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6005 Aluminum vs. C23000 Brass

6005 aluminum belongs to the aluminum alloys classification, while C23000 brass belongs to the copper alloys. There are 30 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 6005 aluminum and the bottom bar is C23000 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
110
Elongation at Break, % 9.5 to 17
2.9 to 47
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
42
Shear Strength, MPa 120 to 210
220 to 340
Tensile Strength: Ultimate (UTS), MPa 190 to 310
280 to 590
Tensile Strength: Yield (Proof), MPa 100 to 280
83 to 480

Thermal Properties

Latent Heat of Fusion, J/g 410
190
Maximum Temperature: Mechanical, °C 160
170
Melting Completion (Liquidus), °C 650
1030
Melting Onset (Solidus), °C 610
990
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 180 to 200
160
Thermal Expansion, µm/m-K 23
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
37
Electrical Conductivity: Equal Weight (Specific), % IACS 180
39

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
28
Calomel Potential, mV -740
-350
Density, g/cm3 2.7
8.6
Embodied Carbon, kg CO2/kg material 8.3
2.6
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1180
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 36
6.2 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 550
31 to 1040
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 51
19
Strength to Weight: Axial, points 20 to 32
8.9 to 19
Strength to Weight: Bending, points 28 to 38
11 to 18
Thermal Diffusivity, mm2/s 74 to 83
48
Thermal Shock Resistance, points 8.6 to 14
9.4 to 20

Alloy Composition

Aluminum (Al), % 97.5 to 99
0
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.1
84 to 86
Iron (Fe), % 0 to 0.35
0 to 0.050
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
0
Silicon (Si), % 0.6 to 0.9
0
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
13.7 to 16
Residuals, % 0
0 to 0.2