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C33200 Brass vs. C61900 Bronze

Both C33200 brass and C61900 bronze are copper alloys. They have 67% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.

For each property being compared, the top bar is C33200 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, % 7.0 to 60
21 to 32
Poisson's Ratio 0.31
0.34
Shear Modulus, GPa 40
43
Shear Strength, MPa 240 to 300
370 to 410
Tensile Strength: Ultimate (UTS), MPa 320 to 520
570 to 650
Tensile Strength: Yield (Proof), MPa 110 to 450
230 to 310

Thermal Properties

Latent Heat of Fusion, J/g 170
230
Maximum Temperature: Mechanical, °C 130
220
Melting Completion (Liquidus), °C 930
1050
Melting Onset (Solidus), °C 900
1040
Specific Heat Capacity, J/kg-K 380
440
Thermal Conductivity, W/m-K 120
79
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
11
Electrical Conductivity: Equal Weight (Specific), % IACS 28
11

Otherwise Unclassified Properties

Base Metal Price, % relative 24
28
Density, g/cm3 8.2
8.3
Embodied Carbon, kg CO2/kg material 2.6
3.1
Embodied Energy, MJ/kg 44
51
Embodied Water, L/kg 320
380

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 960
230 to 430
Stiffness to Weight: Axial, points 7.1
7.6
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 11 to 17
19 to 22
Strength to Weight: Bending, points 13 to 17
18 to 20
Thermal Diffusivity, mm2/s 37
22
Thermal Shock Resistance, points 11 to 17
20 to 23

Alloy Composition

Aluminum (Al), % 0
8.5 to 10
Copper (Cu), % 65 to 68
83.6 to 88.5
Iron (Fe), % 0 to 0.070
3.0 to 4.5
Lead (Pb), % 1.5 to 2.5
0 to 0.020
Tin (Sn), % 0
0 to 0.6
Zinc (Zn), % 29 to 33.5
0 to 0.8
Residuals, % 0
0 to 0.5