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C37100 Brass vs. 6063 Aluminum

C37100 brass belongs to the copper alloys classification, while 6063 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 C37100 brass and the bottom bar is 6063 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
68
Elongation at Break, % 8.0 to 40
7.3 to 21
Poisson's Ratio 0.31
0.33
Shear Modulus, GPa 40
26
Shear Strength, MPa 260 to 300
70 to 190
Tensile Strength: Ultimate (UTS), MPa 370 to 520
110 to 300
Tensile Strength: Yield (Proof), MPa 150 to 390
49 to 270

Thermal Properties

Latent Heat of Fusion, J/g 170
400
Maximum Temperature: Mechanical, °C 120
160
Melting Completion (Liquidus), °C 900
650
Melting Onset (Solidus), °C 890
620
Specific Heat Capacity, J/kg-K 380
900
Thermal Conductivity, W/m-K 120
190 to 220
Thermal Expansion, µm/m-K 21
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
49 to 58
Electrical Conductivity: Equal Weight (Specific), % IACS 30
160 to 190

Otherwise Unclassified Properties

Base Metal Price, % relative 23
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.3
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 320
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 38 to 120
13 to 27
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 750
18 to 540
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 20
50
Strength to Weight: Axial, points 13 to 18
11 to 31
Strength to Weight: Bending, points 14 to 18
18 to 37
Thermal Diffusivity, mm2/s 39
79 to 89
Thermal Shock Resistance, points 12 to 17
4.8 to 13

Alloy Composition

Aluminum (Al), % 0
97.5 to 99.4
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 58 to 62
0 to 0.1
Iron (Fe), % 0 to 0.15
0 to 0.35
Lead (Pb), % 0.6 to 1.2
0
Magnesium (Mg), % 0
0.45 to 0.9
Manganese (Mn), % 0
0 to 0.1
Silicon (Si), % 0
0.2 to 0.6
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 36.3 to 41.4
0 to 0.1
Residuals, % 0
0 to 0.15