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EN-MC21220 Magnesium vs. AISI 321 Stainless Steel

EN-MC21220 magnesium belongs to the magnesium alloys classification, while AISI 321 stainless steel belongs to the iron alloys. There are 31 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 EN-MC21220 magnesium and the bottom bar is AISI 321 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58
170 to 210
Elastic (Young's, Tensile) Modulus, GPa 45
200
Elongation at Break, % 11
34 to 50
Fatigue Strength, MPa 89
220 to 270
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
77
Shear Strength, MPa 120
420 to 460
Tensile Strength: Ultimate (UTS), MPa 210
590 to 690
Tensile Strength: Yield (Proof), MPa 120
220 to 350

Thermal Properties

Latent Heat of Fusion, J/g 350
290
Maximum Temperature: Mechanical, °C 120
870
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 540
1400
Specific Heat Capacity, J/kg-K 1000
480
Thermal Conductivity, W/m-K 65
16
Thermal Expansion, µm/m-K 27
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 16
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 87
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 990
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 20
190 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 160
130 to 310
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 71
25
Strength to Weight: Axial, points 34
21 to 25
Strength to Weight: Bending, points 46
20 to 22
Thermal Diffusivity, mm2/s 39
4.1
Thermal Shock Resistance, points 12
13 to 15

Alloy Composition

Aluminum (Al), % 4.4 to 5.5
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 19
Copper (Cu), % 0 to 0.010
0
Iron (Fe), % 0 to 0.0050
65.3 to 74
Magnesium (Mg), % 93.5 to 95.5
0
Manganese (Mn), % 0.1 to 0.6
0 to 2.0
Nickel (Ni), % 0 to 0.0020
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), % 0 to 0.3
0
Residuals, % 0 to 0.010
0