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EN-MC21110 Magnesium vs. EN 1.4419 Stainless Steel

EN-MC21110 magnesium belongs to the magnesium alloys classification, while EN 1.4419 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-MC21110 magnesium and the bottom bar is EN 1.4419 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.8 to 6.7
11 to 17
Fatigue Strength, MPa 75 to 78
230 to 680
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 120 to 160
410 to 950
Tensile Strength: Ultimate (UTS), MPa 200 to 270
660 to 1590
Tensile Strength: Yield (Proof), MPa 100 to 120
370 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 130
790
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 500
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 80
30
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
2.8
Electrical Conductivity: Equal Weight (Specific), % IACS 61
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
8.0
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
2.2
Embodied Energy, MJ/kg 160
30
Embodied Water, L/kg 990
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 14
95 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 120 to 150
350 to 3920
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 33 to 44
24 to 57
Strength to Weight: Bending, points 45 to 54
22 to 39
Thermal Diffusivity, mm2/s 47
8.1
Thermal Shock Resistance, points 12 to 16
23 to 55

Alloy Composition

Aluminum (Al), % 7.0 to 8.7
0
Carbon (C), % 0
0.36 to 0.42
Chromium (Cr), % 0
13 to 14.5
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
82 to 86
Magnesium (Mg), % 89.6 to 92.6
0
Manganese (Mn), % 0.1 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
0.6 to 1.0
Nickel (Ni), % 0 to 0.0020
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0