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C85400 Brass vs. C33200 Brass

Both C85400 brass and C33200 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 C85400 brass and the bottom bar is C33200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

Aluminum (Al), % 0 to 0.35
0
Copper (Cu), % 65 to 70
65 to 68
Iron (Fe), % 0 to 0.7
0 to 0.070
Lead (Pb), % 1.5 to 3.8
1.5 to 2.5
Nickel (Ni), % 0 to 1.0
0
Silicon (Si), % 0 to 0.050
0
Tin (Sn), % 0.5 to 1.5
0
Zinc (Zn), % 24 to 32
29 to 33.5
Residuals, % 0
0 to 0.4