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C85700 Brass vs. 60Cr-40Ni Alloy

C85700 brass belongs to the copper alloys classification, while 60Cr-40Ni alloy belongs to the otherwise unclassified metals. There are 19 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.

For each property being compared, the top bar is C85700 brass and the bottom bar is 60Cr-40Ni alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
220
Poisson's Ratio 0.31
0.25
Shear Modulus, GPa 40
87
Tensile Strength: Ultimate (UTS), MPa 310
870
Tensile Strength: Yield (Proof), MPa 110
660

Thermal Properties

Latent Heat of Fusion, J/g 170
370
Specific Heat Capacity, J/kg-K 380
490
Thermal Expansion, µm/m-K 21
16

Otherwise Unclassified Properties

Base Metal Price, % relative 24
49
Density, g/cm3 8.0
7.8
Embodied Carbon, kg CO2/kg material 2.8
7.4
Embodied Energy, MJ/kg 47
110
Embodied Water, L/kg 330
380

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m3 59
1000
Stiffness to Weight: Axial, points 7.2
16
Stiffness to Weight: Bending, points 20
26
Strength to Weight: Axial, points 11
31
Strength to Weight: Bending, points 13
26
Thermal Shock Resistance, points 10
18

Alloy Composition

Aluminum (Al), % 0 to 0.8
0 to 0.25
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
58 to 62
Copper (Cu), % 58 to 64
0
Iron (Fe), % 0 to 0.7
0 to 1.0
Lead (Pb), % 0.8 to 1.5
0
Manganese (Mn), % 0
0 to 0.3
Nickel (Ni), % 0 to 1.0
34.5 to 42
Nitrogen (N), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.050
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tin (Sn), % 0.5 to 1.5
0
Titanium (Ti), % 0
0 to 0.5
Zinc (Zn), % 32 to 40
0
Residuals, % 0 to 1.3
0