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333.0 Aluminum vs. C66300 Brass

333.0 aluminum belongs to the aluminum alloys classification, while C66300 brass belongs to the copper 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 333.0 aluminum and the bottom bar is C66300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
110
Elongation at Break, % 1.0 to 2.0
2.3 to 22
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 28
42
Shear Strength, MPa 190 to 230
290 to 470
Tensile Strength: Ultimate (UTS), MPa 230 to 280
460 to 810
Tensile Strength: Yield (Proof), MPa 130 to 210
400 to 800

Thermal Properties

Latent Heat of Fusion, J/g 520
200
Maximum Temperature: Mechanical, °C 170
180
Melting Completion (Liquidus), °C 590
1050
Melting Onset (Solidus), °C 530
1000
Specific Heat Capacity, J/kg-K 880
380
Thermal Conductivity, W/m-K 100 to 140
110
Thermal Expansion, µm/m-K 21
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26 to 35
25
Electrical Conductivity: Equal Weight (Specific), % IACS 83 to 110
26

Otherwise Unclassified Properties

Base Metal Price, % relative 10
29
Density, g/cm3 2.8
8.6
Embodied Carbon, kg CO2/kg material 7.6
2.8
Embodied Energy, MJ/kg 140
46
Embodied Water, L/kg 1040
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.1 to 4.6
17 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 290
710 to 2850
Stiffness to Weight: Axial, points 14
7.2
Stiffness to Weight: Bending, points 49
19
Strength to Weight: Axial, points 22 to 27
15 to 26
Strength to Weight: Bending, points 29 to 34
15 to 22
Thermal Diffusivity, mm2/s 42 to 57
32
Thermal Shock Resistance, points 11 to 13
16 to 28

Alloy Composition

Aluminum (Al), % 81.8 to 89
0
Cobalt (Co), % 0
0 to 0.2
Copper (Cu), % 3.0 to 4.0
84.5 to 87.5
Iron (Fe), % 0 to 1.0
1.4 to 2.4
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.050 to 0.5
0
Manganese (Mn), % 0 to 0.5
0
Nickel (Ni), % 0 to 0.5
0
Phosphorus (P), % 0
0 to 0.35
Silicon (Si), % 8.0 to 10
0
Tin (Sn), % 0
1.5 to 3.0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
6.0 to 12.8
Residuals, % 0
0 to 0.5