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EN-MC21120 Magnesium vs. AISI 440A Stainless Steel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while AISI 440A stainless steel belongs to the iron alloys. There are 29 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-MC21120 magnesium and the bottom bar is AISI 440A stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 6.7
5.0 to 20
Fatigue Strength, MPa 84 to 96
270 to 790
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 110 to 160
450 to 1040
Tensile Strength: Ultimate (UTS), MPa 200 to 270
730 to 1790
Tensile Strength: Yield (Proof), MPa 130 to 170
420 to 1650

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 130
760
Melting Completion (Liquidus), °C 600
1480
Melting Onset (Solidus), °C 490
1370
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 76
23
Thermal Expansion, µm/m-K 26
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.0
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 22
2.2
Embodied Energy, MJ/kg 160
31
Embodied Water, L/kg 990
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
87 to 120
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 31 to 43
26 to 65
Strength to Weight: Bending, points 43 to 53
23 to 43
Thermal Diffusivity, mm2/s 44
6.2
Thermal Shock Resistance, points 11 to 16
26 to 65

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0.6 to 0.75
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
78.4 to 83.4
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 1.0
Molybdenum (Mo), % 0
0 to 0.75
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