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C65100 Bronze vs. C85700 Brass

Both C65100 bronze and C85700 brass are copper alloys. They have 62% of their average alloy composition in common. There are 28 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 C65100 bronze and the bottom bar is C85700 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 2.4 to 50
17
Poisson's Ratio 0.34
0.31
Shear Modulus, GPa 43
40
Tensile Strength: Ultimate (UTS), MPa 280 to 560
310
Tensile Strength: Yield (Proof), MPa 95 to 440
110

Thermal Properties

Latent Heat of Fusion, J/g 230
170
Maximum Temperature: Mechanical, °C 200
120
Melting Completion (Liquidus), °C 1060
940
Melting Onset (Solidus), °C 1030
910
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 57
84
Thermal Expansion, µm/m-K 18
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
22
Electrical Conductivity: Equal Weight (Specific), % IACS 12
25

Otherwise Unclassified Properties

Base Metal Price, % relative 30
24
Density, g/cm3 8.8
8.0
Embodied Carbon, kg CO2/kg material 2.6
2.8
Embodied Energy, MJ/kg 41
47
Embodied Water, L/kg 300
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 110
41
Resilience: Unit (Modulus of Resilience), kJ/m3 39 to 820
59
Stiffness to Weight: Axial, points 7.3
7.2
Stiffness to Weight: Bending, points 18
20
Strength to Weight: Axial, points 8.7 to 18
11
Strength to Weight: Bending, points 11 to 17
13
Thermal Diffusivity, mm2/s 16
27
Thermal Shock Resistance, points 9.5 to 19
10

Alloy Composition

Aluminum (Al), % 0
0 to 0.8
Copper (Cu), % 94.5 to 99.2
58 to 64
Iron (Fe), % 0 to 0.8
0 to 0.7
Lead (Pb), % 0 to 0.050
0.8 to 1.5
Manganese (Mn), % 0 to 0.7
0
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 0.8 to 2.0
0 to 0.050
Tin (Sn), % 0
0.5 to 1.5
Zinc (Zn), % 0 to 1.5
32 to 40
Residuals, % 0
0 to 1.3