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EN-MC21110 Magnesium vs. EN 1.4458 Stainless Steel

EN-MC21110 magnesium belongs to the magnesium alloys classification, while EN 1.4458 stainless steel belongs to the iron alloys. There are 30 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 EN-MC21110 magnesium and the bottom bar is EN 1.4458 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 63
150
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.8 to 6.7
34
Fatigue Strength, MPa 75 to 78
150
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Tensile Strength: Ultimate (UTS), MPa 200 to 270
510
Tensile Strength: Yield (Proof), MPa 100 to 120
190

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 600
1420
Melting Onset (Solidus), °C 500
1370
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 80
16
Thermal Expansion, µm/m-K 26
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 61
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
30
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 23
5.4
Embodied Energy, MJ/kg 160
75
Embodied Water, L/kg 990
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
140
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
89
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 33 to 44
17
Strength to Weight: Bending, points 45 to 54
18
Thermal Diffusivity, mm2/s 47
4.2
Thermal Shock Resistance, points 12 to 16
12

Alloy Composition


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Aluminum (Al), % 7.0 to 8.7
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
19 to 22
Copper (Cu), % 0 to 0.030
0 to 2.0
Iron (Fe), % 0 to 0.0050
40.2 to 53
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0 to 0.0020
26 to 30
Nitrogen (N), % 0
0 to 0.2
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0