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ISO-WD32350 Magnesium vs. S64512 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while S64512 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 S64512 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
17
Fatigue Strength, MPa 120 to 130
540
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 150 to 170
700
Tensile Strength: Ultimate (UTS), MPa 250 to 290
1140
Tensile Strength: Yield (Proof), MPa 140 to 180
890

Thermal Properties

Latent Heat of Fusion, J/g 340
270
Maximum Temperature: Mechanical, °C 95
750
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 130
28
Thermal Expansion, µm/m-K 25
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
3.6
Electrical Conductivity: Equal Weight (Specific), % IACS 130
4.1

Otherwise Unclassified Properties

Base Metal Price, % relative 12
10
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
3.3
Embodied Energy, MJ/kg 160
47
Embodied Water, L/kg 960
110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
180
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
2020
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
40
Strength to Weight: Bending, points 50 to 55
31
Thermal Diffusivity, mm2/s 73
7.5
Thermal Shock Resistance, points 16 to 18
42

Alloy Composition


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Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0
11 to 12.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
80.6 to 84.7
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0.5 to 0.9
Molybdenum (Mo), % 0
1.5 to 2.0
Nickel (Ni), % 0 to 0.0050
2.0 to 3.0
Nitrogen (N), % 0
0.010 to 0.050
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.35
Sulfur (S), % 0
0 to 0.025
Vanadium (V), % 0
0.25 to 0.4
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0