ASTM B817 Type I vs. ISO-WD21150 Magnesium
ASTM B817 type I belongs to the titanium alloys classification, while ISO-WD21150 magnesium belongs to the magnesium alloys. There are 28 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 ASTM B817 type I and the bottom bar is ISO-WD21150 magnesium.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 100 | |
| 45 |
| Elongation at Break, % | 4.0 to 13 | |
| 5.7 to 11 |
| Poisson's Ratio | 0.32 | |
| 0.29 |
| Shear Modulus, GPa | 40 | |
| 17 |
| Tensile Strength: Ultimate (UTS), MPa | 770 to 960 | |
| 240 to 290 |
| Tensile Strength: Yield (Proof), MPa | 700 to 860 | |
| 120 to 200 |
Thermal Properties
| Latent Heat of Fusion, J/g | 410 | |
| 350 |
| Maximum Temperature: Mechanical, °C | 340 | |
| 110 |
| Melting Completion (Liquidus), °C | 1600 | |
| 600 |
| Melting Onset (Solidus), °C | 1550 | |
| 550 |
| Specific Heat Capacity, J/kg-K | 560 | |
| 990 |
| Thermal Conductivity, W/m-K | 7.1 | |
| 100 |
| Thermal Expansion, µm/m-K | 9.6 | |
| 27 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.0 | |
| 19 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 2.0 | |
| 100 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 36 | |
| 12 |
| Density, g/cm3 | 4.4 | |
| 1.7 |
| Embodied Carbon, kg CO2/kg material | 38 | |
| 23 |
| Embodied Energy, MJ/kg | 610 | |
| 160 |
| Embodied Water, L/kg | 200 | |
| 980 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 30 to 120 | |
| 15 to 24 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 2310 to 3540 | |
| 160 to 460 |
| Stiffness to Weight: Axial, points | 13 | |
| 15 |
| Stiffness to Weight: Bending, points | 35 | |
| 70 |
| Strength to Weight: Axial, points | 48 to 60 | |
| 40 to 48 |
| Strength to Weight: Bending, points | 42 to 49 | |
| 52 to 58 |
| Thermal Diffusivity, mm2/s | 2.9 | |
| 60 |
| Thermal Shock Resistance, points | 54 to 68 | |
| 15 to 17 |
Alloy Composition
| Aluminum (Al), % | 5.5 to 6.8 | |
| 2.4 to 3.6 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chlorine (Cl), % | 0 to 0.2 | |
| 0 |
| Copper (Cu), % | 0 | |
| 0 to 0.050 |
| Hydrogen (H), % | 0 to 0.015 | |
| 0 |
| Iron (Fe), % | 0 to 0.4 | |
| 0 to 0.0050 |
| Magnesium (Mg), % | 0 | |
| 94 to 97 |
| Manganese (Mn), % | 0 | |
| 0.15 to 0.4 |
| Nickel (Ni), % | 0 | |
| 0 to 0.0050 |
| Nitrogen (N), % | 0 to 0.040 | |
| 0 |
| Oxygen (O), % | 0 to 0.3 | |
| 0 |
| Silicon (Si), % | 0 to 0.1 | |
| 0 to 0.1 |
| Sodium (Na), % | 0 to 0.2 | |
| 0 |
| Titanium (Ti), % | 87 to 91 | |
| 0 |
| Vanadium (V), % | 3.5 to 4.5 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0.5 to 1.5 |
| Residuals, % | 0 | |
| 0 to 0.3 |