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C70260 Copper vs. 7475 Aluminum

C70260 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 C70260 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, % 9.5 to 19
10 to 12
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 44
26
Shear Strength, MPa 320 to 450
320 to 350
Tensile Strength: Ultimate (UTS), MPa 520 to 760
530 to 590
Tensile Strength: Yield (Proof), MPa 410 to 650
440 to 520

Thermal Properties

Latent Heat of Fusion, J/g 220
380
Maximum Temperature: Mechanical, °C 200
180
Melting Completion (Liquidus), °C 1060
640
Melting Onset (Solidus), °C 1040
480
Specific Heat Capacity, J/kg-K 390
870
Thermal Conductivity, W/m-K 160
140 to 160
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40 to 50
33 to 42
Electrical Conductivity: Equal Weight (Specific), % IACS 40 to 51
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 43
150
Embodied Water, L/kg 310
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 46 to 140
53 to 68
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 1810
1390 to 1920
Stiffness to Weight: Axial, points 7.3
13
Stiffness to Weight: Bending, points 18
46
Strength to Weight: Axial, points 16 to 24
49 to 55
Strength to Weight: Bending, points 16 to 21
48 to 52
Thermal Diffusivity, mm2/s 45
53 to 63
Thermal Shock Resistance, points 18 to 27
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), % 95.8 to 98.8
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), % 1.0 to 3.0
0
Phosphorus (P), % 0 to 0.010
0
Silicon (Si), % 0.2 to 0.7
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