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ISO-WD32260 Magnesium vs. EN 1.4598 Stainless Steel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while EN 1.4598 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 ISO-WD32260 magnesium and the bottom bar is EN 1.4598 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 6.0
46
Fatigue Strength, MPa 150 to 190
210
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 190 to 200
420
Tensile Strength: Ultimate (UTS), MPa 330 to 340
600
Tensile Strength: Yield (Proof), MPa 230 to 250
230

Thermal Properties

Latent Heat of Fusion, J/g 330
290
Maximum Temperature: Mechanical, °C 120
950
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 520
1390
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 27
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 13
19
Density, g/cm3 1.9
7.9
Embodied Carbon, kg CO2/kg material 23
3.8
Embodied Energy, MJ/kg 160
52
Embodied Water, L/kg 940
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
220
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
130
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 48 to 51
21
Strength to Weight: Bending, points 56 to 58
20
Thermal Diffusivity, mm2/s 63
4.1
Thermal Shock Resistance, points 19 to 20
14

Alloy Composition


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Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16.5 to 18.5
Copper (Cu), % 0
1.3 to 1.8
Iron (Fe), % 0
60.8 to 70.1
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0
10 to 13
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0
0 to 1.0
Sulfur (S), % 0
0.1 to 0.2
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0