MakeItFrom.com
Menu (ESC)

6262A Aluminum vs. C19700 Copper

6262A aluminum belongs to the aluminum alloys classification, while C19700 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 6262A aluminum and the bottom bar is C19700 copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
120
Elongation at Break, % 4.5 to 11
2.4 to 13
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 190 to 240
240 to 300
Tensile Strength: Ultimate (UTS), MPa 310 to 410
400 to 530
Tensile Strength: Yield (Proof), MPa 270 to 370
330 to 520

Thermal Properties

Latent Heat of Fusion, J/g 400
210
Maximum Temperature: Mechanical, °C 160
200
Melting Completion (Liquidus), °C 640
1090
Melting Onset (Solidus), °C 580
1040
Specific Heat Capacity, J/kg-K 890
390
Thermal Conductivity, W/m-K 170
250
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 45
86 to 88
Electrical Conductivity: Equal Weight (Specific), % IACS 140
87 to 89

Otherwise Unclassified Properties

Base Metal Price, % relative 11
30
Density, g/cm3 2.8
8.9
Embodied Carbon, kg CO2/kg material 8.4
2.6
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1190
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 34
12 to 49
Resilience: Unit (Modulus of Resilience), kJ/m3 540 to 1000
460 to 1160
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 49
18
Strength to Weight: Axial, points 31 to 41
12 to 16
Strength to Weight: Bending, points 36 to 44
14 to 16
Thermal Diffusivity, mm2/s 67
73
Thermal Shock Resistance, points 14 to 18
14 to 19

Alloy Composition

Aluminum (Al), % 94.2 to 97.8
0
Bismuth (Bi), % 0.4 to 0.9
0
Chromium (Cr), % 0.040 to 0.14
0
Cobalt (Co), % 0
0 to 0.050
Copper (Cu), % 0.15 to 0.4
97.4 to 99.59
Iron (Fe), % 0 to 0.7
0.3 to 1.2
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.8 to 1.2
0.010 to 0.2
Manganese (Mn), % 0 to 0.15
0 to 0.050
Nickel (Ni), % 0
0 to 0.050
Phosphorus (P), % 0
0.1 to 0.4
Silicon (Si), % 0.4 to 0.8
0
Tin (Sn), % 0.4 to 1.0
0 to 0.2
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.25
0 to 0.2
Residuals, % 0
0 to 0.2