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C33200 Brass vs. C61500 Bronze

Both C33200 brass and C61500 bronze are copper alloys. They have 67% of their average alloy composition in common.

For each property being compared, the top bar is C33200 brass and the bottom bar is C61500 bronze.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 7.0 to 60
3.0 to 55
Poisson's Ratio 0.31
0.34
Rockwell Superficial 30T Hardness 26 to 69
42 to 85
Shear Modulus, GPa 40
42
Shear Strength, MPa 240 to 300
350 to 550
Tensile Strength: Ultimate (UTS), MPa 320 to 520
480 to 970
Tensile Strength: Yield (Proof), MPa 110 to 450
150 to 720

Thermal Properties

Latent Heat of Fusion, J/g 170
220
Maximum Temperature: Mechanical, °C 130
220
Melting Completion (Liquidus), °C 930
1040
Melting Onset (Solidus), °C 900
1030
Specific Heat Capacity, J/kg-K 380
430
Thermal Conductivity, W/m-K 120
58
Thermal Expansion, µm/m-K 20
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
13
Electrical Conductivity: Equal Weight (Specific), % IACS 28
13

Otherwise Unclassified Properties

Base Metal Price, % relative 24
29
Density, g/cm3 8.2
8.4
Embodied Carbon, kg CO2/kg material 2.6
3.2
Embodied Energy, MJ/kg 44
52
Embodied Water, L/kg 320
380

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
27 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 960
100 to 2310
Stiffness to Weight: Axial, points 7.1
7.5
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 11 to 17
16 to 32
Strength to Weight: Bending, points 13 to 17
16 to 26
Thermal Diffusivity, mm2/s 37
16
Thermal Shock Resistance, points 11 to 17
17 to 34

Alloy Composition


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Aluminum (Al), % 0
7.7 to 8.3
Copper (Cu), % 65 to 68
89 to 90.5
Iron (Fe), % 0 to 0.070
0
Lead (Pb), % 1.5 to 2.5
0 to 0.015
Nickel (Ni), % 0
1.8 to 2.2
Zinc (Zn), % 29 to 33.5
0
Residuals, % 0 to 0.4
0 to 0.5

Comparable Variants