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EN-MC95310 Magnesium vs. S36200 Stainless Steel

EN-MC95310 magnesium belongs to the magnesium alloys classification, while S36200 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-MC95310 magnesium and the bottom bar is S36200 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 2.2
3.4 to 4.6
Fatigue Strength, MPa 110
450 to 570
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
76
Shear Strength, MPa 160
680 to 810
Tensile Strength: Ultimate (UTS), MPa 280
1180 to 1410
Tensile Strength: Yield (Proof), MPa 190
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 170
820
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 540
1400
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 51
16
Thermal Expansion, µm/m-K 25
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 50
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 34
12
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 29
2.8
Embodied Energy, MJ/kg 260
40
Embodied Water, L/kg 900
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.6
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 420
2380 to 3930
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 61
25
Strength to Weight: Axial, points 40
42 to 50
Strength to Weight: Bending, points 49
32 to 36
Thermal Diffusivity, mm2/s 28
4.3
Thermal Shock Resistance, points 18
40 to 48

Alloy Composition


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Aluminum (Al), % 0
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
14 to 14.5
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.010
75.4 to 79.5
Lithium (Li), % 0 to 0.2
0
Magnesium (Mg), % 88.9 to 93.4
0
Manganese (Mn), % 0 to 0.15
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0 to 0.0050
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.010
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.6 to 0.9
Unspecified Rare Earths, % 1.5 to 4.0
0
Yttrium (Y), % 4.8 to 5.5
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0.4 to 1.0
0
Residuals, % 0 to 0.010
0