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C42200 Brass vs. 5059 Aluminum

C42200 brass belongs to the copper alloys classification, while 5059 aluminum belongs to the aluminum alloys. There are 29 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 C42200 brass and the bottom bar is 5059 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
69
Elongation at Break, % 2.0 to 46
11 to 25
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 42
26
Shear Strength, MPa 210 to 350
220 to 250
Tensile Strength: Ultimate (UTS), MPa 300 to 610
350 to 410
Tensile Strength: Yield (Proof), MPa 100 to 570
170 to 300

Thermal Properties

Latent Heat of Fusion, J/g 200
390
Maximum Temperature: Mechanical, °C 170
210
Melting Completion (Liquidus), °C 1040
650
Melting Onset (Solidus), °C 1020
510
Specific Heat Capacity, J/kg-K 380
900
Thermal Conductivity, W/m-K 130
110
Thermal Expansion, µm/m-K 18
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
29
Electrical Conductivity: Equal Weight (Specific), % IACS 32
95

Otherwise Unclassified Properties

Base Metal Price, % relative 29
9.5
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 2.7
9.1
Embodied Energy, MJ/kg 44
160
Embodied Water, L/kg 320
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 110
42 to 75
Resilience: Unit (Modulus of Resilience), kJ/m3 49 to 1460
220 to 650
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 19
50
Strength to Weight: Axial, points 9.5 to 19
36 to 42
Strength to Weight: Bending, points 11 to 18
41 to 45
Thermal Diffusivity, mm2/s 39
44
Thermal Shock Resistance, points 10 to 21
16 to 18

Alloy Composition

Aluminum (Al), % 0
89.9 to 94
Chromium (Cr), % 0
0 to 0.25
Copper (Cu), % 86 to 89
0 to 0.25
Iron (Fe), % 0 to 0.050
0 to 0.5
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0
5.0 to 6.0
Manganese (Mn), % 0
0.6 to 1.2
Phosphorus (P), % 0 to 0.35
0
Silicon (Si), % 0
0 to 0.45
Tin (Sn), % 0.8 to 1.4
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 8.7 to 13.2
0.4 to 0.9
Zirconium (Zr), % 0
0.050 to 0.25
Residuals, % 0
0 to 0.15