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AISI 422 Stainless Steel vs. AZ63A Magnesium

AISI 422 stainless steel belongs to the iron alloys classification, while AZ63A magnesium belongs to the magnesium 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 AISI 422 stainless steel and the bottom bar is AZ63A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 15 to 17
2.2 to 8.0
Fatigue Strength, MPa 410 to 500
76 to 83
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 560 to 660
110 to 160
Tensile Strength: Ultimate (UTS), MPa 910 to 1080
190 to 270
Tensile Strength: Yield (Proof), MPa 670 to 870
81 to 120

Thermal Properties

Latent Heat of Fusion, J/g 270
350
Maximum Temperature: Mechanical, °C 650
120
Melting Completion (Liquidus), °C 1480
610
Melting Onset (Solidus), °C 1470
450
Specific Heat Capacity, J/kg-K 470
980
Thermal Conductivity, W/m-K 24
52 to 65
Thermal Expansion, µm/m-K 10
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.7
12 to 15
Electrical Conductivity: Equal Weight (Specific), % IACS 5.3
59 to 74

Otherwise Unclassified Properties

Base Metal Price, % relative 11
12
Density, g/cm3 7.9
1.8
Embodied Carbon, kg CO2/kg material 3.1
22
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140 to 150
3.7 to 16
Resilience: Unit (Modulus of Resilience), kJ/m3 1140 to 1910
71 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
66
Strength to Weight: Axial, points 32 to 38
29 to 41
Strength to Weight: Bending, points 26 to 30
40 to 51
Thermal Diffusivity, mm2/s 6.4
29 to 37
Thermal Shock Resistance, points 33 to 39
11 to 16

Alloy Composition


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Aluminum (Al), % 0
5.3 to 6.7
Carbon (C), % 0.2 to 0.25
0
Chromium (Cr), % 11 to 12.5
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 81.9 to 85.8
0
Magnesium (Mg), % 0
88.6 to 92.1
Manganese (Mn), % 0.5 to 1.0
0.15 to 0.35
Molybdenum (Mo), % 0.9 to 1.3
0
Nickel (Ni), % 0.5 to 1.0
0 to 0.010
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.3
Sulfur (S), % 0 to 0.025
0
Tungsten (W), % 0.9 to 1.3
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
2.5 to 3.5
Residuals, % 0
0 to 0.3