AZ91E Magnesium vs. EN 1.4646 Stainless Steel
AZ91E magnesium belongs to the magnesium alloys classification, while EN 1.4646 stainless steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (9, 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 AZ91E magnesium and the bottom bar is EN 1.4646 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 75 | |
| 220 |
| Elastic (Young's, Tensile) Modulus, GPa | 46 | |
| 200 |
| Elongation at Break, % | 2.5 to 6.2 | |
| 34 |
| Fatigue Strength, MPa | 81 to 85 | |
| 340 |
| Impact Strength: V-Notched Charpy, J | 0.79 to 2.8 | |
| 90 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 18 | |
| 77 |
| Shear Strength, MPa | 89 to 150 | |
| 500 |
| Tensile Strength: Ultimate (UTS), MPa | 160 to 260 | |
| 750 |
| Tensile Strength: Yield (Proof), MPa | 96 to 130 | |
| 430 |
Thermal Properties
| Latent Heat of Fusion, J/g | 350 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 130 | |
| 910 |
| Melting Completion (Liquidus), °C | 600 | |
| 1390 |
| Melting Onset (Solidus), °C | 500 | |
| 1340 |
| Specific Heat Capacity, J/kg-K | 990 | |
| 480 |
| Thermal Expansion, µm/m-K | 27 | |
| 17 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 12 | |
| 13 |
| Density, g/cm3 | 1.7 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 22 | |
| 2.8 |
| Embodied Energy, MJ/kg | 160 | |
| 41 |
| Embodied Water, L/kg | 990 | |
| 160 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 3.4 to 12 | |
| 220 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 100 to 190 | |
| 460 |
| Stiffness to Weight: Axial, points | 15 | |
| 14 |
| Stiffness to Weight: Bending, points | 69 | |
| 25 |
| Strength to Weight: Axial, points | 25 to 42 | |
| 27 |
| Strength to Weight: Bending, points | 37 to 53 | |
| 24 |
| Thermal Shock Resistance, points | 9.0 to 15 | |
| 16 |
Alloy Composition
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| Aluminum (Al), % | 8.1 to 9.3 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.020 to 0.1 |
| Chromium (Cr), % | 0 | |
| 17 to 19 |
| Copper (Cu), % | 0 to 0.015 | |
| 1.5 to 3.0 |
| Iron (Fe), % | 0 to 0.0050 | |
| 59 to 67.3 |
| Magnesium (Mg), % | 88.8 to 91.3 | |
| 0 |
| Manganese (Mn), % | 0.17 to 0.35 | |
| 10.5 to 12.5 |
| Molybdenum (Mo), % | 0 | |
| 0 to 0.5 |
| Nickel (Ni), % | 0 to 0.0010 | |
| 3.5 to 4.5 |
| Nitrogen (N), % | 0 | |
| 0.2 to 0.3 |
| Phosphorus (P), % | 0 | |
| 0 to 0.050 |
| Silicon (Si), % | 0 to 0.2 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Zinc (Zn), % | 0.4 to 1.0 | |
| 0 |
| Residuals, % | 0 to 0.3 | |
| 0 |