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6005A Aluminum vs. C65400 Bronze

6005A aluminum belongs to the aluminum alloys classification, while C65400 bronze belongs to the copper alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 6005A aluminum and the bottom bar is C65400 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
110
Elongation at Break, % 8.6 to 17
2.6 to 47
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 26
43
Shear Strength, MPa 120 to 180
350 to 530
Tensile Strength: Ultimate (UTS), MPa 190 to 300
500 to 1060
Tensile Strength: Yield (Proof), MPa 100 to 270
170 to 910

Thermal Properties

Latent Heat of Fusion, J/g 410
260
Maximum Temperature: Mechanical, °C 170
200
Melting Completion (Liquidus), °C 650
1020
Melting Onset (Solidus), °C 600
960
Specific Heat Capacity, J/kg-K 900
400
Thermal Conductivity, W/m-K 180 to 190
36
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 47 to 50
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 150 to 170
7.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
31
Density, g/cm3 2.7
8.7
Embodied Carbon, kg CO2/kg material 8.3
2.8
Embodied Energy, MJ/kg 150
45
Embodied Water, L/kg 1180
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 29
10 to 480
Resilience: Unit (Modulus of Resilience), kJ/m3 76 to 530
130 to 3640
Stiffness to Weight: Axial, points 14
7.3
Stiffness to Weight: Bending, points 50
19
Strength to Weight: Axial, points 20 to 30
16 to 34
Strength to Weight: Bending, points 27 to 36
16 to 27
Thermal Diffusivity, mm2/s 72 to 79
10
Thermal Shock Resistance, points 8.6 to 13
18 to 39

Alloy Composition

Aluminum (Al), % 96.5 to 99.1
0
Chromium (Cr), % 0 to 0.3
0.010 to 0.12
Copper (Cu), % 0 to 0.3
93.8 to 96.1
Iron (Fe), % 0 to 0.35
0
Lead (Pb), % 0
0 to 0.050
Magnesium (Mg), % 0.4 to 0.7
0
Manganese (Mn), % 0 to 0.5
0
Silicon (Si), % 0.5 to 0.9
2.7 to 3.4
Tin (Sn), % 0
1.2 to 1.9
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0 to 0.5
Residuals, % 0
0 to 0.2