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ISO-WD32260 Magnesium vs. S66286 Stainless Steel

ISO-WD32260 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-WD32260 magnesium and the bottom bar is S66286 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 4.5 to 6.0
17 to 40
Fatigue Strength, MPa 150 to 190
240 to 410
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
75
Shear Strength, MPa 190 to 200
420 to 630
Tensile Strength: Ultimate (UTS), MPa 330 to 340
620 to 1020
Tensile Strength: Yield (Proof), MPa 230 to 250
280 to 670

Thermal Properties

Latent Heat of Fusion, J/g 330
300
Maximum Temperature: Mechanical, °C 120
920
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 520
1370
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 13
26
Density, g/cm3 1.9
7.9
Embodied Carbon, kg CO2/kg material 23
6.0
Embodied Energy, MJ/kg 160
87
Embodied Water, L/kg 940
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
150 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
190 to 1150
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
24
Strength to Weight: Axial, points 48 to 51
22 to 36
Strength to Weight: Bending, points 56 to 58
20 to 28
Thermal Diffusivity, mm2/s 63
4.0
Thermal Shock Resistance, points 19 to 20
13 to 22

Alloy Composition

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), % 92.7 to 94.8
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), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0