EN 1.4962 Stainless Steel vs. EN 1.8918 Steel
Both EN 1.4962 stainless steel and EN 1.8918 steel are iron alloys. They have 67% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is EN 1.4962 stainless steel and the bottom bar is EN 1.8918 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 190 to 210 | |
190 |
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
190 |
Elongation at Break, % | 22 to 34 | |
19 |
Fatigue Strength, MPa | 210 to 330 | |
330 |
Poisson's Ratio | 0.28 | |
0.29 |
Shear Modulus, GPa | 77 | |
73 |
Shear Strength, MPa | 420 to 440 | |
400 |
Tensile Strength: Ultimate (UTS), MPa | 630 to 690 | |
640 |
Tensile Strength: Yield (Proof), MPa | 260 to 490 | |
490 |
Thermal Properties
Latent Heat of Fusion, J/g | 280 | |
250 |
Maximum Temperature: Mechanical, °C | 910 | |
400 |
Melting Completion (Liquidus), °C | 1480 | |
1460 |
Melting Onset (Solidus), °C | 1440 | |
1420 |
Specific Heat Capacity, J/kg-K | 470 | |
470 |
Thermal Conductivity, W/m-K | 14 | |
46 |
Thermal Expansion, µm/m-K | 16 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
7.5 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
8.6 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 23 | |
2.5 |
Density, g/cm3 | 8.1 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 4.1 | |
1.7 |
Embodied Energy, MJ/kg | 59 | |
24 |
Embodied Water, L/kg | 150 | |
51 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 170 | |
110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 170 to 610 | |
640 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
24 |
Strength to Weight: Axial, points | 21 to 24 | |
23 |
Strength to Weight: Bending, points | 20 to 21 | |
21 |
Thermal Diffusivity, mm2/s | 3.7 | |
12 |
Thermal Shock Resistance, points | 14 to 16 | |
19 |
Alloy Composition
Aluminum (Al), % | 0 | |
0.020 to 0.050 |
Boron (B), % | 0.0015 to 0.0060 | |
0 |
Carbon (C), % | 0.070 to 0.15 | |
0 to 0.2 |
Chromium (Cr), % | 15.5 to 17.5 | |
0 to 0.3 |
Copper (Cu), % | 0 | |
0 to 0.7 |
Iron (Fe), % | 62.1 to 69 | |
95.2 to 98.9 |
Manganese (Mn), % | 0 to 1.5 | |
1.1 to 1.7 |
Molybdenum (Mo), % | 0 | |
0 to 0.1 |
Nickel (Ni), % | 12.5 to 14.5 | |
0 to 0.8 |
Niobium (Nb), % | 0 | |
0 to 0.050 |
Nitrogen (N), % | 0 | |
0 to 0.025 |
Phosphorus (P), % | 0 to 0.035 | |
0 to 0.020 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.6 |
Sulfur (S), % | 0 to 0.015 | |
0 to 0.0050 |
Titanium (Ti), % | 0.4 to 0.7 | |
0 to 0.030 |
Tungsten (W), % | 2.5 to 3.0 | |
0 |
Vanadium (V), % | 0 | |
0 to 0.2 |