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EN 1.4462 Stainless Steel vs. ZK60A Magnesium

EN 1.4462 stainless steel belongs to the iron alloys classification, while ZK60A magnesium belongs to the magnesium 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 EN 1.4462 stainless steel and the bottom bar is ZK60A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 26
4.5 to 9.9
Fatigue Strength, MPa 370
150 to 180
Poisson's Ratio 0.27
0.29
Shear Modulus, GPa 80
18
Shear Strength, MPa 500
170 to 190
Tensile Strength: Ultimate (UTS), MPa 780
320 to 330
Tensile Strength: Yield (Proof), MPa 520
230 to 250

Thermal Properties

Latent Heat of Fusion, J/g 300
330
Maximum Temperature: Mechanical, °C 1060
120
Melting Completion (Liquidus), °C 1450
600
Melting Onset (Solidus), °C 1400
550
Specific Heat Capacity, J/kg-K 480
960
Thermal Conductivity, W/m-K 15
120
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
29 to 30
Electrical Conductivity: Equal Weight (Specific), % IACS 2.5
140

Otherwise Unclassified Properties

Base Metal Price, % relative 17
13
Density, g/cm3 7.8
1.9
Embodied Carbon, kg CO2/kg material 3.6
23
Embodied Energy, MJ/kg 49
160
Embodied Water, L/kg 160
940

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
14 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 670
570 to 690
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
63
Strength to Weight: Axial, points 28
47 to 49
Strength to Weight: Bending, points 24
55 to 56
Thermal Diffusivity, mm2/s 4.0
66
Thermal Shock Resistance, points 21
19 to 20

Alloy Composition


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Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 21 to 23
0
Iron (Fe), % 63.7 to 71.9
0
Magnesium (Mg), % 0
92.5 to 94.8
Manganese (Mn), % 0 to 2.0
0
Molybdenum (Mo), % 2.5 to 3.5
0
Nickel (Ni), % 4.5 to 6.5
0
Nitrogen (N), % 0.1 to 0.22
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 1.0
0
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
4.8 to 6.2
Zirconium (Zr), % 0
0.45 to 1.0
Residuals, % 0
0 to 0.3