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C26200 Brass vs. C85500 Brass

Both C26200 brass and C85500 brass are copper alloys. They have a moderately high 93% of their average alloy composition in common. There are 29 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 C26200 brass and the bottom bar is C85500 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
100
Elongation at Break, % 3.0 to 180
40
Poisson's Ratio 0.31
0.31
Rockwell B Hardness 55 to 93
55
Shear Modulus, GPa 41
40
Tensile Strength: Ultimate (UTS), MPa 330 to 770
410
Tensile Strength: Yield (Proof), MPa 110 to 490
160

Thermal Properties

Latent Heat of Fusion, J/g 180
170
Maximum Temperature: Mechanical, °C 140
120
Melting Completion (Liquidus), °C 950
900
Melting Onset (Solidus), °C 920
890
Specific Heat Capacity, J/kg-K 390
390
Thermal Conductivity, W/m-K 120
120
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
26
Electrical Conductivity: Equal Weight (Specific), % IACS 31
29

Otherwise Unclassified Properties

Base Metal Price, % relative 25
23
Density, g/cm3 8.2
8.0
Embodied Carbon, kg CO2/kg material 2.7
2.7
Embodied Energy, MJ/kg 45
46
Embodied Water, L/kg 320
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 160
130
Resilience: Unit (Modulus of Resilience), kJ/m3 62 to 1110
120
Stiffness to Weight: Axial, points 7.2
7.3
Stiffness to Weight: Bending, points 19
20
Strength to Weight: Axial, points 11 to 26
14
Strength to Weight: Bending, points 13 to 23
15
Thermal Diffusivity, mm2/s 38
38
Thermal Shock Resistance, points 11 to 26
14

Alloy Composition


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Copper (Cu), % 67 to 70
59 to 63
Iron (Fe), % 0 to 0.050
0 to 0.2
Lead (Pb), % 0 to 0.070
0 to 0.2
Manganese (Mn), % 0
0 to 0.2
Nickel (Ni), % 0
0 to 0.2
Tin (Sn), % 0
0 to 0.2
Zinc (Zn), % 29.6 to 33
35.1 to 41
Residuals, % 0 to 0.3
0 to 0.9