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EN-MC65220 Magnesium vs. EN 1.4310 Stainless Steel

EN-MC65220 magnesium belongs to the magnesium alloys classification, while EN 1.4310 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-MC65220 magnesium and the bottom bar is EN 1.4310 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
200 to 270
Elastic (Young's, Tensile) Modulus, GPa 44
200
Elongation at Break, % 2.2
14 to 45
Fatigue Strength, MPa 110
240 to 330
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 150
510 to 550
Tensile Strength: Ultimate (UTS), MPa 270
730 to 900
Tensile Strength: Yield (Proof), MPa 200
260 to 570

Thermal Properties

Latent Heat of Fusion, J/g 340
290
Maximum Temperature: Mechanical, °C 160
910
Melting Completion (Liquidus), °C 610
1420
Melting Onset (Solidus), °C 550
1380
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 26
18

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 80
14
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 27
2.9
Embodied Energy, MJ/kg 210
42

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.5
110 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 450
170 to 830
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 62
25
Strength to Weight: Axial, points 40
26 to 32
Strength to Weight: Bending, points 49
23 to 27
Thermal Diffusivity, mm2/s 61
4.0
Thermal Shock Resistance, points 17
15 to 18

Alloy Composition

Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
16 to 19
Copper (Cu), % 0.050 to 0.1
0
Iron (Fe), % 0 to 0.010
66.4 to 78
Magnesium (Mg), % 93.8 to 96.8
0
Manganese (Mn), % 0 to 0.15
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.8
Nickel (Ni), % 0 to 0.0050
6.0 to 9.5
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.010
0 to 2.0
Silver (Ag), % 1.3 to 1.7
0
Sulfur (S), % 0
0 to 0.015
Unspecified Rare Earths, % 1.5 to 3.0
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0