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ISO-WD21150 Magnesium vs. EN 1.4113 Stainless Steel

ISO-WD21150 magnesium belongs to the magnesium alloys classification, while EN 1.4113 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1.4113 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 11
20
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
78
Shear Strength, MPa 150 to 170
340
Tensile Strength: Ultimate (UTS), MPa 240 to 290
540
Tensile Strength: Yield (Proof), MPa 120 to 200
310

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 110
880
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 550
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 100
25
Thermal Expansion, µm/m-K 27
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 19
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.5
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
2.4
Embodied Energy, MJ/kg 160
33
Embodied Water, L/kg 980
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 24
94
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 460
240
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
6.7
Thermal Shock Resistance, points 15 to 17
20

Alloy Composition

Aluminum (Al), % 2.4 to 3.6
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.0050
78.5 to 83.1
Magnesium (Mg), % 94 to 97
0
Manganese (Mn), % 0.15 to 0.4
0 to 1.0
Molybdenum (Mo), % 0
0.9 to 1.4
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