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6063 Aluminum vs. C33500 Brass

6063 aluminum belongs to the aluminum alloys classification, while C33500 brass belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 6063 aluminum and the bottom bar is C33500 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
100
Elongation at Break, % 7.3 to 21
3.0 to 28
Poisson's Ratio 0.33
0.31
Shear Modulus, GPa 26
40
Shear Strength, MPa 70 to 190
220 to 360
Tensile Strength: Ultimate (UTS), MPa 110 to 300
340 to 650
Tensile Strength: Yield (Proof), MPa 49 to 270
120 to 420

Thermal Properties

Latent Heat of Fusion, J/g 400
170
Maximum Temperature: Mechanical, °C 160
120
Melting Completion (Liquidus), °C 650
930
Melting Onset (Solidus), °C 620
900
Specific Heat Capacity, J/kg-K 900
390
Thermal Conductivity, W/m-K 190 to 220
120
Thermal Expansion, µm/m-K 23
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 49 to 58
26
Electrical Conductivity: Equal Weight (Specific), % IACS 160 to 190
29

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
24
Density, g/cm3 2.7
8.1
Embodied Carbon, kg CO2/kg material 8.3
2.7
Embodied Energy, MJ/kg 150
45
Embodied Water, L/kg 1190
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 27
8.0 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 540
69 to 860
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 50
19
Strength to Weight: Axial, points 11 to 31
12 to 22
Strength to Weight: Bending, points 18 to 37
13 to 21
Thermal Diffusivity, mm2/s 79 to 89
37
Thermal Shock Resistance, points 4.8 to 13
11 to 22

Alloy Composition

Aluminum (Al), % 97.5 to 99.4
0
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0 to 0.1
62 to 65
Iron (Fe), % 0 to 0.35
0 to 0.1
Lead (Pb), % 0
0.25 to 0.7
Magnesium (Mg), % 0.45 to 0.9
0
Manganese (Mn), % 0 to 0.1
0
Silicon (Si), % 0.2 to 0.6
0
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.1
33.8 to 37.8
Residuals, % 0
0 to 0.4