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C61900 Bronze vs. C85400 Brass

Both C61900 bronze and C85400 brass are copper alloys. They have 69% 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 C61900 bronze and the bottom bar is C85400 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
100
Elongation at Break, % 21 to 32
23
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 43
40
Tensile Strength: Ultimate (UTS), MPa 570 to 650
220
Tensile Strength: Yield (Proof), MPa 230 to 310
85

Thermal Properties

Latent Heat of Fusion, J/g 230
180
Maximum Temperature: Mechanical, °C 220
130
Melting Completion (Liquidus), °C 1050
940
Melting Onset (Solidus), °C 1040
940
Specific Heat Capacity, J/kg-K 440
380
Thermal Conductivity, W/m-K 79
89
Thermal Expansion, µm/m-K 18
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
20
Electrical Conductivity: Equal Weight (Specific), % IACS 11
22

Otherwise Unclassified Properties

Base Metal Price, % relative 28
25
Density, g/cm3 8.3
8.3
Embodied Carbon, kg CO2/kg material 3.1
2.8
Embodied Energy, MJ/kg 51
46
Embodied Water, L/kg 380
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 150
40
Resilience: Unit (Modulus of Resilience), kJ/m3 230 to 430
35
Stiffness to Weight: Axial, points 7.6
7.0
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 19 to 22
7.5
Strength to Weight: Bending, points 18 to 20
9.9
Thermal Diffusivity, mm2/s 22
28
Thermal Shock Resistance, points 20 to 23
7.6

Alloy Composition


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Aluminum (Al), % 8.5 to 10
0 to 0.35
Copper (Cu), % 83.6 to 88.5
65 to 70
Iron (Fe), % 3.0 to 4.5
0 to 0.7
Lead (Pb), % 0 to 0.020
1.5 to 3.8
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 0
0 to 0.050
Tin (Sn), % 0 to 0.6
0.5 to 1.5
Zinc (Zn), % 0 to 0.8
24 to 32
Residuals, % 0 to 0.5
0 to 1.1