AISI 422 Stainless Steel vs. S17600 Stainless Steel
Both AISI 422 stainless steel and S17600 stainless steel are iron alloys. They have 88% of their average alloy composition in common.
For each property being compared, the top bar is AISI 422 stainless steel and the bottom bar is S17600 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 260 to 330 | |
| 270 to 410 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 15 to 17 | |
| 8.6 to 11 |
| Fatigue Strength, MPa | 410 to 500 | |
| 300 to 680 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Reduction in Area, % | 34 to 40 | |
| 28 to 50 |
| Rockwell C Hardness | 21 | |
| 28 to 44 |
| Shear Modulus, GPa | 76 | |
| 76 |
| Shear Strength, MPa | 560 to 660 | |
| 560 to 880 |
| Tensile Strength: Ultimate (UTS), MPa | 910 to 1080 | |
| 940 to 1490 |
| Tensile Strength: Yield (Proof), MPa | 670 to 870 | |
| 580 to 1310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 270 | |
| 290 |
| Maximum Temperature: Corrosion, °C | 380 | |
| 550 |
| Maximum Temperature: Mechanical, °C | 650 | |
| 890 |
| Melting Completion (Liquidus), °C | 1480 | |
| 1430 |
| Melting Onset (Solidus), °C | 1470 | |
| 1390 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 480 |
| Thermal Conductivity, W/m-K | 24 | |
| 15 |
| Thermal Expansion, µm/m-K | 10 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 4.7 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 5.3 | |
| 2.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 13 |
| Density, g/cm3 | 7.9 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 3.1 | |
| 2.9 |
| Embodied Energy, MJ/kg | 44 | |
| 42 |
| Embodied Water, L/kg | 100 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 17 | |
| 17 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 150 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 1140 to 1910 | |
| 850 to 4390 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 32 to 38 | |
| 34 to 54 |
| Strength to Weight: Bending, points | 26 to 30 | |
| 28 to 37 |
| Thermal Diffusivity, mm2/s | 6.4 | |
| 4.1 |
| Thermal Shock Resistance, points | 33 to 39 | |
| 31 to 50 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.4 |
| Carbon (C), % | 0.2 to 0.25 | |
| 0 to 0.080 |
| Chromium (Cr), % | 11 to 12.5 | |
| 16 to 17.5 |
| Iron (Fe), % | 81.9 to 85.8 | |
| 71.3 to 77.6 |
| Manganese (Mn), % | 0.5 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0.9 to 1.3 | |
| 0 |
| Nickel (Ni), % | 0.5 to 1.0 | |
| 6.0 to 7.5 |
| Phosphorus (P), % | 0 to 0.025 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 0.5 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.025 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 | |
| 0.4 to 1.2 |
| Tungsten (W), % | 0.9 to 1.3 | |
| 0 |
| Vanadium (V), % | 0.2 to 0.3 | |
| 0 |