50Cr-50Ni Alloy vs. SAE-AISI 1065 Steel
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while SAE-AISI 1065 steel belongs to the iron alloys. There are 21 material properties with values for both materials. Properties with values for just one material (11, in this case) are not shown.
For each property being compared, the top bar is 50Cr-50Ni alloy and the bottom bar is SAE-AISI 1065 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 5.7 | |
11 to 14 |
Poisson's Ratio | 0.26 | |
0.29 |
Shear Modulus, GPa | 84 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
710 to 780 |
Tensile Strength: Yield (Proof), MPa | 390 | |
430 to 550 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
250 |
Specific Heat Capacity, J/kg-K | 490 | |
470 |
Thermal Expansion, µm/m-K | 15 | |
11 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
1.8 |
Density, g/cm3 | 8.0 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
1.4 |
Embodied Energy, MJ/kg | 110 | |
19 |
Embodied Water, L/kg | 350 | |
46 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
74 to 90 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
490 to 820 |
Stiffness to Weight: Axial, points | 15 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
24 |
Strength to Weight: Axial, points | 21 | |
25 to 28 |
Strength to Weight: Bending, points | 20 | |
23 to 24 |
Thermal Shock Resistance, points | 14 | |
25 to 27 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0.6 to 0.7 |
Chromium (Cr), % | 48 to 52 | |
0 |
Iron (Fe), % | 0 to 1.0 | |
98.3 to 98.8 |
Manganese (Mn), % | 0 to 0.3 | |
0.6 to 0.9 |
Nickel (Ni), % | 44.5 to 52 | |
0 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.040 |
Silicon (Si), % | 0 to 1.0 | |
0 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.050 |
Titanium (Ti), % | 0 to 0.5 | |
0 |