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EN-MC65120 Magnesium vs. EN 1.4110 Stainless Steel

EN-MC65120 magnesium belongs to the magnesium alloys classification, while EN 1.4110 stainless steel belongs to the iron alloys. There are 30 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 EN-MC65120 magnesium and the bottom bar is EN 1.4110 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 3.1
11 to 14
Fatigue Strength, MPa 80
250 to 730
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 92
470 to 1030
Tensile Strength: Ultimate (UTS), MPa 160
770 to 1720
Tensile Strength: Yield (Proof), MPa 110
430 to 1330

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 180
790
Melting Completion (Liquidus), °C 590
1440
Melting Onset (Solidus), °C 520
1400
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 100
30
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.8
Electrical Conductivity: Equal Weight (Specific), % IACS 120
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 25
8.0
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 25
2.3
Embodied Energy, MJ/kg 190
33
Embodied Water, L/kg 930
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.4
90 to 180
Resilience: Unit (Modulus of Resilience), kJ/m3 140
480 to 4550
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 23
28 to 62
Strength to Weight: Bending, points 34
24 to 41
Thermal Diffusivity, mm2/s 56
8.1
Thermal Shock Resistance, points 9.8
27 to 60

Alloy Composition

Carbon (C), % 0
0.48 to 0.6
Chromium (Cr), % 0
13 to 15
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.010
81.4 to 86
Magnesium (Mg), % 91.8 to 95.1
0
Manganese (Mn), % 0 to 0.15
0 to 1.0
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0 to 0.0050
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.010
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Unspecified Rare Earths, % 2.5 to 4.0
0
Vanadium (V), % 0
0 to 0.15
Zinc (Zn), % 2.0 to 3.0
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0