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ISO-WD21150 Magnesium vs. EN 1.4578 Stainless Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while EN 1.4578 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 1.4578 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 11
51
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 150 to 170
400
Tensile Strength: Ultimate (UTS), MPa 240 to 290
550
Tensile Strength: Yield (Proof), MPa 120 to 200
200

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 110
930
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 550
1390
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 100
14
Thermal Expansion, µm/m-K 27
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
19
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 23
3.7
Embodied Energy, MJ/kg 160
51
Embodied Water, L/kg 980
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
220
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
100
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 70
25
Strength to Weight: Axial, points 40 to 48
19
Strength to Weight: Bending, points 52 to 58
19
Thermal Diffusivity, mm2/s 60
3.9
Thermal Shock Resistance, points 15 to 17
12

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0
16.5 to 17.5
Copper (Cu), % 0 to 0.050
3.0 to 3.5
Iron (Fe), % 0 to 0.0050
62.3 to 68.5
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0 to 0.0050
10 to 11
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
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