MakeItFrom.com
Menu (ESC)

5449 Aluminum vs. C17510 Copper

5449 aluminum belongs to the aluminum alloys classification, while C17510 copper 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 5449 aluminum and the bottom bar is C17510 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
120
Elongation at Break, % 4.0 to 17
5.4 to 37
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
44
Shear Strength, MPa 130 to 190
210 to 500
Tensile Strength: Ultimate (UTS), MPa 210 to 330
310 to 860
Tensile Strength: Yield (Proof), MPa 91 to 260
120 to 750

Thermal Properties

Latent Heat of Fusion, J/g 400
220
Maximum Temperature: Mechanical, °C 190
220
Melting Completion (Liquidus), °C 650
1070
Melting Onset (Solidus), °C 590
1030
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 140
210
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
22 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 110
23 to 54

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
49
Density, g/cm3 2.8
8.9
Embodied Carbon, kg CO2/kg material 8.5
4.2
Embodied Energy, MJ/kg 150
65
Embodied Water, L/kg 1180
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 29
39 to 92
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 480
64 to 2410
Stiffness to Weight: Axial, points 14
7.4
Stiffness to Weight: Bending, points 50
18
Strength to Weight: Axial, points 22 to 33
9.7 to 27
Strength to Weight: Bending, points 29 to 39
11 to 23
Thermal Diffusivity, mm2/s 56
60
Thermal Shock Resistance, points 9.4 to 15
11 to 30

Alloy Composition

Aluminum (Al), % 94.1 to 97.8
0 to 0.2
Beryllium (Be), % 0
0.2 to 0.6
Chromium (Cr), % 0 to 0.3
0
Cobalt (Co), % 0
0 to 0.3
Copper (Cu), % 0 to 0.3
95.9 to 98.4
Iron (Fe), % 0 to 0.7
0 to 0.1
Magnesium (Mg), % 1.6 to 2.6
0
Manganese (Mn), % 0.6 to 1.1
0
Nickel (Ni), % 0
1.4 to 2.2
Silicon (Si), % 0 to 0.4
0 to 0.2
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0
0 to 0.5