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ISO-WD32260 Magnesium vs. AISI 201L Stainless Steel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while AISI 201L stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 ISO-WD32260 magnesium and the bottom bar is AISI 201L stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 4.5 to 6.0
22 to 46
Fatigue Strength, MPa 150 to 190
270 to 530
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 190 to 200
520 to 660
Tensile Strength: Ultimate (UTS), MPa 330 to 340
740 to 1040
Tensile Strength: Yield (Proof), MPa 230 to 250
290 to 790

Thermal Properties

Latent Heat of Fusion, J/g 330
280
Maximum Temperature: Mechanical, °C 120
880
Melting Completion (Liquidus), °C 600
1410
Melting Onset (Solidus), °C 520
1370
Specific Heat Capacity, J/kg-K 970
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 140
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 13
12
Density, g/cm3 1.9
7.7
Embodied Carbon, kg CO2/kg material 23
2.6
Embodied Energy, MJ/kg 160
38
Embodied Water, L/kg 940
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
210 to 300
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
220 to 1570
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 63
25
Strength to Weight: Axial, points 48 to 51
27 to 37
Strength to Weight: Bending, points 56 to 58
24 to 30
Thermal Diffusivity, mm2/s 63
4.0
Thermal Shock Resistance, points 19 to 20
16 to 23

Alloy Composition

Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16 to 18
Iron (Fe), % 0
67.9 to 75
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
5.5 to 7.5
Nickel (Ni), % 0
3.5 to 5.5
Nitrogen (N), % 0
0 to 0.25
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0