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ZK60A Magnesium vs. EN 1.4578 Stainless Steel

ZK60A magnesium belongs to the magnesium alloys classification, while EN 1.4578 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 ZK60A magnesium and the bottom bar is EN 1.4578 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 9.9
51
Fatigue Strength, MPa 150 to 180
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 170 to 190
400
Tensile Strength: Ultimate (UTS), MPa 320 to 330
550
Tensile Strength: Yield (Proof), MPa 230 to 250
200

Thermal Properties

Latent Heat of Fusion, J/g 330
290
Maximum Temperature: Mechanical, °C 120
930
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 550
1390
Specific Heat Capacity, J/kg-K 960
470
Thermal Conductivity, W/m-K 120
14
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29 to 30
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
3.7
Embodied Energy, MJ/kg 160
51
Embodied Water, L/kg 940
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 29
220
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 690
100
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 47 to 49
19
Strength to Weight: Bending, points 55 to 56
19
Thermal Diffusivity, mm2/s 66
3.9
Thermal Shock Resistance, points 19 to 20
12

Alloy Composition


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Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0
16.5 to 17.5
Copper (Cu), % 0
3.0 to 3.5
Iron (Fe), % 0
62.3 to 68.5
Magnesium (Mg), % 92.5 to 94.8
0
Manganese (Mn), % 0
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 2.5
Nickel (Ni), % 0
10 to 11
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 to 0.015
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 1.0
0
Residuals, % 0 to 0.3
0