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ISO-WD32350 Magnesium vs. N08801 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while N08801 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 N08801 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
34
Fatigue Strength, MPa 120 to 130
260
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 150 to 170
570
Tensile Strength: Ultimate (UTS), MPa 250 to 290
860
Tensile Strength: Yield (Proof), MPa 140 to 180
190

Thermal Properties

Latent Heat of Fusion, J/g 340
300
Maximum Temperature: Mechanical, °C 95
1090
Melting Completion (Liquidus), °C 600
1390
Melting Onset (Solidus), °C 560
1360
Specific Heat Capacity, J/kg-K 990
480
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
30
Density, g/cm3 1.7
8.0
Embodied Carbon, kg CO2/kg material 23
5.5
Embodied Energy, MJ/kg 160
79
Embodied Water, L/kg 960
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
220
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
92
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
24
Strength to Weight: Axial, points 39 to 46
30
Strength to Weight: Bending, points 50 to 55
25
Thermal Diffusivity, mm2/s 73
3.3
Thermal Shock Resistance, points 16 to 18
20

Alloy Composition


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Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
19 to 22
Copper (Cu), % 0 to 0.1
0 to 0.5
Iron (Fe), % 0 to 0.060
39.5 to 50.3
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 1.5
Nickel (Ni), % 0 to 0.0050
30 to 34
Silicon (Si), % 0 to 0.1
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0
0.75 to 1.5
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0