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ISO-WD32350 Magnesium vs. S36200 Stainless Steel

ISO-WD32350 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 (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 ISO-WD32350 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, % 5.7 to 10
3.4 to 4.6
Fatigue Strength, MPa 120 to 130
450 to 570
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 150 to 170
680 to 810
Tensile Strength: Ultimate (UTS), MPa 250 to 290
1180 to 1410
Tensile Strength: Yield (Proof), MPa 140 to 180
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 340
280
Maximum Temperature: Mechanical, °C 95
820
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 560
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
16
Thermal Expansion, µm/m-K 25
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
12
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 960
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
2380 to 3930
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
42 to 50
Strength to Weight: Bending, points 50 to 55
32 to 36
Thermal Diffusivity, mm2/s 73
4.3
Thermal Shock Resistance, points 16 to 18
40 to 48

Alloy Composition

Aluminum (Al), % 0 to 0.1
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
14 to 14.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
75.4 to 79.5
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
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 0.1
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.6 to 0.9
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0

Comparable Variants