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ISO-WD43150 Magnesium vs. ASTM A387 Grade 9 Steel

ISO-WD43150 magnesium belongs to the magnesium alloys classification, while ASTM A387 grade 9 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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-WD43150 magnesium and the bottom bar is ASTM A387 grade 9 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 2.8
20 to 21
Fatigue Strength, MPa 100
160 to 240
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
75
Shear Strength, MPa 140
310 to 380
Tensile Strength: Ultimate (UTS), MPa 250
500 to 600
Tensile Strength: Yield (Proof), MPa 150
230 to 350

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 95
600
Melting Completion (Liquidus), °C 610
1460
Melting Onset (Solidus), °C 590
1410
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 140
26
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
9.0
Electrical Conductivity: Equal Weight (Specific), % IACS 170
10

Otherwise Unclassified Properties

Base Metal Price, % relative 12
6.5
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 24
2.1
Embodied Energy, MJ/kg 160
28
Embodied Water, L/kg 970
87

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.1
83 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 250
140 to 310
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
25
Strength to Weight: Axial, points 41
18 to 21
Strength to Weight: Bending, points 52
18 to 20
Thermal Diffusivity, mm2/s 81
6.9
Thermal Shock Resistance, points 14
14 to 17

Alloy Composition

Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
8.0 to 10
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0
87.1 to 90.8
Magnesium (Mg), % 97.5 to 98.8
0
Manganese (Mn), % 1.2 to 2.0
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.010
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.025
Vanadium (V), % 0
0 to 0.040
Residuals, % 0 to 0.3
0