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ISO-WD32350 Magnesium vs. S35125 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while S35125 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 S35125 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
39
Fatigue Strength, MPa 120 to 130
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
78
Shear Strength, MPa 150 to 170
370
Tensile Strength: Ultimate (UTS), MPa 250 to 290
540
Tensile Strength: Yield (Proof), MPa 140 to 180
230

Thermal Properties

Latent Heat of Fusion, J/g 340
300
Maximum Temperature: Mechanical, °C 95
1100
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 560
1380
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 130
12
Thermal Expansion, µm/m-K 25
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 12
36
Density, g/cm3 1.7
8.1
Embodied Carbon, kg CO2/kg material 23
6.4
Embodied Energy, MJ/kg 160
89
Embodied Water, L/kg 960
210

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
170
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
140
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
24
Strength to Weight: Axial, points 39 to 46
19
Strength to Weight: Bending, points 50 to 55
18
Thermal Diffusivity, mm2/s 73
3.1
Thermal Shock Resistance, points 16 to 18
12

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
20 to 23
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
36.2 to 45.8
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
1.0 to 1.5
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0 to 0.0050
31 to 35
Niobium (Nb), % 0
0.25 to 0.6
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0