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C85400 Brass vs. C61900 Bronze

Both C85400 brass and C61900 bronze 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 C85400 brass and the bottom bar is C61900 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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