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C33200 Brass vs. C85400 Brass

Both C33200 brass and C85400 brass are copper alloys. They have a very high 97% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C33200 brass and the bottom bar is C85400 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
100
Elongation at Break, % 7.0 to 60
23
Poisson's Ratio 0.31
0.32
Shear Modulus, GPa 40
40
Tensile Strength: Ultimate (UTS), MPa 320 to 520
220
Tensile Strength: Yield (Proof), MPa 110 to 450
85

Thermal Properties

Latent Heat of Fusion, J/g 170
180
Maximum Temperature: Mechanical, °C 130
130
Melting Completion (Liquidus), °C 930
940
Melting Onset (Solidus), °C 900
940
Specific Heat Capacity, J/kg-K 380
380
Thermal Conductivity, W/m-K 120
89
Thermal Expansion, µm/m-K 20
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
20
Electrical Conductivity: Equal Weight (Specific), % IACS 28
22

Otherwise Unclassified Properties

Base Metal Price, % relative 24
25
Density, g/cm3 8.2
8.3
Embodied Carbon, kg CO2/kg material 2.6
2.8
Embodied Energy, MJ/kg 44
46
Embodied Water, L/kg 320
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 35 to 150
40
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 960
35
Stiffness to Weight: Axial, points 7.1
7.0
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 11 to 17
7.5
Strength to Weight: Bending, points 13 to 17
9.9
Thermal Diffusivity, mm2/s 37
28
Thermal Shock Resistance, points 11 to 17
7.6

Alloy Composition

Aluminum (Al), % 0
0 to 0.35
Copper (Cu), % 65 to 68
65 to 70
Iron (Fe), % 0 to 0.070
0 to 0.7
Lead (Pb), % 1.5 to 2.5
1.5 to 3.8
Nickel (Ni), % 0
0 to 1.0
Silicon (Si), % 0
0 to 0.050
Tin (Sn), % 0
0.5 to 1.5
Zinc (Zn), % 29 to 33.5
24 to 32
Residuals, % 0
0 to 1.1