S36200 Stainless Steel vs. Type 4 Magnetic Alloy
S36200 stainless steel belongs to the iron alloys classification, while Type 4 magnetic alloy belongs to the nickel alloys. They have a modest 21% of their average alloy composition in common, which, by itself, doesn't mean much. There are 28 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.
For each property being compared, the top bar is S36200 stainless steel and the bottom bar is Type 4 magnetic alloy.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 190 |
| Elongation at Break, % | 3.4 to 4.6 | |
| 2.0 to 40 |
| Fatigue Strength, MPa | 450 to 570 | |
| 220 to 400 |
| Poisson's Ratio | 0.28 | |
| 0.31 |
| Shear Modulus, GPa | 76 | |
| 73 |
| Shear Strength, MPa | 680 to 810 | |
| 420 to 630 |
| Tensile Strength: Ultimate (UTS), MPa | 1180 to 1410 | |
| 620 to 1100 |
| Tensile Strength: Yield (Proof), MPa | 960 to 1240 | |
| 270 to 1040 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 820 | |
| 900 |
| Melting Completion (Liquidus), °C | 1440 | |
| 1420 |
| Melting Onset (Solidus), °C | 1400 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 440 |
| Thermal Expansion, µm/m-K | 11 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.3 | |
| 2.9 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.6 | |
| 3.0 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 60 |
| Density, g/cm3 | 7.8 | |
| 8.8 |
| Embodied Carbon, kg CO2/kg material | 2.8 | |
| 10 |
| Embodied Energy, MJ/kg | 40 | |
| 140 |
| Embodied Water, L/kg | 120 | |
| 210 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 46 to 51 | |
| 22 to 200 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2380 to 3930 | |
| 190 to 2840 |
| Stiffness to Weight: Axial, points | 14 | |
| 12 |
| Stiffness to Weight: Bending, points | 25 | |
| 22 |
| Strength to Weight: Axial, points | 42 to 50 | |
| 19 to 35 |
| Strength to Weight: Bending, points | 32 to 36 | |
| 18 to 27 |
| Thermal Shock Resistance, points | 40 to 48 | |
| 21 to 37 |
Alloy Composition
| Aluminum (Al), % | 0 to 0.1 | |
| 0 |
| Carbon (C), % | 0 to 0.050 | |
| 0 to 0.050 |
| Chromium (Cr), % | 14 to 14.5 | |
| 0 to 0.3 |
| Cobalt (Co), % | 0 | |
| 0 to 0.5 |
| Copper (Cu), % | 0 | |
| 0 to 0.3 |
| Iron (Fe), % | 75.4 to 79.5 | |
| 9.5 to 17.5 |
| Manganese (Mn), % | 0 to 0.5 | |
| 0 to 0.8 |
| Molybdenum (Mo), % | 0 to 0.3 | |
| 3.5 to 6.0 |
| Nickel (Ni), % | 6.5 to 7.0 | |
| 79 to 82 |
| Phosphorus (P), % | 0 to 0.030 | |
| 0 to 0.010 |
| Silicon (Si), % | 0 to 0.3 | |
| 0 to 0.5 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 to 0.020 |
| Titanium (Ti), % | 0.6 to 0.9 | |
| 0 |