310
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.3 to 140
53 to 68
Resilience: Unit (Modulus of Resilience), kJ/m3 290 to 1680
1390 to 1920
Stiffness to Weight: Axial, points 7.3
13
Stiffness to Weight: Bending, points 18
46
Strength to Weight: Axial, points 10 to 20
49 to 55
Strength to Weight: Bending, points 12 to 18
48 to 52
Thermal Diffusivity, mm2/s 75
53 to 63
Thermal Shock Resistance, points 12 to 23
23 to 26

Alloy Composition


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Aluminum (Al), % 0
88.6 to 91.6
Chromium (Cr), % 0
0.18 to 0.25
Copper (Cu), % 97.3 to 99.04
1.2 to 1.9
Iron (Fe), % 0
0 to 0.12
Magnesium (Mg), % 0
1.9 to 2.6
Manganese (Mn), % 0
0 to 0.060
Nickel (Ni), % 0.8 to 1.8
0
Phosphorus (P), % 0.010 to 0.050
0
Silicon (Si), % 0.15 to 0.35
0 to 0.1
Titanium (Ti), % 0
0 to 0.060
Zinc (Zn), % 0
5.1 to 6.2
Residuals, % 0 to 0.5
0 to 0.15