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355.0 Aluminum vs. C62300 Bronze

355.0 aluminum belongs to the aluminum alloys classification, while C62300 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 355.0 aluminum and the bottom bar is C62300 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
110
Elongation at Break, % 1.5 to 2.6
18 to 32
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 27
43
Shear Strength, MPa 150 to 240
360 to 390
Tensile Strength: Ultimate (UTS), MPa 200 to 260
570 to 630
Tensile Strength: Yield (Proof), MPa 150 to 190
230 to 310

Thermal Properties

Latent Heat of Fusion, J/g 470
230
Maximum Temperature: Mechanical, °C 180
220
Melting Completion (Liquidus), °C 620
1050
Melting Onset (Solidus), °C 560
1040
Specific Heat Capacity, J/kg-K 890
440
Thermal Conductivity, W/m-K 150 to 170
54
Thermal Expansion, µm/m-K 22
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38 to 43
12
Electrical Conductivity: Equal Weight (Specific), % IACS 120 to 140
13

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
28
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.0
3.1
Embodied Energy, MJ/kg 150
52
Embodied Water, L/kg 1120
390

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.9
95 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 150 to 250
240 to 430
Stiffness to Weight: Axial, points 14
7.6
Stiffness to Weight: Bending, points 51
19
Strength to Weight: Axial, points 20 to 27
19 to 21
Strength to Weight: Bending, points 28 to 33
18 to 20
Thermal Diffusivity, mm2/s 60 to 69
15
Thermal Shock Resistance, points 9.1 to 12
20 to 22

Alloy Composition


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Aluminum (Al), % 90.3 to 94.1
8.5 to 10
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 1.0 to 1.5
83.2 to 89.5
Iron (Fe), % 0 to 0.6
2.0 to 4.0
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.5
0 to 0.5
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 4.5 to 5.5
0 to 0.25
Tin (Sn), % 0
0 to 0.6
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0 to 0.5