S20910 Stainless Steel vs. EN 1.4606 Stainless Steel
Both S20910 stainless steel and EN 1.4606 stainless steel are iron alloys. They have 84% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.
For each property being compared, the top bar is S20910 stainless steel and the bottom bar is EN 1.4606 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
190 |
Elongation at Break, % | 14 to 39 | |
23 to 39 |
Fatigue Strength, MPa | 310 to 460 | |
240 to 420 |
Poisson's Ratio | 0.28 | |
0.29 |
Shear Modulus, GPa | 79 | |
75 |
Shear Strength, MPa | 500 to 570 | |
410 to 640 |
Tensile Strength: Ultimate (UTS), MPa | 780 to 940 | |
600 to 1020 |
Tensile Strength: Yield (Proof), MPa | 430 to 810 | |
280 to 630 |
Thermal Properties
Latent Heat of Fusion, J/g | 300 | |
300 |
Maximum Temperature: Corrosion, °C | 460 | |
770 |
Maximum Temperature: Mechanical, °C | 1080 | |
910 |
Melting Completion (Liquidus), °C | 1420 | |
1430 |
Melting Onset (Solidus), °C | 1380 | |
1380 |
Specific Heat Capacity, J/kg-K | 480 | |
470 |
Thermal Conductivity, W/m-K | 13 | |
14 |
Thermal Expansion, µm/m-K | 16 | |
11 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 22 | |
26 |
Density, g/cm3 | 7.8 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 4.8 | |
6.0 |
Embodied Energy, MJ/kg | 68 | |
87 |
Embodied Water, L/kg | 180 | |
170 |
Common Calculations
PREN (Pitting Resistance) | 34 | |
19 |
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 120 to 260 | |
190 to 200 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 1640 | |
200 to 1010 |
Stiffness to Weight: Axial, points | 14 | |
14 |
Stiffness to Weight: Bending, points | 25 | |
24 |
Strength to Weight: Axial, points | 28 to 33 | |
21 to 36 |
Strength to Weight: Bending, points | 24 to 27 | |
20 to 28 |
Thermal Diffusivity, mm2/s | 3.6 | |
3.7 |
Thermal Shock Resistance, points | 17 to 21 | |
21 to 35 |
Alloy Composition
Aluminum (Al), % | 0 | |
0 to 0.35 |
Boron (B), % | 0 | |
0.0010 to 0.010 |
Carbon (C), % | 0 to 0.060 | |
0 to 0.080 |
Chromium (Cr), % | 20.5 to 23.5 | |
13 to 16 |
Iron (Fe), % | 52.1 to 62.1 | |
49.2 to 59 |
Manganese (Mn), % | 4.0 to 6.0 | |
1.0 to 2.0 |
Molybdenum (Mo), % | 1.5 to 3.0 | |
1.0 to 1.5 |
Nickel (Ni), % | 11.5 to 13.5 | |
24 to 27 |
Niobium (Nb), % | 0.1 to 0.3 | |
0 |
Nitrogen (N), % | 0.2 to 0.4 | |
0 |
Phosphorus (P), % | 0 to 0.040 | |
0 to 0.025 |
Silicon (Si), % | 0 to 0.75 | |
0 to 1.0 |
Sulfur (S), % | 0 to 0.030 | |
0 to 0.015 |
Titanium (Ti), % | 0 | |
1.9 to 2.3 |
Vanadium (V), % | 0.1 to 0.3 | |
0.1 to 0.5 |