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AISI 201L Stainless Steel vs. AZ92A Magnesium

AISI 201L stainless steel belongs to the iron alloys classification, while AZ92A 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 201L stainless steel and the bottom bar is AZ92A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
47
Elongation at Break, % 22 to 46
2.1 to 6.8
Fatigue Strength, MPa 270 to 530
76 to 90
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 77
18
Shear Strength, MPa 520 to 660
97 to 160
Tensile Strength: Ultimate (UTS), MPa 740 to 1040
170 to 270
Tensile Strength: Yield (Proof), MPa 290 to 790
83 to 140

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 880
130
Melting Completion (Liquidus), °C 1410
590
Melting Onset (Solidus), °C 1370
440
Specific Heat Capacity, J/kg-K 480
980
Thermal Conductivity, W/m-K 15
44 to 58
Thermal Expansion, µm/m-K 17
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
11 to 12
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
53 to 62

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
160
Embodied Water, L/kg 140
980

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210 to 300
4.0 to 14
Resilience: Unit (Modulus of Resilience), kJ/m3 220 to 1570
73 to 220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
67
Strength to Weight: Axial, points 27 to 37
26 to 41
Strength to Weight: Bending, points 24 to 30
38 to 51
Thermal Diffusivity, mm2/s 4.0
25 to 33
Thermal Shock Resistance, points 16 to 23
10 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 16 to 18
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 67.9 to 75
0
Magnesium (Mg), % 0
86.7 to 90
Manganese (Mn), % 5.5 to 7.5
0.1 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 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.3
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
1.6 to 2.4
Residuals, % 0
0 to 0.3