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C72150 Copper-nickel vs. 5154A Aluminum

C72150 copper-nickel belongs to the copper alloys classification, while 5154A aluminum belongs to the aluminum alloys. There are 30 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 C72150 copper-nickel and the bottom bar is 5154A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 99
58 to 100
Elastic (Young's, Tensile) Modulus, GPa 150
68
Elongation at Break, % 29
1.1 to 19
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 55
26
Shear Strength, MPa 320
140 to 210
Tensile Strength: Ultimate (UTS), MPa 490
230 to 370
Tensile Strength: Yield (Proof), MPa 210
96 to 320

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 600
190
Melting Completion (Liquidus), °C 1210
650
Melting Onset (Solidus), °C 1250
600
Specific Heat Capacity, J/kg-K 410
900
Thermal Conductivity, W/m-K 22
130
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.5
32
Electrical Conductivity: Equal Weight (Specific), % IACS 3.6
110

Otherwise Unclassified Properties

Base Metal Price, % relative 45
9.5
Density, g/cm3 8.9
2.7
Embodied Carbon, kg CO2/kg material 6.1
8.8
Embodied Energy, MJ/kg 88
150
Embodied Water, L/kg 270
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
4.0 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 150
68 to 760
Stiffness to Weight: Axial, points 9.1
14
Stiffness to Weight: Bending, points 20
51
Strength to Weight: Axial, points 15
24 to 38
Strength to Weight: Bending, points 15
31 to 43
Thermal Diffusivity, mm2/s 6.0
53
Thermal Shock Resistance, points 18
10 to 16

Alloy Composition


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Aluminum (Al), % 0
93.7 to 96.9
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 0
0 to 0.25
Copper (Cu), % 52.5 to 57
0 to 0.1
Iron (Fe), % 0 to 0.1
0 to 0.5
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
3.1 to 3.9
Manganese (Mn), % 0 to 0.050
0 to 0.5
Nickel (Ni), % 43 to 46
0
Silicon (Si), % 0 to 0.5
0 to 0.5
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0 to 0.2
0 to 0.2
Residuals, % 0 to 0.5
0 to 0.15