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C68800 Brass vs. C63020 Bronze

Both C68800 brass and C63020 bronze are copper alloys. They have 77% of their average alloy composition in common. There are 27 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is C68800 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, % 2.0 to 36
6.8
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 41
44
Shear Strength, MPa 380 to 510
600
Tensile Strength: Ultimate (UTS), MPa 570 to 890
1020
Tensile Strength: Yield (Proof), MPa 390 to 790
740

Thermal Properties

Latent Heat of Fusion, J/g 190
230
Maximum Temperature: Mechanical, °C 160
230
Melting Completion (Liquidus), °C 960
1070
Melting Onset (Solidus), °C 950
1020
Specific Heat Capacity, J/kg-K 400
450
Thermal Conductivity, W/m-K 40
40
Thermal Expansion, µm/m-K 19
18

Otherwise Unclassified Properties

Base Metal Price, % relative 26
29
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.8
3.6
Embodied Energy, MJ/kg 48
58
Embodied Water, L/kg 350
390

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 180
63
Resilience: Unit (Modulus of Resilience), kJ/m3 710 to 2860
2320
Stiffness to Weight: Axial, points 7.3
8.0
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 19 to 30
34
Strength to Weight: Bending, points 19 to 25
27
Thermal Diffusivity, mm2/s 12
11
Thermal Shock Resistance, points 19 to 30
35

Alloy Composition

Aluminum (Al), % 3.0 to 3.8
10 to 11
Chromium (Cr), % 0
0 to 0.050
Cobalt (Co), % 0.25 to 0.55
0 to 0.2
Copper (Cu), % 70.8 to 75.5
74.7 to 81.8
Iron (Fe), % 0 to 0.2
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
4.2 to 6.0
Tin (Sn), % 0
0 to 0.25
Zinc (Zn), % 21.3 to 24.1
0 to 0.3
Residuals, % 0
0 to 0.5