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ISO-WD32350 Magnesium vs. AISI 348 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while AISI 348 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 AISI 348 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
41
Fatigue Strength, MPa 120 to 130
200
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 150 to 170
400
Tensile Strength: Ultimate (UTS), MPa 250 to 290
580
Tensile Strength: Yield (Proof), MPa 140 to 180
230

Thermal Properties

Latent Heat of Fusion, J/g 340
290
Maximum Temperature: Mechanical, °C 95
940
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 560
1390
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
16
Thermal Expansion, µm/m-K 25
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 12
19
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
3.7
Embodied Energy, MJ/kg 160
54
Embodied Water, L/kg 960
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
190
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
21
Strength to Weight: Bending, points 50 to 55
20
Thermal Diffusivity, mm2/s 73
4.2
Thermal Shock Resistance, points 16 to 18
13

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 19
Cobalt (Co), % 0
0 to 0.2
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
63.8 to 74
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
0 to 2.0
Nickel (Ni), % 0 to 0.0050
9.0 to 13
Niobium (Nb), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.1
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Tantalum (Ta), % 0
0 to 0.1
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0