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7003 Aluminum vs. C71520 Copper-nickel

7003 aluminum belongs to the aluminum alloys classification, while C71520 copper-nickel belongs to the copper 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 7003 aluminum and the bottom bar is C71520 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
140
Elongation at Break, % 11
10 to 45
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 26
51
Shear Strength, MPa 210 to 230
250 to 340
Tensile Strength: Ultimate (UTS), MPa 350 to 390
370 to 570
Tensile Strength: Yield (Proof), MPa 300 to 310
140 to 430

Thermal Properties

Latent Heat of Fusion, J/g 380
230
Maximum Temperature: Mechanical, °C 200
260
Melting Completion (Liquidus), °C 630
1170
Melting Onset (Solidus), °C 510
1120
Specific Heat Capacity, J/kg-K 870
400
Thermal Conductivity, W/m-K 150
32
Thermal Expansion, µm/m-K 24
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
5.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
5.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
40
Density, g/cm3 2.9
8.9
Embodied Carbon, kg CO2/kg material 8.1
5.0
Embodied Energy, MJ/kg 150
73
Embodied Water, L/kg 1140
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 37 to 41
54 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 710
67 to 680
Stiffness to Weight: Axial, points 13
8.6
Stiffness to Weight: Bending, points 47
19
Strength to Weight: Axial, points 33 to 37
12 to 18
Strength to Weight: Bending, points 37 to 40
13 to 17
Thermal Diffusivity, mm2/s 59
8.9
Thermal Shock Resistance, points 15 to 17
12 to 19

Alloy Composition

Aluminum (Al), % 90.6 to 94.5
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0 to 0.2
65 to 71.6
Iron (Fe), % 0 to 0.35
0.4 to 1.0
Lead (Pb), % 0
0 to 0.020
Magnesium (Mg), % 0.5 to 1.0
0
Manganese (Mn), % 0 to 0.3
0 to 1.0
Nickel (Ni), % 0
28 to 33
Phosphorus (P), % 0
0 to 0.2
Silicon (Si), % 0 to 0.3
0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 5.0 to 6.5
0 to 0.5
Zirconium (Zr), % 0.050 to 0.25
0
Residuals, % 0
0 to 0.5