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1350 Aluminum vs. C19010 Copper

1350 aluminum belongs to the aluminum alloys classification, while C19010 copper belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 C19010 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 1.4 to 30
2.4 to 22
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 44 to 110
210 to 360
Tensile Strength: Ultimate (UTS), MPa 68 to 190
330 to 640
Tensile Strength: Yield (Proof), MPa 25 to 170
260 to 620

Thermal Properties

Latent Heat of Fusion, J/g 400
210
Maximum Temperature: Mechanical, °C 170
200
Melting Completion (Liquidus), °C 660
1060
Melting Onset (Solidus), °C 650
1010
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 230
260
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 61 to 62
48 to 63
Electrical Conductivity: Equal Weight (Specific), % IACS 200 to 210
48 to 63

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.9
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 160
42
Embodied Water, L/kg 1200
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 0.77 to 54
7.3 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 4.4 to 200
290 to 1680
Stiffness to Weight: Axial, points 14
7.3
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 7.0 to 19
10 to 20
Strength to Weight: Bending, points 14 to 27
12 to 18
Thermal Diffusivity, mm2/s 96
75
Thermal Shock Resistance, points 3.0 to 8.2
12 to 23

Alloy Composition

Aluminum (Al), % 99.5 to 100
0
Boron (B), % 0 to 0.050
0
Chromium (Cr), % 0 to 0.010
0
Copper (Cu), % 0 to 0.050
97.3 to 99.04
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.4
0
Manganese (Mn), % 0 to 0.010
0
Nickel (Ni), % 0
0.8 to 1.8
Phosphorus (P), % 0
0.010 to 0.050
Silicon (Si), % 0 to 0.1
0.15 to 0.35
Titanium (Ti), % 0 to 0.020
0
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0
0 to 0.5