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1350 Aluminum vs. C72800 Copper-nickel

1350 aluminum belongs to the aluminum alloys classification, while C72800 copper-nickel belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1350 aluminum and the bottom bar is C72800 copper-nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 1.4 to 30
3.9 to 23
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
44
Shear Strength, MPa 44 to 110
330 to 740
Tensile Strength: Ultimate (UTS), MPa 68 to 190
520 to 1270
Tensile Strength: Yield (Proof), MPa 25 to 170
250 to 1210

Thermal Properties

Latent Heat of Fusion, J/g 400
210
Maximum Temperature: Mechanical, °C 170
200
Melting Completion (Liquidus), °C 660
1080
Melting Onset (Solidus), °C 650
920
Specific Heat Capacity, J/kg-K 900
380
Thermal Conductivity, W/m-K 230
55
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
11
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
11

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
38
Density, g/cm3 2.7
8.8
Embodied Carbon, kg CO2/kg material 8.3
4.4
Embodied Energy, MJ/kg 160
68
Embodied Water, L/kg 1200
360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
37 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
260 to 5650
Stiffness to Weight: Axial, points 14
7.4
Stiffness to Weight: Bending, points 50
19
Strength to Weight: Axial, points 7.0 to 19
17 to 40
Strength to Weight: Bending, points 14 to 27
16 to 30
Thermal Diffusivity, mm2/s 96
17
Thermal Shock Resistance, points 3.0 to 8.2
19 to 45

Alloy Composition

Aluminum (Al), % 99.5 to 100
0 to 0.1
Antimony (Sb), % 0
0 to 0.020
Bismuth (Bi), % 0
0 to 0.0010
Boron (B), % 0 to 0.050
0 to 0.0010
Chromium (Cr), % 0 to 0.010
0
Copper (Cu), % 0 to 0.050
78.3 to 82.8
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
0 to 0.5
Lead (Pb), % 0
0 to 0.0050
Magnesium (Mg), % 0
0.0050 to 0.15
Manganese (Mn), % 0 to 0.010
0.050 to 0.3
Nickel (Ni), % 0
9.5 to 10.5
Niobium (Nb), % 0
0.1 to 0.3
Phosphorus (P), % 0
0 to 0.0050
Silicon (Si), % 0 to 0.1
0 to 0.050
Sulfur (S), % 0
0 to 0.0025
Tin (Sn), % 0
7.5 to 8.5
Titanium (Ti), % 0 to 0.020
0 to 0.010
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.050
0 to 1.0
Residuals, % 0
0 to 0.3