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C85700 Brass vs. C33200 Brass

Both C85700 brass and C33200 brass are copper alloys. They have a moderately high 94% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is C85700 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, % 17
7.0 to 60
Poisson's Ratio 0.31
0.31
Shear Modulus, GPa 40
40
Tensile Strength: Ultimate (UTS), MPa 310
320 to 520
Tensile Strength: Yield (Proof), MPa 110
110 to 450

Thermal Properties

Latent Heat of Fusion, J/g 170
170
Maximum Temperature: Mechanical, °C 120
130
Melting Completion (Liquidus), °C 940
930
Melting Onset (Solidus), °C 910
900
Specific Heat Capacity, J/kg-K 380
380
Thermal Conductivity, W/m-K 84
120
Thermal Expansion, µm/m-K 21
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22
26
Electrical Conductivity: Equal Weight (Specific), % IACS 25
28

Otherwise Unclassified Properties

Base Metal Price, % relative 24
24
Density, g/cm3 8.0
8.2
Embodied Carbon, kg CO2/kg material 2.8
2.6
Embodied Energy, MJ/kg 47
44
Embodied Water, L/kg 330
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 41
35 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 59
60 to 960
Stiffness to Weight: Axial, points 7.2
7.1
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 11
11 to 17
Strength to Weight: Bending, points 13
13 to 17
Thermal Diffusivity, mm2/s 27
37
Thermal Shock Resistance, points 10
11 to 17

Alloy Composition


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Aluminum (Al), % 0 to 0.8
0
Copper (Cu), % 58 to 64
65 to 68
Iron (Fe), % 0 to 0.7
0 to 0.070
Lead (Pb), % 0.8 to 1.5
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), % 32 to 40
29 to 33.5
Residuals, % 0 to 1.3
0 to 0.4