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7050 Aluminum vs. C70260 Copper

7050 aluminum belongs to the aluminum alloys classification, while C70260 copper belongs to the copper 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 7050 aluminum and the bottom bar is C70260 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
120
Elongation at Break, % 2.2 to 12
9.5 to 19
Poisson's Ratio 0.32
0.34
Shear Modulus, GPa 26
44
Shear Strength, MPa 280 to 330
320 to 450
Tensile Strength: Ultimate (UTS), MPa 490 to 570
520 to 760
Tensile Strength: Yield (Proof), MPa 390 to 500
410 to 650

Thermal Properties

Latent Heat of Fusion, J/g 370
220
Maximum Temperature: Mechanical, °C 190
200
Melting Completion (Liquidus), °C 630
1060
Melting Onset (Solidus), °C 490
1040
Specific Heat Capacity, J/kg-K 860
390
Thermal Conductivity, W/m-K 140
160
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
40 to 50
Electrical Conductivity: Equal Weight (Specific), % IACS 100
40 to 51

Otherwise Unclassified Properties

Base Metal Price, % relative 10
31
Density, g/cm3 3.1
8.9
Embodied Carbon, kg CO2/kg material 8.2
2.7
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1120
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
46 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
710 to 1810
Stiffness to Weight: Axial, points 13
7.3
Stiffness to Weight: Bending, points 45
18
Strength to Weight: Axial, points 45 to 51
16 to 24
Strength to Weight: Bending, points 45 to 50
16 to 21
Thermal Diffusivity, mm2/s 54
45
Thermal Shock Resistance, points 21 to 25
18 to 27

Alloy Composition


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Aluminum (Al), % 87.3 to 92.1
0
Chromium (Cr), % 0 to 0.040
0
Copper (Cu), % 2.0 to 2.6
95.8 to 98.8
Iron (Fe), % 0 to 0.15
0
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0
Nickel (Ni), % 0
1.0 to 3.0
Phosphorus (P), % 0
0 to 0.010
Silicon (Si), % 0 to 0.12
0.2 to 0.7
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0 to 0.5