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ISO-WD32350 Magnesium vs. S44330 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while S44330 stainless steel belongs to the iron 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 ISO-WD32350 magnesium and the bottom bar is S44330 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
25
Fatigue Strength, MPa 120 to 130
160
Poisson's Ratio 0.29
0.27
Shear Modulus, GPa 18
78
Shear Strength, MPa 150 to 170
280
Tensile Strength: Ultimate (UTS), MPa 250 to 290
440
Tensile Strength: Yield (Proof), MPa 140 to 180
230

Thermal Properties

Latent Heat of Fusion, J/g 340
290
Maximum Temperature: Mechanical, °C 95
990
Melting Completion (Liquidus), °C 600
1440
Melting Onset (Solidus), °C 560
1390
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
21
Thermal Expansion, µm/m-K 25
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
13
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 23
2.8
Embodied Energy, MJ/kg 160
40
Embodied Water, L/kg 960
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
91
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
140
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
16
Strength to Weight: Bending, points 50 to 55
17
Thermal Diffusivity, mm2/s 73
5.7
Thermal Shock Resistance, points 16 to 18
16

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.025
Chromium (Cr), % 0
20 to 23
Copper (Cu), % 0 to 0.1
0.3 to 0.8
Iron (Fe), % 0 to 0.060
72.5 to 79.7
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.0
Nickel (Ni), % 0 to 0.0050
0
Niobium (Nb), % 0
0 to 0.8
Nitrogen (N), % 0
0 to 0.025
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0
0 to 0.8
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0