S45000 Stainless Steel vs. S17600 Stainless Steel
Both S45000 stainless steel and S17600 stainless steel are iron alloys. They have a very high 97% of their average alloy composition in common.
For each property being compared, the top bar is S45000 stainless steel and the bottom bar is S17600 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 280 to 410 | |
| 270 to 410 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 200 |
| Elongation at Break, % | 6.8 to 14 | |
| 8.6 to 11 |
| Fatigue Strength, MPa | 330 to 650 | |
| 300 to 680 |
| Poisson's Ratio | 0.28 | |
| 0.28 |
| Reduction in Area, % | 22 to 50 | |
| 28 to 50 |
| Rockwell C Hardness | 28 to 44 | |
| 28 to 44 |
| Shear Modulus, GPa | 76 | |
| 76 |
| Shear Strength, MPa | 590 to 830 | |
| 560 to 880 |
| Tensile Strength: Ultimate (UTS), MPa | 980 to 1410 | |
| 940 to 1490 |
| Tensile Strength: Yield (Proof), MPa | 580 to 1310 | |
| 580 to 1310 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 290 |
| Maximum Temperature: Corrosion, °C | 400 | |
| 550 |
| Maximum Temperature: Mechanical, °C | 840 | |
| 890 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1430 |
| Melting Onset (Solidus), °C | 1390 | |
| 1390 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 480 |
| Thermal Conductivity, W/m-K | 17 | |
| 15 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.2 | |
| 2.3 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.5 | |
| 2.7 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 13 |
| Density, g/cm3 | 7.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 2.9 |
| Embodied Energy, MJ/kg | 39 | |
| 42 |
| Embodied Water, L/kg | 130 | |
| 130 |
Common Calculations
| PREN (Pitting Resistance) | 17 | |
| 17 |
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 94 to 160 | |
| 70 to 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 850 to 4400 | |
| 850 to 4390 |
| Stiffness to Weight: Axial, points | 14 | |
| 14 |
| Stiffness to Weight: Bending, points | 25 | |
| 25 |
| Strength to Weight: Axial, points | 35 to 50 | |
| 34 to 54 |
| Strength to Weight: Bending, points | 28 to 36 | |
| 28 to 37 |
| Thermal Diffusivity, mm2/s | 4.5 | |
| 4.1 |
| Thermal Shock Resistance, points | 33 to 47 | |
| 31 to 50 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 0 to 0.4 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.080 |
| Chromium (Cr), % | 14 to 16 | |
| 16 to 17.5 |
| Copper (Cu), % | 1.3 to 1.8 | |
| 0 |
| Iron (Fe), % | 72.1 to 79.3 | |
| 71.3 to 77.6 |
| Manganese (Mn), % | 0 to 1.0 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0.5 to 1.0 | |
| 0 |
| Nickel (Ni), % | 5.0 to 7.0 | |
| 6.0 to 7.5 |
| Phosphorus (P), % | 0 to 0.040 | |
| 0 to 0.040 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.030 |
| Titanium (Ti), % | 0 | |
| 0.4 to 1.2 |