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50Cr-50Ni Alloy vs. C66200 Brass

50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while C66200 brass belongs to the copper alloys. There are 21 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is 50Cr-50Ni alloy and the bottom bar is C66200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 210
110
Elongation at Break, % 5.7
8.0 to 15
Poisson's Ratio 0.26
0.33
Shear Modulus, GPa 84
42
Tensile Strength: Ultimate (UTS), MPa 620
450 to 520
Tensile Strength: Yield (Proof), MPa 390
410 to 480

Thermal Properties

Latent Heat of Fusion, J/g 350
200
Specific Heat Capacity, J/kg-K 490
390
Thermal Expansion, µm/m-K 15
18

Otherwise Unclassified Properties

Base Metal Price, % relative 50
29
Density, g/cm3 8.0
8.7
Embodied Carbon, kg CO2/kg material 7.9
2.7
Embodied Energy, MJ/kg 110
43
Embodied Water, L/kg 350
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31
40 to 66
Resilience: Unit (Modulus of Resilience), kJ/m3 350
760 to 1030
Stiffness to Weight: Axial, points 15
7.2
Stiffness to Weight: Bending, points 25
19
Strength to Weight: Axial, points 21
14 to 17
Strength to Weight: Bending, points 20
15 to 16
Thermal Shock Resistance, points 14
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.25
0
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 48 to 52
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), % 44.5 to 52
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