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AISI 201 Stainless Steel vs. AZ63A Magnesium

AISI 201 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 (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 AISI 201 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, % 4.6 to 51
2.2 to 8.0
Fatigue Strength, MPa 280 to 600
76 to 83
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 77
18
Shear Strength, MPa 450 to 840
110 to 160
Tensile Strength: Ultimate (UTS), MPa 650 to 1450
190 to 270
Tensile Strength: Yield (Proof), MPa 300 to 1080
81 to 120

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 880
120
Melting Completion (Liquidus), °C 1410
610
Melting Onset (Solidus), °C 1370
450
Specific Heat Capacity, J/kg-K 480
980
Thermal Conductivity, W/m-K 15
52 to 65
Thermal Expansion, µm/m-K 17
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
12 to 15
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
59 to 74

Otherwise Unclassified Properties

Base Metal Price, % relative 12
12
Density, g/cm3 7.7
1.8
Embodied Carbon, kg CO2/kg material 2.6
22
Embodied Energy, MJ/kg 38
150
Embodied Water, L/kg 140
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 61 to 340
3.7 to 16
Resilience: Unit (Modulus of Resilience), kJ/m3 230 to 2970
71 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
66
Strength to Weight: Axial, points 23 to 52
29 to 41
Strength to Weight: Bending, points 22 to 37
40 to 51
Thermal Diffusivity, mm2/s 4.0
29 to 37
Thermal Shock Resistance, points 14 to 32
11 to 16

Alloy Composition

Aluminum (Al), % 0
5.3 to 6.7
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 67.5 to 75
0
Magnesium (Mg), % 0
88.6 to 92.1
Manganese (Mn), % 5.5 to 7.5
0.15 to 0.35
Nickel (Ni), % 3.5 to 5.5
0 to 0.010
Nitrogen (N), % 0 to 0.25
0
Phosphorus (P), % 0 to 0.060
0
Silicon (Si), % 0 to 1.0
0 to 0.3
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
2.5 to 3.5
Residuals, % 0
0 to 0.3