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C68000 Brass vs. C85200 Brass

Both C68000 brass and C85200 brass are copper alloys. Both are furnished in the as-fabricated (no temper or treatment) condition. They have 84% of their average alloy composition in common. There are 26 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 C68000 brass and the bottom bar is C85200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
110
Elongation at Break, % 27
28
Poisson's Ratio 0.3
0.32
Shear Modulus, GPa 40
40
Tensile Strength: Ultimate (UTS), MPa 390
270
Tensile Strength: Yield (Proof), MPa 140
95

Thermal Properties

Latent Heat of Fusion, J/g 170
180
Maximum Temperature: Mechanical, °C 120
140
Melting Completion (Liquidus), °C 880
940
Melting Onset (Solidus), °C 870
930
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 96
84
Thermal Expansion, µm/m-K 21
20

Otherwise Unclassified Properties

Base Metal Price, % relative 23
26
Density, g/cm3 8.0
8.4
Embodied Carbon, kg CO2/kg material 2.8
2.8
Embodied Energy, MJ/kg 48
46
Embodied Water, L/kg 330
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 82
59
Resilience: Unit (Modulus of Resilience), kJ/m3 95
42
Stiffness to Weight: Axial, points 7.3
7.0
Stiffness to Weight: Bending, points 20
19
Strength to Weight: Axial, points 14
8.9
Strength to Weight: Bending, points 15
11
Thermal Diffusivity, mm2/s 31
27
Thermal Shock Resistance, points 13
9.3

Alloy Composition

Aluminum (Al), % 0 to 0.010
0 to 0.0050
Antimony (Sb), % 0
0 to 0.2
Copper (Cu), % 56 to 60
70 to 74
Iron (Fe), % 0.25 to 1.3
0 to 0.6
Lead (Pb), % 0 to 0.050
1.5 to 3.8
Manganese (Mn), % 0.010 to 0.5
0
Nickel (Ni), % 0.2 to 0.8
0 to 1.0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.040 to 0.15
0 to 0.050
Sulfur (S), % 0
0 to 0.050
Tin (Sn), % 0.75 to 1.1
0.7 to 2.0
Zinc (Zn), % 35.6 to 42.8
20 to 27
Residuals, % 0
0 to 0.9