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ISO-WD32350 Magnesium vs. AISI 321 Stainless Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while AISI 321 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-WD32350 magnesium and the bottom bar is AISI 321 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 5.7 to 10
34 to 50
Fatigue Strength, MPa 120 to 130
220 to 270
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Shear Strength, MPa 150 to 170
420 to 460
Tensile Strength: Ultimate (UTS), MPa 250 to 290
590 to 690
Tensile Strength: Yield (Proof), MPa 140 to 180
220 to 350

Thermal Properties

Latent Heat of Fusion, J/g 340
290
Maximum Temperature: Mechanical, °C 95
870
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 560
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 130
16
Thermal Expansion, µm/m-K 25
17

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
16
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
3.2
Embodied Energy, MJ/kg 160
45
Embodied Water, L/kg 960
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
190 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
130 to 310
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 68
25
Strength to Weight: Axial, points 39 to 46
21 to 25
Strength to Weight: Bending, points 50 to 55
20 to 22
Thermal Diffusivity, mm2/s 73
4.1
Thermal Shock Resistance, points 16 to 18
13 to 15

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 19
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
65.3 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 12
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
Titanium (Ti), % 0
0 to 0.7
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0