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AZ63A Magnesium vs. S31100 Stainless Steel

AZ63A magnesium belongs to the magnesium alloys classification, while S31100 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 S31100 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 8.0
4.5
Fatigue Strength, MPa 76 to 83
330
Poisson's Ratio 0.29
0.27
Shear Modulus, GPa 18
79
Shear Strength, MPa 110 to 160
580
Tensile Strength: Ultimate (UTS), MPa 190 to 270
1000
Tensile Strength: Yield (Proof), MPa 81 to 120
710

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 120
1100
Melting Completion (Liquidus), °C 610
1420
Melting Onset (Solidus), °C 450
1380
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 52 to 65
16
Thermal Expansion, µm/m-K 26
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12 to 15
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 59 to 74
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
16
Density, g/cm3 1.8
7.7
Embodied Carbon, kg CO2/kg material 22
3.1
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 970
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.7 to 16
40
Resilience: Unit (Modulus of Resilience), kJ/m3 71 to 160
1240
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 66
25
Strength to Weight: Axial, points 29 to 41
36
Strength to Weight: Bending, points 40 to 51
29
Thermal Diffusivity, mm2/s 29 to 37
4.2
Thermal Shock Resistance, points 11 to 16
28

Alloy Composition


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Aluminum (Al), % 5.3 to 6.7
0
Carbon (C), % 0
0 to 0.060
Chromium (Cr), % 0
25 to 27
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0
63.6 to 69
Magnesium (Mg), % 88.6 to 92.1
0
Manganese (Mn), % 0.15 to 0.35
0 to 1.0
Nickel (Ni), % 0 to 0.010
6.0 to 7.0
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.3
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 2.5 to 3.5
0
Residuals, % 0 to 0.3
0