EN-MC21320 Magnesium vs. AISI 440C Stainless Steel
EN-MC21320 magnesium belongs to the magnesium alloys classification, while AISI 440C stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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-MC21320 magnesium and the bottom bar is AISI 440C stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 45 | |
| 200 |
| Elongation at Break, % | 7.5 | |
| 2.0 to 14 |
| Fatigue Strength, MPa | 95 | |
| 260 to 840 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 18 | |
| 76 |
| Shear Strength, MPa | 130 | |
| 430 to 1120 |
| Tensile Strength: Ultimate (UTS), MPa | 230 | |
| 710 to 1970 |
| Tensile Strength: Yield (Proof), MPa | 140 | |
| 450 to 1900 |
Thermal Properties
| Latent Heat of Fusion, J/g | 370 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 110 | |
| 870 |
| Melting Completion (Liquidus), °C | 600 | |
| 1480 |
| Melting Onset (Solidus), °C | 530 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 1000 | |
| 480 |
| Thermal Conductivity, W/m-K | 66 | |
| 22 |
| Thermal Expansion, µm/m-K | 26 | |
| 10 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 17 | |
| 2.4 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 91 | |
| 2.8 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 9.0 |
| Density, g/cm3 | 1.6 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 23 | |
| 2.2 |
| Embodied Energy, MJ/kg | 160 | |
| 31 |
| Embodied Water, L/kg | 980 | |
| 120 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 15 | |
| 39 to 88 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 72 | |
| 25 |
| Strength to Weight: Axial, points | 38 | |
| 26 to 71 |
| Strength to Weight: Bending, points | 50 | |
| 23 to 46 |
| Thermal Diffusivity, mm2/s | 40 | |
| 6.0 |
| Thermal Shock Resistance, points | 13 | |
| 26 to 71 |
Alloy Composition
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| Aluminum (Al), % | 3.5 to 5.0 | |
| 0 |
| Carbon (C), % | 0 | |
| 1.0 to 1.2 |
| Chromium (Cr), % | 0 | |
| 16 to 18 |
| Copper (Cu), % | 0 to 0.010 | |
| 0 |
| Iron (Fe), % | 0 to 0.0050 | |
| 78 to 83.1 |
| Magnesium (Mg), % | 92.5 to 95.9 | |
| 0 |
| Manganese (Mn), % | 0.1 to 0.7 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.75 |
| Nickel (Ni), % | 0 to 0.0020 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 0.5 to 1.5 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Zinc (Zn), % | 0 to 0.2 | |
| 0 |
| Residuals, % | 0 to 0.010 | |
| 0 |