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EN-MC21210 Magnesium vs. AISI 414 Stainless Steel

EN-MC21210 magnesium belongs to the magnesium alloys classification, while AISI 414 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-MC21210 magnesium and the bottom bar is AISI 414 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 14
17
Fatigue Strength, MPa 70
430 to 480
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 110
550 to 590
Tensile Strength: Ultimate (UTS), MPa 190
900 to 960
Tensile Strength: Yield (Proof), MPa 90
700 to 790

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 100
750
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 570
1400
Specific Heat Capacity, J/kg-K 1000
480
Thermal Conductivity, W/m-K 120
25
Thermal Expansion, µm/m-K 27
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
8.0
Density, g/cm3 1.6
7.8
Embodied Carbon, kg CO2/kg material 24
2.1
Embodied Energy, MJ/kg 160
29
Embodied Water, L/kg 980
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
140 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 92
1260 to 1590
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 72
25
Strength to Weight: Axial, points 32
32 to 34
Strength to Weight: Bending, points 44
27 to 28
Thermal Diffusivity, mm2/s 76
6.7
Thermal Shock Resistance, points 11
33 to 35

Alloy Composition

Aluminum (Al), % 1.6 to 2.6
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 0 to 0.010
0
Iron (Fe), % 0 to 0.0050
81.8 to 87.3
Magnesium (Mg), % 96.3 to 98.3
0
Manganese (Mn), % 0.1 to 0.7
0 to 1.0
Nickel (Ni), % 0 to 0.0020
1.3 to 2.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.010
0