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ISO-WD21150 Magnesium vs. SAE-AISI 1090 Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while SAE-AISI 1090 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 1090 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 11
11
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
72
Shear Strength, MPa 150 to 170
470 to 570
Tensile Strength: Ultimate (UTS), MPa 240 to 290
790 to 950
Tensile Strength: Yield (Proof), MPa 120 to 200
520 to 610

Thermal Properties

Latent Heat of Fusion, J/g 350
240
Maximum Temperature: Mechanical, °C 110
400
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
50
Thermal Expansion, µm/m-K 27
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.2

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
19
Embodied Water, L/kg 980
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
82 to 91
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
730 to 1000
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 40 to 48
28 to 34
Strength to Weight: Bending, points 52 to 58
24 to 27
Thermal Diffusivity, mm2/s 60
13
Thermal Shock Resistance, points 15 to 17
25 to 31

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0.85 to 1.0
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
98 to 98.6
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0.6 to 0.9
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 to 0.050
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0