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AZ63A Magnesium vs. S36200 Stainless Steel

AZ63A 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 (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 AZ63A 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, % 2.2 to 8.0
3.4 to 4.6
Fatigue Strength, MPa 76 to 83
450 to 570
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 110 to 160
680 to 810
Tensile Strength: Ultimate (UTS), MPa 190 to 270
1180 to 1410
Tensile Strength: Yield (Proof), MPa 81 to 120
960 to 1240

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 120
820
Melting Completion (Liquidus), °C 610
1440
Melting Onset (Solidus), °C 450
1400
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 52 to 65
16
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
12
Density, g/cm3 1.8
7.8
Embodied Carbon, kg CO2/kg material 22
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 970
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
46 to 51
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
2380 to 3930
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 66
25
Strength to Weight: Axial, points 29 to 41
42 to 50
Strength to Weight: Bending, points 40 to 51
32 to 36
Thermal Diffusivity, mm2/s 29 to 37
4.3
Thermal Shock Resistance, points 11 to 16
40 to 48

Alloy Composition


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Aluminum (Al), % 5.3 to 6.7
0 to 0.1
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
14 to 14.5
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0
75.4 to 79.5
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0 to 0.5
Molybdenum (Mo), % 0
0 to 0.3
Nickel (Ni), % 0 to 0.010
6.5 to 7.0
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.3
0 to 0.3
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0.6 to 0.9
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0