EN 1.8201 Steel vs. EN 1.5414 Steel
Both EN 1.8201 steel and EN 1.5414 steel are iron alloys. They have a very high 96% of their average alloy composition in common. There are 32 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.
For each property being compared, the top bar is EN 1.8201 steel and the bottom bar is EN 1.5414 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 190 | |
170 to 180 |
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
190 |
Elongation at Break, % | 20 | |
22 |
Fatigue Strength, MPa | 310 | |
250 to 270 |
Impact Strength: V-Notched Charpy, J | 38 | |
46 |
Poisson's Ratio | 0.29 | |
0.29 |
Shear Modulus, GPa | 74 | |
73 |
Shear Strength, MPa | 390 | |
350 to 370 |
Tensile Strength: Ultimate (UTS), MPa | 630 | |
550 to 580 |
Tensile Strength: Yield (Proof), MPa | 450 | |
350 to 380 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
250 |
Maximum Temperature: Mechanical, °C | 450 | |
410 |
Melting Completion (Liquidus), °C | 1500 | |
1470 |
Melting Onset (Solidus), °C | 1450 | |
1420 |
Specific Heat Capacity, J/kg-K | 470 | |
470 |
Thermal Conductivity, W/m-K | 40 | |
44 |
Thermal Expansion, µm/m-K | 13 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.8 | |
7.3 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.8 | |
8.4 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 7.0 | |
2.6 |
Density, g/cm3 | 8.0 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 2.5 | |
1.6 |
Embodied Energy, MJ/kg | 36 | |
21 |
Embodied Water, L/kg | 59 | |
50 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 110 | |
110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 530 | |
320 to 370 |
Stiffness to Weight: Axial, points | 13 | |
13 |
Stiffness to Weight: Bending, points | 24 | |
24 |
Strength to Weight: Axial, points | 22 | |
19 to 20 |
Strength to Weight: Bending, points | 20 | |
19 to 20 |
Thermal Diffusivity, mm2/s | 11 | |
12 |
Thermal Shock Resistance, points | 18 | |
16 to 17 |
Alloy Composition
Aluminum (Al), % | 0 to 0.030 | |
0 |
Boron (B), % | 0.0010 to 0.0060 | |
0 |
Carbon (C), % | 0.040 to 0.1 | |
0 to 0.2 |
Chromium (Cr), % | 1.9 to 2.6 | |
0 to 0.3 |
Copper (Cu), % | 0 | |
0 to 0.3 |
Iron (Fe), % | 93.6 to 96.2 | |
96.4 to 98.7 |
Manganese (Mn), % | 0.1 to 0.6 | |
0.9 to 1.5 |
Molybdenum (Mo), % | 0.050 to 0.3 | |
0.45 to 0.6 |
Nickel (Ni), % | 0 | |
0 to 0.3 |
Niobium (Nb), % | 0.020 to 0.080 | |
0 |
Nitrogen (N), % | 0 to 0.015 | |
0 to 0.012 |
Phosphorus (P), % | 0 to 0.030 | |
0 to 0.015 |
Silicon (Si), % | 0 to 0.5 | |
0 to 0.4 |
Sulfur (S), % | 0 to 0.010 | |
0 to 0.0050 |
Titanium (Ti), % | 0.0050 to 0.060 | |
0 |
Tungsten (W), % | 1.5 to 1.8 | |
0 |
Vanadium (V), % | 0.2 to 0.3 | |
0 |