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ISO-WD21150 Magnesium vs. EN 1.4024 Stainless Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while EN 1.4024 stainless 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 EN 1.4024 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 11
15 to 22
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 150 to 170
370 to 460
Tensile Strength: Ultimate (UTS), MPa 240 to 290
590 to 750
Tensile Strength: Yield (Proof), MPa 120 to 200
330 to 510

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 110
760
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 550
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 100
30
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
7.0
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
1.9
Embodied Energy, MJ/kg 160
27
Embodied Water, L/kg 980
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
98 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
280 to 660
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 40 to 48
21 to 27
Strength to Weight: Bending, points 52 to 58
20 to 24
Thermal Diffusivity, mm2/s 60
8.1
Thermal Shock Resistance, points 15 to 17
21 to 26

Alloy Composition


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Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0.12 to 0.17
Chromium (Cr), % 0
12 to 14
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
83.8 to 87.9
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.0
Nickel (Ni), % 0 to 0.0050
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0.5 to 1.5
0
Residuals, % 0 to 0.3
0

Comparable Variants