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C66200 Brass vs. C61900 Bronze

Both C66200 brass and C61900 bronze are copper alloys. They have 87% of their average alloy composition in common.

For each property being compared, the top bar is C66200 brass and the bottom bar is C61900 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
110
Elongation at Break, % 8.0 to 15
21 to 32
Poisson's Ratio 0.33
0.34
Shear Modulus, GPa 42
43
Shear Strength, MPa 270 to 300
370 to 410
Tensile Strength: Ultimate (UTS), MPa 450 to 520
570 to 650
Tensile Strength: Yield (Proof), MPa 410 to 480
230 to 310

Thermal Properties

Latent Heat of Fusion, J/g 200
230
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
440
Thermal Conductivity, W/m-K 150
79
Thermal Expansion, µm/m-K 18
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
11
Electrical Conductivity: Equal Weight (Specific), % IACS 36
11

Otherwise Unclassified Properties

Base Metal Price, % relative 29
28
Density, g/cm3 8.7
8.3
Embodied Carbon, kg CO2/kg material 2.7
3.1
Embodied Energy, MJ/kg 43
51
Embodied Water, L/kg 320
380

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 40 to 66
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 760 to 1030
230 to 430
Stiffness to Weight: Axial, points 7.2
7.6
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 14 to 17
19 to 22
Strength to Weight: Bending, points 15 to 16
18 to 20
Thermal Diffusivity, mm2/s 45
22
Thermal Shock Resistance, points 16 to 18
20 to 23

Alloy Composition

Aluminum (Al), % 0
8.5 to 10
Copper (Cu), % 86.6 to 91
83.6 to 88.5
Iron (Fe), % 0 to 0.050
3.0 to 4.5
Lead (Pb), % 0 to 0.050
0 to 0.020
Nickel (Ni), % 0.3 to 1.0
0
Phosphorus (P), % 0.050 to 0.2
0
Tin (Sn), % 0.2 to 0.7
0 to 0.6
Zinc (Zn), % 6.5 to 12.9
0 to 0.8
Residuals, % 0
0 to 0.5