50Cr-50Ni Alloy vs. ASTM A182 Grade FR
50Cr-50Ni alloy belongs to the otherwise unclassified metals classification, while ASTM A182 grade FR 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 ASTM A182 grade FR.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 210 | |
190 |
Elongation at Break, % | 5.7 | |
28 |
Poisson's Ratio | 0.26 | |
0.29 |
Shear Modulus, GPa | 84 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 620 | |
490 |
Tensile Strength: Yield (Proof), MPa | 390 | |
360 |
Thermal Properties
Latent Heat of Fusion, J/g | 350 | |
250 |
Specific Heat Capacity, J/kg-K | 490 | |
470 |
Thermal Expansion, µm/m-K | 15 | |
13 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 50 | |
3.3 |
Density, g/cm3 | 8.0 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 7.9 | |
1.6 |
Embodied Energy, MJ/kg | 110 | |
21 |
Embodied Water, L/kg | 350 | |
52 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 31 | |
120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 350 | |
340 |
Stiffness to Weight: Axial, points | 15 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
24 |
Strength to Weight: Axial, points | 21 | |
17 |
Strength to Weight: Bending, points | 20 | |
17 |
Thermal Shock Resistance, points | 14 | |
14 |
Alloy Composition
Aluminum (Al), % | 0 to 0.25 | |
0 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.2 |
Chromium (Cr), % | 48 to 52 | |
0 |
Copper (Cu), % | 0 | |
0.75 to 1.3 |
Iron (Fe), % | 0 to 1.0 | |
95.2 to 97.3 |
Manganese (Mn), % | 0 to 0.3 | |
0.4 to 1.1 |
Nickel (Ni), % | 44.5 to 52 | |
1.6 to 2.2 |
Nitrogen (N), % | 0 to 0.3 | |
0 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.045 |
Silicon (Si), % | 0 to 1.0 | |
0 |
Sulfur (S), % | 0 to 0.020 | |
0 to 0.050 |
Titanium (Ti), % | 0 to 0.5 | |
0 |