EN 1.4618 Stainless Steel vs. EN-MC21120 Magnesium
EN 1.4618 stainless steel belongs to the iron alloys classification, while EN-MC21120 magnesium belongs to the magnesium alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 1.4618 stainless steel and the bottom bar is EN-MC21120 magnesium.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 200 to 210 | |
| 63 to 75 |
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 46 |
| Elongation at Break, % | 51 | |
| 2.2 to 6.7 |
| Fatigue Strength, MPa | 240 to 250 | |
| 84 to 96 |
| Poisson's Ratio | 0.28 | |
| 0.29 |
| Shear Modulus, GPa | 77 | |
| 18 |
| Shear Strength, MPa | 480 to 500 | |
| 110 to 160 |
| Tensile Strength: Ultimate (UTS), MPa | 680 to 700 | |
| 200 to 270 |
| Tensile Strength: Yield (Proof), MPa | 250 to 260 | |
| 130 to 170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 280 | |
| 350 |
| Maximum Temperature: Mechanical, °C | 900 | |
| 130 |
| Melting Completion (Liquidus), °C | 1400 | |
| 600 |
| Melting Onset (Solidus), °C | 1360 | |
| 490 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 990 |
| Thermal Conductivity, W/m-K | 15 | |
| 76 |
| Thermal Expansion, µm/m-K | 16 | |
| 26 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 2.4 | |
| 11 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.7 | |
| 59 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 13 | |
| 12 |
| Density, g/cm3 | 7.7 | |
| 1.7 |
| Embodied Carbon, kg CO2/kg material | 2.7 | |
| 22 |
| Embodied Energy, MJ/kg | 39 | |
| 160 |
| Embodied Water, L/kg | 150 | |
| 990 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 270 to 280 | |
| 5.0 to 15 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 160 to 170 | |
| 180 to 320 |
| Stiffness to Weight: Axial, points | 14 | |
| 15 |
| Stiffness to Weight: Bending, points | 25 | |
| 69 |
| Strength to Weight: Axial, points | 24 to 25 | |
| 31 to 43 |
| Strength to Weight: Bending, points | 22 to 23 | |
| 43 to 53 |
| Thermal Diffusivity, mm2/s | 4.0 | |
| 44 |
| Thermal Shock Resistance, points | 15 to 16 | |
| 11 to 16 |
Alloy Composition
| Aluminum (Al), % | 0 | |
| 8.3 to 9.7 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 16.5 to 18.5 | |
| 0 |
| Copper (Cu), % | 1.0 to 2.5 | |
| 0 to 0.030 |
| Iron (Fe), % | 62.7 to 72.5 | |
| 0 to 0.0050 |
| Magnesium (Mg), % | 0 | |
| 88.6 to 91.3 |
| Manganese (Mn), % | 5.5 to 9.5 | |
| 0.1 to 0.5 |
| Nickel (Ni), % | 4.5 to 5.5 | |
| 0 to 0.0020 |
| Nitrogen (N), % | 0 to 0.15 | |
| 0 |
| Phosphorus (P), % | 0 to 0.070 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.2 |
| Sulfur (S), % | 0 to 0.010 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0.35 to 1.0 |
| Residuals, % | 0 | |
| 0 to 0.010 |