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EN AC-48100 Aluminum vs. C17500 Copper

EN AC-48100 aluminum belongs to the aluminum alloys classification, while C17500 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 EN AC-48100 aluminum and the bottom bar is C17500 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 76
120
Elongation at Break, % 1.1
6.0 to 30
Fatigue Strength, MPa 120 to 130
170 to 310
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 29
45
Tensile Strength: Ultimate (UTS), MPa 240 to 330
310 to 860
Tensile Strength: Yield (Proof), MPa 190 to 300
170 to 760

Thermal Properties

Latent Heat of Fusion, J/g 640
220
Maximum Temperature: Mechanical, °C 170
220
Melting Completion (Liquidus), °C 580
1060
Melting Onset (Solidus), °C 470
1020
Specific Heat Capacity, J/kg-K 880
390
Thermal Conductivity, W/m-K 130
200
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
24 to 53
Electrical Conductivity: Equal Weight (Specific), % IACS 87
24 to 54

Otherwise Unclassified Properties

Base Metal Price, % relative 11
60
Density, g/cm3 2.8
8.9
Embodied Carbon, kg CO2/kg material 7.3
4.7
Embodied Energy, MJ/kg 130
73
Embodied Water, L/kg 940
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
30 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
120 to 2390
Stiffness to Weight: Axial, points 15
7.5
Stiffness to Weight: Bending, points 51
18
Strength to Weight: Axial, points 24 to 33
9.7 to 27
Strength to Weight: Bending, points 31 to 38
11 to 23
Thermal Diffusivity, mm2/s 55
59
Thermal Shock Resistance, points 11 to 16
11 to 29

Alloy Composition

Aluminum (Al), % 72.1 to 79.8
0 to 0.2
Beryllium (Be), % 0
0.4 to 0.7
Cobalt (Co), % 0
2.4 to 2.7
Copper (Cu), % 4.0 to 5.0
95.6 to 97.2
Iron (Fe), % 0 to 1.3
0 to 0.1
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0
Nickel (Ni), % 0 to 0.3
0
Silicon (Si), % 16 to 18
0 to 0.2
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0
0 to 0.5