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ZK60A Magnesium vs. S36200 Stainless Steel

ZK60A magnesium belongs to the magnesium alloys classification, while S36200 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 S36200 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 4.5 to 9.9
3.4 to 4.6
Fatigue Strength, MPa 150 to 180
450 to 570
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 170 to 190
680 to 810
Tensile Strength: Ultimate (UTS), MPa 320 to 330
1180 to 1410
Tensile Strength: Yield (Proof), MPa 230 to 250
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 120
820
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 550
1400
Specific Heat Capacity, J/kg-K 960
480
Thermal Conductivity, W/m-K 120
16
Thermal Expansion, µm/m-K 26
11

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
12
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 23
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 940
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 29
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 690
2380 to 3930
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 47 to 49
42 to 50
Strength to Weight: Bending, points 55 to 56
32 to 36
Thermal Diffusivity, mm2/s 66
4.3
Thermal Shock Resistance, points 19 to 20
40 to 48

Alloy Composition

Aluminum (Al), % 0
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
14 to 14.5
Iron (Fe), % 0
75.4 to 79.5
Magnesium (Mg), % 92.5 to 94.8
0
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.6 to 0.9
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 1.0
0
Residuals, % 0 to 0.3
0