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ISO-WD32250 Magnesium vs. S66286 Stainless Steel

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while S66286 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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-WD32250 magnesium and the bottom bar is S66286 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 4.5 to 8.6
17 to 40
Fatigue Strength, MPa 170 to 210
240 to 410
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 17
75
Shear Strength, MPa 180 to 190
420 to 630
Tensile Strength: Ultimate (UTS), MPa 310 to 330
620 to 1020
Tensile Strength: Yield (Proof), MPa 240 to 290
280 to 670

Thermal Properties

Latent Heat of Fusion, J/g 340
300
Maximum Temperature: Mechanical, °C 120
920
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 550
1370
Specific Heat Capacity, J/kg-K 980
470
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 26
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 13
26
Density, g/cm3 1.8
7.9
Embodied Carbon, kg CO2/kg material 24
6.0
Embodied Energy, MJ/kg 160
87
Embodied Water, L/kg 950
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
150 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
190 to 1150
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
24
Strength to Weight: Axial, points 49 to 51
22 to 36
Strength to Weight: Bending, points 58 to 60
20 to 28
Thermal Diffusivity, mm2/s 72
4.0
Thermal Shock Resistance, points 19 to 20
13 to 22

Alloy Composition


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Aluminum (Al), % 0
0 to 0.35
Boron (B), % 0
0.0010 to 0.010
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
13.5 to 16
Iron (Fe), % 0
49.1 to 59.5
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0
24 to 27
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
1.9 to 2.4
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0