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ISO-WD43150 Magnesium vs. AISI 317 Stainless Steel

ISO-WD43150 magnesium belongs to the magnesium alloys classification, while AISI 317 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-WD43150 magnesium and the bottom bar is AISI 317 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 2.8
35 to 55
Fatigue Strength, MPa 100
250 to 330
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
79
Shear Strength, MPa 140
420 to 470
Tensile Strength: Ultimate (UTS), MPa 250
580 to 710
Tensile Strength: Yield (Proof), MPa 150
250 to 420

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 95
590
Melting Completion (Liquidus), °C 610
1400
Melting Onset (Solidus), °C 590
1380
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 140
15
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 170
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 12
21
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 24
4.3
Embodied Energy, MJ/kg 160
59
Embodied Water, L/kg 970
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.1
210 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 250
150 to 430
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
25
Strength to Weight: Axial, points 41
20 to 25
Strength to Weight: Bending, points 52
20 to 22
Thermal Diffusivity, mm2/s 81
4.1
Thermal Shock Resistance, points 14
12 to 15

Alloy Composition

Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
18 to 20
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0
58 to 68
Magnesium (Mg), % 97.5 to 98.8
0
Manganese (Mn), % 1.2 to 2.0
0 to 2.0
Molybdenum (Mo), % 0
3.0 to 4.0
Nickel (Ni), % 0 to 0.010
11 to 15
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Residuals, % 0 to 0.3
0