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C66200 Brass vs. C61400 Bronze

Both C66200 brass and C61400 bronze are copper alloys. They have 90% of their average alloy composition in common.

For each property being compared, the top bar is C66200 brass and the bottom bar is C61400 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 8.0 to 15
34 to 40
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 42
43
Shear Strength, MPa 270 to 300
370 to 380
Tensile Strength: Ultimate (UTS), MPa 450 to 520
540 to 570
Tensile Strength: Yield (Proof), MPa 410 to 480
220 to 270

Thermal Properties

Latent Heat of Fusion, J/g 200
220
Maximum Temperature: Mechanical, °C 180
220
Melting Completion (Liquidus), °C 1070
1050
Melting Onset (Solidus), °C 1030
1040
Specific Heat Capacity, J/kg-K 390
420
Thermal Conductivity, W/m-K 150
67
Thermal Expansion, µm/m-K 18
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
14
Electrical Conductivity: Equal Weight (Specific), % IACS 36
15

Otherwise Unclassified Properties

Base Metal Price, % relative 29
28
Density, g/cm3 8.7
8.5
Embodied Carbon, kg CO2/kg material 2.7
3.0
Embodied Energy, MJ/kg 43
48
Embodied Water, L/kg 320
360

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
160 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
210 to 310
Stiffness to Weight: Axial, points 7.2
7.5
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 14 to 17
18 to 19
Strength to Weight: Bending, points 15 to 16
17 to 18
Thermal Diffusivity, mm2/s 45
19
Thermal Shock Resistance, points 16 to 18
18 to 20

Alloy Composition


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Aluminum (Al), % 0
6.0 to 8.0
Copper (Cu), % 86.6 to 91
86 to 92.5
Iron (Fe), % 0 to 0.050
1.5 to 3.5
Lead (Pb), % 0 to 0.050
0 to 0.010
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0.3 to 1.0
0
Phosphorus (P), % 0.050 to 0.2
0 to 0.015
Tin (Sn), % 0.2 to 0.7
0
Zinc (Zn), % 6.5 to 12.9
0 to 1.0
Residuals, % 0 to 0.5
0 to 0.5