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ISO-WD32260 Magnesium vs. S17600 Stainless Steel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while S17600 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 S17600 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 6.0
8.6 to 11
Fatigue Strength, MPa 150 to 190
300 to 680
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 190 to 200
560 to 880
Tensile Strength: Ultimate (UTS), MPa 330 to 340
940 to 1490
Tensile Strength: Yield (Proof), MPa 230 to 250
580 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 330
290
Maximum Temperature: Mechanical, °C 120
890
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 520
1390
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 13
13
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 23
2.9
Embodied Energy, MJ/kg 160
42
Embodied Water, L/kg 940
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
70 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
850 to 4390
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 48 to 51
34 to 54
Strength to Weight: Bending, points 56 to 58
28 to 37
Thermal Diffusivity, mm2/s 63
4.1
Thermal Shock Resistance, points 19 to 20
31 to 50

Alloy Composition


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Aluminum (Al), % 0
0 to 0.4
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 17.5
Iron (Fe), % 0
71.3 to 77.6
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0
6.0 to 7.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.4 to 1.2
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0