EN 1.5662 Steel vs. Nickel 718
EN 1.5662 steel belongs to the iron alloys classification, while nickel 718 belongs to the nickel alloys. They have a modest 28% of their average alloy composition in common, which, by itself, doesn't mean much. There are 29 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.
For each property being compared, the top bar is EN 1.5662 steel and the bottom bar is nickel 718.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
190 |
Elongation at Break, % | 20 | |
12 to 50 |
Fatigue Strength, MPa | 380 to 450 | |
460 to 760 |
Poisson's Ratio | 0.29 | |
0.29 |
Reduction in Area, % | 56 to 57 | |
34 to 64 |
Shear Modulus, GPa | 73 | |
75 |
Shear Strength, MPa | 460 to 470 | |
660 to 950 |
Tensile Strength: Ultimate (UTS), MPa | 740 to 750 | |
930 to 1530 |
Tensile Strength: Yield (Proof), MPa | 550 to 660 | |
510 to 1330 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
310 |
Maximum Temperature: Mechanical, °C | 430 | |
980 |
Melting Completion (Liquidus), °C | 1460 | |
1340 |
Melting Onset (Solidus), °C | 1410 | |
1260 |
Specific Heat Capacity, J/kg-K | 470 | |
450 |
Thermal Expansion, µm/m-K | 13 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 8.7 | |
1.4 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 9.8 | |
1.5 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 7.5 | |
75 |
Density, g/cm3 | 8.0 | |
8.3 |
Embodied Carbon, kg CO2/kg material | 2.3 | |
13 |
Embodied Energy, MJ/kg | 31 | |
190 |
Embodied Water, L/kg | 63 | |
250 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 150 | |
140 to 390 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 810 to 1150 | |
660 to 4560 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
23 |
Strength to Weight: Axial, points | 26 | |
31 to 51 |
Strength to Weight: Bending, points | 23 | |
25 to 35 |
Thermal Shock Resistance, points | 22 | |
27 to 44 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.2 to 0.8 |
Boron (B), % | 0 | |
0 to 0.0060 |
Carbon (C), % | 0 to 0.1 | |
0 to 0.080 |
Chromium (Cr), % | 0 | |
17 to 21 |
Cobalt (Co), % | 0 | |
0 to 1.0 |
Copper (Cu), % | 0 | |
0 to 0.3 |
Iron (Fe), % | 88.6 to 91.2 | |
11.1 to 24.6 |
Manganese (Mn), % | 0.3 to 0.8 | |
0 to 0.35 |
Molybdenum (Mo), % | 0 to 0.1 | |
2.8 to 3.3 |
Nickel (Ni), % | 8.5 to 10 | |
50 to 55 |
Niobium (Nb), % | 0 | |
4.8 to 5.5 |
Phosphorus (P), % | 0 to 0.020 | |
0 to 0.015 |
Silicon (Si), % | 0 to 0.35 | |
0 to 0.35 |
Sulfur (S), % | 0 to 0.0050 | |
0 to 0.015 |
Titanium (Ti), % | 0 | |
0.65 to 1.2 |
Vanadium (V), % | 0 to 0.050 | |
0 |