5456 Aluminum vs. C17000 Copper
5456 aluminum belongs to the aluminum alloys classification, while C17000 copper belongs to the copper alloys. There are 28 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 5456 aluminum and the bottom bar is C17000 copper.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
120 |
Elongation at Break, % | 11 to 18 | |
1.1 to 31 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 26 | |
45 |
Shear Strength, MPa | 190 to 210 | |
320 to 750 |
Tensile Strength: Ultimate (UTS), MPa | 320 to 340 | |
490 to 1310 |
Tensile Strength: Yield (Proof), MPa | 150 to 250 | |
160 to 1140 |
Thermal Properties
Latent Heat of Fusion, J/g | 390 | |
230 |
Maximum Temperature: Mechanical, °C | 190 | |
270 |
Melting Completion (Liquidus), °C | 640 | |
980 |
Melting Onset (Solidus), °C | 570 | |
870 |
Specific Heat Capacity, J/kg-K | 900 | |
390 |
Thermal Conductivity, W/m-K | 120 | |
110 |
Thermal Expansion, µm/m-K | 24 | |
17 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 29 | |
22 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 97 | |
22 |
Otherwise Unclassified Properties
Density, g/cm3 | 2.7 | |
8.8 |
Embodied Carbon, kg CO2/kg material | 9.0 | |
8.7 |
Embodied Energy, MJ/kg | 150 | |
140 |
Embodied Water, L/kg | 1170 | |
310 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 33 to 46 | |
4.2 to 390 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 to 470 | |
110 to 5420 |
Stiffness to Weight: Axial, points | 14 | |
7.6 |
Stiffness to Weight: Bending, points | 50 | |
19 |
Strength to Weight: Axial, points | 33 to 35 | |
15 to 41 |
Strength to Weight: Bending, points | 38 to 40 | |
16 to 30 |
Thermal Diffusivity, mm2/s | 48 | |
32 |
Thermal Shock Resistance, points | 14 to 15 | |
17 to 45 |
Alloy Composition
Aluminum (Al), % | 92 to 94.8 | |
0 to 0.2 |
Beryllium (Be), % | 0 | |
1.6 to 1.8 |
Chromium (Cr), % | 0.050 to 0.2 | |
0 |
Copper (Cu), % | 0 to 0.1 | |
96.3 to 98.2 |
Iron (Fe), % | 0 to 0.4 | |
0 to 0.4 |
Magnesium (Mg), % | 4.7 to 5.5 | |
0 |
Manganese (Mn), % | 0.5 to 1.0 | |
0 |
Nickel (Ni), % | 0 | |
0.2 to 0.6 |
Silicon (Si), % | 0 to 0.25 | |
0 to 0.2 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 0 to 0.25 | |
0 |
Residuals, % | 0 | |
0 to 0.5 |