ISO-WD32350 Magnesium vs. Type 2 Magnetic Alloy
ISO-WD32350 magnesium belongs to the magnesium alloys classification, while Type 2 magnetic alloy belongs to the iron alloys. There are 25 material properties with values for both materials. Properties with values for just one material (6, 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 ISO-WD32350 magnesium and the bottom bar is Type 2 magnetic alloy.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 45 | |
190 |
Elongation at Break, % | 5.7 to 10 | |
2.0 to 38 |
Poisson's Ratio | 0.29 | |
0.3 |
Shear Modulus, GPa | 18 | |
72 |
Tensile Strength: Ultimate (UTS), MPa | 250 to 290 | |
510 to 910 |
Tensile Strength: Yield (Proof), MPa | 140 to 180 | |
260 to 870 |
Thermal Properties
Latent Heat of Fusion, J/g | 340 | |
270 |
Melting Completion (Liquidus), °C | 600 | |
1420 |
Melting Onset (Solidus), °C | 560 | |
1370 |
Specific Heat Capacity, J/kg-K | 990 | |
460 |
Thermal Expansion, µm/m-K | 25 | |
12 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 25 | |
3.9 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 130 | |
4.2 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 12 | |
33 |
Density, g/cm3 | 1.7 | |
8.4 |
Embodied Carbon, kg CO2/kg material | 23 | |
5.9 |
Embodied Energy, MJ/kg | 160 | |
81 |
Embodied Water, L/kg | 960 | |
140 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 14 to 23 | |
18 to 160 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 210 to 380 | |
170 to 2010 |
Stiffness to Weight: Axial, points | 15 | |
12 |
Stiffness to Weight: Bending, points | 68 | |
23 |
Strength to Weight: Axial, points | 39 to 46 | |
17 to 30 |
Strength to Weight: Bending, points | 50 to 55 | |
17 to 25 |
Thermal Shock Resistance, points | 16 to 18 | |
16 to 29 |
Alloy Composition
Aluminum (Al), % | 0 to 0.1 | |
0 |
Carbon (C), % | 0 | |
0 to 0.050 |
Chromium (Cr), % | 0 | |
0 to 0.3 |
Cobalt (Co), % | 0 | |
0 to 0.5 |
Copper (Cu), % | 0 to 0.1 | |
0 to 0.3 |
Iron (Fe), % | 0 to 0.060 | |
48.2 to 53 |
Magnesium (Mg), % | 95.7 to 97.7 | |
0 |
Manganese (Mn), % | 0.6 to 1.3 | |
0 to 0.8 |
Molybdenum (Mo), % | 0 | |
0 to 0.3 |
Nickel (Ni), % | 0 to 0.0050 | |
47 to 49 |
Phosphorus (P), % | 0 | |
0 to 0.010 |
Silicon (Si), % | 0 to 0.1 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.030 |
Zinc (Zn), % | 1.8 to 2.3 | |
0 |
Residuals, % | 0 to 0.3 | |
0 |