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ISO-WD32250 Magnesium vs. EN 1.4618 Stainless Steel

ISO-WD32250 magnesium belongs to the magnesium alloys classification, while EN 1.4618 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-WD32250 magnesium and the bottom bar is EN 1.4618 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 4.5 to 8.6
51
Fatigue Strength, MPa 170 to 210
240 to 250
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 180 to 190
480 to 500
Tensile Strength: Ultimate (UTS), MPa 310 to 330
680 to 700
Tensile Strength: Yield (Proof), MPa 240 to 290
250 to 260

Thermal Properties

Latent Heat of Fusion, J/g 340
280
Maximum Temperature: Mechanical, °C 120
900
Melting Completion (Liquidus), °C 600
1400
Melting Onset (Solidus), °C 550
1360
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 13
13
Density, g/cm3 1.8
7.7
Embodied Carbon, kg CO2/kg material 24
2.7
Embodied Energy, MJ/kg 160
39
Embodied Water, L/kg 950
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
270 to 280
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
160 to 170
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
25
Strength to Weight: Axial, points 49 to 51
24 to 25
Strength to Weight: Bending, points 58 to 60
22 to 23
Thermal Diffusivity, mm2/s 72
4.0
Thermal Shock Resistance, points 19 to 20
15 to 16

Alloy Composition


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Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
16.5 to 18.5
Copper (Cu), % 0
1.0 to 2.5
Iron (Fe), % 0
62.7 to 72.5
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
5.5 to 9.5
Nickel (Ni), % 0
4.5 to 5.5
Nitrogen (N), % 0
0 to 0.15
Phosphorus (P), % 0
0 to 0.070
Silicon (Si), % 0
0 to 1.0
Sulfur (S), % 0
0 to 0.010
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0