EN 1.4020 Stainless Steel vs. ISO-WD32260 Magnesium
EN 1.4020 stainless steel belongs to the iron alloys classification, while ISO-WD32260 magnesium belongs to the magnesium alloys. There are 26 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is EN 1.4020 stainless steel and the bottom bar is ISO-WD32260 magnesium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 46 |
| Elongation at Break, % | 13 to 34 | |
| 4.5 to 6.0 |
| Fatigue Strength, MPa | 340 to 540 | |
| 150 to 190 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 77 | |
| 18 |
| Shear Strength, MPa | 510 to 680 | |
| 190 to 200 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 1130 | |
| 330 to 340 |
| Tensile Strength: Yield (Proof), MPa | 430 to 950 | |
| 230 to 250 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 330 |
| Maximum Temperature: Mechanical, °C | 890 | |
| 120 |
| Melting Completion (Liquidus), °C | 1390 | |
| 600 |
| Melting Onset (Solidus), °C | 1350 | |
| 520 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 970 |
| Thermal Expansion, µm/m-K | 17 | |
| 27 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 13 |
| Density, g/cm3 | 7.6 | |
| 1.9 |
| Embodied Carbon, kg CO2/kg material | 2.5 | |
| 23 |
| Embodied Energy, MJ/kg | 37 | |
| 160 |
| Embodied Water, L/kg | 150 | |
| 940 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 220 | |
| 14 to 19 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 460 to 2290 | |
| 560 to 700 |
| Stiffness to Weight: Axial, points | 14 | |
| 13 |
| Stiffness to Weight: Bending, points | 25 | |
| 63 |
| Strength to Weight: Axial, points | 28 to 41 | |
| 48 to 51 |
| Strength to Weight: Bending, points | 25 to 32 | |
| 56 to 58 |
| Thermal Shock Resistance, points | 16 to 23 | |
| 19 to 20 |
Alloy Composition
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| Carbon (C), % | 0 to 0.15 | |
| 0 |
| Chromium (Cr), % | 16.5 to 19 | |
| 0 |
| Iron (Fe), % | 62.8 to 71.8 | |
| 0 |
| Magnesium (Mg), % | 0 | |
| 92.7 to 94.8 |
| Manganese (Mn), % | 11 to 14 | |
| 0 |
| Nickel (Ni), % | 0.5 to 2.5 | |
| 0 |
| Nitrogen (N), % | 0.2 to 0.45 | |
| 0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 |
| Sulfur (S), % | 0 to 0.030 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 4.8 to 6.2 |
| Zirconium (Zr), % | 0 | |
| 0.45 to 0.8 |
| Residuals, % | 0 | |
| 0 to 0.3 |