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EN-MC21220 Magnesium vs. EN 1.4923 Stainless Steel

EN-MC21220 magnesium belongs to the magnesium alloys classification, while EN 1.4923 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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-MC21220 magnesium and the bottom bar is EN 1.4923 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 11
12 to 21
Fatigue Strength, MPa 89
300 to 440
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 120
540 to 590
Tensile Strength: Ultimate (UTS), MPa 210
870 to 980
Tensile Strength: Yield (Proof), MPa 120
470 to 780

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 120
740
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 1000
480
Thermal Conductivity, W/m-K 65
24
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 16
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 87
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
8.0
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
2.9
Embodied Energy, MJ/kg 160
41
Embodied Water, L/kg 990
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20
110 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 160
570 to 1580
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
25
Strength to Weight: Axial, points 34
31 to 35
Strength to Weight: Bending, points 46
26 to 28
Thermal Diffusivity, mm2/s 39
6.5
Thermal Shock Resistance, points 12
30 to 34

Alloy Composition


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Aluminum (Al), % 4.4 to 5.5
0
Carbon (C), % 0
0.18 to 0.24
Chromium (Cr), % 0
11 to 12.5
Copper (Cu), % 0 to 0.010
0
Iron (Fe), % 0 to 0.0050
83.5 to 87.1
Magnesium (Mg), % 93.5 to 95.5
0
Manganese (Mn), % 0.1 to 0.6
0.4 to 0.9
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0 to 0.0020
0.3 to 0.8
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.25 to 0.35
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.010
0