50Cr-50Ni Alloy vs. C44400 Brass
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while C44400 brass belongs to the copper alloys. 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 50Cr-50Ni alloy and the bottom bar is C44400 brass.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
110 |
Poisson's Ratio | 0.26 | |
0.32 |
Shear Modulus, GPa | 84 | |
41 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
350 |
Tensile Strength: Yield (Proof), MPa | 390 | |
120 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
180 |
Specific Heat Capacity, J/kg-K | 490 | |
380 |
Thermal Expansion, µm/m-K | 15 | |
20 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
26 |
Density, g/cm3 | 8.0 | |
8.3 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
2.8 |
Embodied Energy, MJ/kg | 110 | |
46 |
Embodied Water, L/kg | 350 | |
330 |
Common Calculations
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
65 |
Stiffness to Weight: Axial, points | 15 | |
7.2 |
Stiffness to Weight: Bending, points | 25 | |
19 |
Strength to Weight: Axial, points | 21 | |
12 |
Strength to Weight: Bending, points | 20 | |
13 |
Thermal Shock Resistance, points | 14 | |
12 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Antimony (Sb), % | 0 | |
0.020 to 0.1 |
Carbon (C), % | 0 to 0.1 | |
0 |
Chromium (Cr), % | 48 to 52 | |
0 |
Copper (Cu), % | 0 | |
70 to 73 |
Iron (Fe), % | 0 to 1.0 | |
0 to 0.060 |
Lead (Pb), % | 0 | |
0 to 0.070 |
Manganese (Mn), % | 0 to 0.3 | |
0 |
Nickel (Ni), % | 44.5 to 52 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 |
Sulfur (S), % | 0 to 0.020 | |
0 |
Tin (Sn), % | 0 | |
0.9 to 1.2 |
Titanium (Ti), % | 0 to 0.5 | |
0 |
Zinc (Zn), % | 0 | |
25.2 to 29.1 |
Residuals, % | 0 | |
0 to 0.4 |