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C36200 Brass vs. 5082 Aluminum

C36200 brass belongs to the copper alloys classification, while 5082 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 C36200 brass and the bottom bar is 5082 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
67
Elongation at Break, % 20 to 53
1.1
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 39
25
Shear Strength, MPa 210 to 240
210 to 230
Tensile Strength: Ultimate (UTS), MPa 340 to 420
380 to 400
Tensile Strength: Yield (Proof), MPa 130 to 360
300 to 340

Thermal Properties

Latent Heat of Fusion, J/g 170
400
Maximum Temperature: Mechanical, °C 120
180
Melting Completion (Liquidus), °C 900
640
Melting Onset (Solidus), °C 890
560
Specific Heat Capacity, J/kg-K 380
910
Thermal Conductivity, W/m-K 120
130
Thermal Expansion, µm/m-K 21
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
32
Electrical Conductivity: Equal Weight (Specific), % IACS 28
110

Otherwise Unclassified Properties

Base Metal Price, % relative 23
9.5
Density, g/cm3 8.2
2.7
Embodied Carbon, kg CO2/kg material 2.6
8.9
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 320
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 140
4.0 to 4.3
Resilience: Unit (Modulus of Resilience), kJ/m3 89 to 630
670 to 870
Stiffness to Weight: Axial, points 6.9
14
Stiffness to Weight: Bending, points 19
51
Strength to Weight: Axial, points 11 to 14
39 to 41
Strength to Weight: Bending, points 13 to 15
43 to 45
Thermal Diffusivity, mm2/s 37
54
Thermal Shock Resistance, points 11 to 14
17 to 18

Alloy Composition

Aluminum (Al), % 0
93.5 to 96
Chromium (Cr), % 0
0 to 0.15
Copper (Cu), % 60 to 63
0 to 0.15
Iron (Fe), % 0 to 0.15
0 to 0.35
Lead (Pb), % 3.5 to 4.5
0
Magnesium (Mg), % 0
4.0 to 5.0
Manganese (Mn), % 0
0 to 0.15
Silicon (Si), % 0
0 to 0.2
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 32.4 to 36.5
0 to 0.25
Residuals, % 0
0 to 0.15