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C66200 Brass vs. C63020 Bronze

Both C66200 brass and C63020 bronze are copper alloys. They have 79% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is C66200 brass and the bottom bar is C63020 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.0 to 15
6.8
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 42
44
Shear Strength, MPa 270 to 300
600
Tensile Strength: Ultimate (UTS), MPa 450 to 520
1020
Tensile Strength: Yield (Proof), MPa 410 to 480
740

Thermal Properties

Latent Heat of Fusion, J/g 200
230
Maximum Temperature: Mechanical, °C 180
230
Melting Completion (Liquidus), °C 1070
1070
Melting Onset (Solidus), °C 1030
1020
Specific Heat Capacity, J/kg-K 390
450
Thermal Conductivity, W/m-K 150
40
Thermal Expansion, µm/m-K 18
18

Otherwise Unclassified Properties

Base Metal Price, % relative 29
29
Density, g/cm3 8.7
8.2
Embodied Carbon, kg CO2/kg material 2.7
3.6
Embodied Energy, MJ/kg 43
58
Embodied Water, L/kg 320
390

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
63
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
2320
Stiffness to Weight: Axial, points 7.2
8.0
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 14 to 17
34
Strength to Weight: Bending, points 15 to 16
27
Thermal Diffusivity, mm2/s 45
11
Thermal Shock Resistance, points 16 to 18
35

Alloy Composition

Aluminum (Al), % 0
10 to 11
Chromium (Cr), % 0
0 to 0.050
Cobalt (Co), % 0
0 to 0.2
Copper (Cu), % 86.6 to 91
74.7 to 81.8
Iron (Fe), % 0 to 0.050
4.0 to 5.5
Lead (Pb), % 0 to 0.050
0 to 0.030
Manganese (Mn), % 0
0 to 1.5
Nickel (Ni), % 0.3 to 1.0
4.2 to 6.0
Phosphorus (P), % 0.050 to 0.2
0
Tin (Sn), % 0.2 to 0.7
0 to 0.25
Zinc (Zn), % 6.5 to 12.9
0 to 0.3
Residuals, % 0
0 to 0.5