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EN-MC95320 Magnesium vs. EN 1.4122 Stainless Steel

EN-MC95320 magnesium belongs to the magnesium alloys classification, while EN 1.4122 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-MC95320 magnesium and the bottom bar is EN 1.4122 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
200
Elongation at Break, % 2.2
14
Fatigue Strength, MPa 110
260 to 360
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 140
480 to 520
Tensile Strength: Ultimate (UTS), MPa 250
790 to 850
Tensile Strength: Yield (Proof), MPa 190
450 to 630

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 180
870
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 530
1400
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 52
15
Thermal Expansion, µm/m-K 25
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 53
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 34
9.5
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 28
2.4
Embodied Energy, MJ/kg 250
33
Embodied Water, L/kg 910
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.1
93 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 420
520 to 1000
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 61
25
Strength to Weight: Axial, points 36
28 to 31
Strength to Weight: Bending, points 45
25 to 26
Thermal Diffusivity, mm2/s 28
4.0
Thermal Shock Resistance, points 16
28 to 30

Alloy Composition


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Carbon (C), % 0
0.33 to 0.45
Chromium (Cr), % 0
15.5 to 17.5
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.010
77.2 to 83.4
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 89.7 to 93.5
0
Manganese (Mn), % 0 to 0.15
0 to 1.5
Molybdenum (Mo), % 0
0.8 to 1.3
Nickel (Ni), % 0 to 0.0050
0 to 1.0
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, % 2.4 to 4.4
0
Yttrium (Y), % 3.7 to 4.3
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0