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C23000 Brass vs. A360.0 Aluminum

C23000 brass belongs to the copper alloys classification, while A360.0 aluminum belongs to the aluminum 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 C23000 brass and the bottom bar is A360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
72
Elongation at Break, % 2.9 to 47
1.6 to 5.0
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 42
27
Shear Strength, MPa 220 to 340
180
Tensile Strength: Ultimate (UTS), MPa 280 to 590
180 to 320
Tensile Strength: Yield (Proof), MPa 83 to 480
170 to 260

Thermal Properties

Latent Heat of Fusion, J/g 190
530
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 1030
680
Melting Onset (Solidus), °C 990
590
Specific Heat Capacity, J/kg-K 390
900
Thermal Conductivity, W/m-K 160
110
Thermal Expansion, µm/m-K 19
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
30
Electrical Conductivity: Equal Weight (Specific), % IACS 39
100

Otherwise Unclassified Properties

Base Metal Price, % relative 28
9.5
Calomel Potential, mV -350
-700
Density, g/cm3 8.6
2.6
Embodied Carbon, kg CO2/kg material 2.6
7.8
Embodied Energy, MJ/kg 43
150
Embodied Water, L/kg 310
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.2 to 260
4.6 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 31 to 1040
190 to 470
Stiffness to Weight: Axial, points 7.2
15
Stiffness to Weight: Bending, points 19
53
Strength to Weight: Axial, points 8.9 to 19
19 to 34
Strength to Weight: Bending, points 11 to 18
27 to 39
Thermal Diffusivity, mm2/s 48
48
Thermal Shock Resistance, points 9.4 to 20
8.5 to 15

Alloy Composition

Aluminum (Al), % 0
85.8 to 90.6
Copper (Cu), % 84 to 86
0 to 0.6
Iron (Fe), % 0 to 0.050
0 to 1.3
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0
0 to 0.35
Nickel (Ni), % 0
0 to 0.5
Silicon (Si), % 0
9.0 to 10
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 13.7 to 16
0 to 0.5
Residuals, % 0
0 to 0.25