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60Cr-40Ni Alloy vs. C66200 Brass

60Cr-40Ni alloy belongs to the otherwise unclassified metals classification, while C66200 brass belongs to the copper alloys. There are 19 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is 60Cr-40Ni alloy and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
110
Poisson's Ratio 0.25
0.33
Shear Modulus, GPa 87
42
Tensile Strength: Ultimate (UTS), MPa 870
450 to 520
Tensile Strength: Yield (Proof), MPa 660
410 to 480

Thermal Properties

Latent Heat of Fusion, J/g 370
200
Specific Heat Capacity, J/kg-K 490
390
Thermal Expansion, µm/m-K 16
18

Otherwise Unclassified Properties

Base Metal Price, % relative 49
29
Density, g/cm3 7.8
8.7
Embodied Carbon, kg CO2/kg material 7.4
2.7
Embodied Energy, MJ/kg 110
43
Embodied Water, L/kg 380
320

Common Calculations

Resilience: Unit (Modulus of Resilience), kJ/m3 1000
760 to 1030
Stiffness to Weight: Axial, points 16
7.2
Stiffness to Weight: Bending, points 26
19
Strength to Weight: Axial, points 31
14 to 17
Strength to Weight: Bending, points 26
15 to 16
Thermal Shock Resistance, points 18
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.25
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 58 to 62
0
Copper (Cu), % 0
86.6 to 91
Iron (Fe), % 0 to 1.0
0 to 0.050
Lead (Pb), % 0
0 to 0.050
Manganese (Mn), % 0 to 0.3
0
Nickel (Ni), % 34.5 to 42
0.3 to 1.0
Nitrogen (N), % 0 to 0.3
0
Phosphorus (P), % 0 to 0.020
0.050 to 0.2
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.020
0
Tin (Sn), % 0
0.2 to 0.7
Titanium (Ti), % 0 to 0.5
0
Zinc (Zn), % 0
6.5 to 12.9
Residuals, % 0
0 to 0.5