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ISO-WD21150 Magnesium vs. SAE-AISI 1146 Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while SAE-AISI 1146 steel belongs to the iron alloys. There are 29 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 ISO-WD21150 magnesium and the bottom bar is SAE-AISI 1146 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 11
13 to 17
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
72
Shear Strength, MPa 150 to 170
410 to 440
Tensile Strength: Ultimate (UTS), MPa 240 to 290
670 to 730
Tensile Strength: Yield (Proof), MPa 120 to 200
360 to 630

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 110
400
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 550
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
51
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
1.8
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
1.4
Embodied Energy, MJ/kg 160
18
Embodied Water, L/kg 980
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
93 to 97
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
340 to 1050
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 40 to 48
24 to 26
Strength to Weight: Bending, points 52 to 58
22 to 23
Thermal Diffusivity, mm2/s 60
14
Thermal Shock Resistance, points 15 to 17
20 to 22

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0.42 to 0.49
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
98.3 to 98.8
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0.7 to 1.0
Nickel (Ni), % 0 to 0.0050
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0
Sulfur (S), % 0
0.080 to 0.13
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0