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AZ92A Magnesium vs. S44800 Stainless Steel

AZ92A magnesium belongs to the magnesium alloys classification, while S44800 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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 AZ92A magnesium and the bottom bar is S44800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 47
210
Elongation at Break, % 2.1 to 6.8
23
Fatigue Strength, MPa 76 to 90
300
Poisson's Ratio 0.29
0.27
Shear Modulus, GPa 18
82
Shear Strength, MPa 97 to 160
370
Tensile Strength: Ultimate (UTS), MPa 170 to 270
590
Tensile Strength: Yield (Proof), MPa 83 to 140
450

Thermal Properties

Latent Heat of Fusion, J/g 350
300
Maximum Temperature: Mechanical, °C 130
1100
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 440
1410
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 44 to 58
17
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11 to 12
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 53 to 62
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 12
19
Density, g/cm3 1.8
7.8
Embodied Carbon, kg CO2/kg material 22
3.8
Embodied Energy, MJ/kg 160
52
Embodied Water, L/kg 980
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 14
120
Resilience: Unit (Modulus of Resilience), kJ/m3 73 to 220
480
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 67
25
Strength to Weight: Axial, points 26 to 41
21
Strength to Weight: Bending, points 38 to 51
20
Thermal Diffusivity, mm2/s 25 to 33
4.6
Thermal Shock Resistance, points 10 to 16
19

Alloy Composition


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Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0 to 0.010
Chromium (Cr), % 0
28 to 30
Copper (Cu), % 0 to 0.25
0 to 0.15
Iron (Fe), % 0
62.6 to 66.5
Magnesium (Mg), % 86.7 to 90
0
Manganese (Mn), % 0.1 to 0.35
0 to 0.3
Molybdenum (Mo), % 0
3.5 to 4.2
Nickel (Ni), % 0 to 0.010
2.0 to 2.5
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.3
0 to 0.2
Sulfur (S), % 0
0 to 0.020
Zinc (Zn), % 1.6 to 2.4
0
Residuals, % 0 to 0.3
0