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ISO-WD32260 Magnesium vs. SAE-AISI D2 Steel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while SAE-AISI D2 steel belongs to the iron alloys. There are 29 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-WD32260 magnesium and the bottom bar is SAE-AISI D2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 4.5 to 6.0
5.0 to 16
Fatigue Strength, MPa 150 to 190
310 to 860
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
75
Shear Strength, MPa 190 to 200
460 to 1160
Tensile Strength: Ultimate (UTS), MPa 330 to 340
760 to 2000
Tensile Strength: Yield (Proof), MPa 230 to 250
470 to 1510

Thermal Properties

Latent Heat of Fusion, J/g 330
270
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 520
1390
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 110
31
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
4.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
5.1

Otherwise Unclassified Properties

Base Metal Price, % relative 13
8.0
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 23
3.4
Embodied Energy, MJ/kg 160
50
Embodied Water, L/kg 940
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
92 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
570 to 5940
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 48 to 51
27 to 72
Strength to Weight: Bending, points 56 to 58
24 to 46
Thermal Diffusivity, mm2/s 63
8.3
Thermal Shock Resistance, points 19 to 20
25 to 67

Alloy Composition

Carbon (C), % 0
1.4 to 1.6
Chromium (Cr), % 0
11 to 13
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 0
81.3 to 86.9
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0 to 0.6
Molybdenum (Mo), % 0
0.7 to 1.2
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Vanadium (V), % 0
0 to 1.1
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0