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C70260 Copper vs. 7005 Aluminum

C70260 copper belongs to the copper alloys classification, while 7005 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 C70260 copper and the bottom bar is 7005 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 9.5 to 19
10 to 20
Poisson's Ratio 0.34
0.33
Shear Modulus, GPa 44
26
Shear Strength, MPa 320 to 450
120 to 230
Tensile Strength: Ultimate (UTS), MPa 520 to 760
200 to 400
Tensile Strength: Yield (Proof), MPa 410 to 650
95 to 350

Thermal Properties

Latent Heat of Fusion, J/g 220
380
Maximum Temperature: Mechanical, °C 200
200
Melting Completion (Liquidus), °C 1060
640
Melting Onset (Solidus), °C 1040
610
Specific Heat Capacity, J/kg-K 390
880
Thermal Conductivity, W/m-K 160
140 to 170
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40 to 50
35 to 43
Electrical Conductivity: Equal Weight (Specific), % IACS 40 to 51
110 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 31
9.5
Density, g/cm3 8.9
2.9
Embodied Carbon, kg CO2/kg material 2.7
8.3
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 310
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 46 to 140
32 to 57
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 1810
65 to 850
Stiffness to Weight: Axial, points 7.3
13
Stiffness to Weight: Bending, points 18
47
Strength to Weight: Axial, points 16 to 24
19 to 38
Strength to Weight: Bending, points 16 to 21
26 to 41
Thermal Diffusivity, mm2/s 45
54 to 65
Thermal Shock Resistance, points 18 to 27
8.7 to 18

Alloy Composition


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Aluminum (Al), % 0
91 to 94.7
Chromium (Cr), % 0
0.060 to 0.2
Copper (Cu), % 95.8 to 98.8
0 to 0.1
Iron (Fe), % 0
0 to 0.4
Magnesium (Mg), % 0
1.0 to 1.8
Manganese (Mn), % 0
0.2 to 0.7
Nickel (Ni), % 1.0 to 3.0
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0.2 to 0.7
0 to 0.35
Titanium (Ti), % 0
0.010 to 0.060
Zinc (Zn), % 0
4.0 to 5.0
Zirconium (Zr), % 0
0.080 to 0.2
Residuals, % 0 to 0.5
0 to 0.15