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EN-MC21120 Magnesium vs. EN 1.4826 Stainless Steel

EN-MC21120 magnesium belongs to the magnesium alloys classification, while EN 1.4826 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 EN-MC21120 magnesium and the bottom bar is EN 1.4826 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 63 to 75
150
Elastic (Young's, Tensile) Modulus, GPa 46
200
Elongation at Break, % 2.2 to 6.7
9.1
Fatigue Strength, MPa 84 to 96
140
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
77
Tensile Strength: Ultimate (UTS), MPa 200 to 270
500
Tensile Strength: Yield (Proof), MPa 130 to 170
260

Thermal Properties

Latent Heat of Fusion, J/g 350
310
Maximum Temperature: Mechanical, °C 130
950
Melting Completion (Liquidus), °C 600
1400
Melting Onset (Solidus), °C 490
1360
Specific Heat Capacity, J/kg-K 990
490
Thermal Conductivity, W/m-K 76
14
Thermal Expansion, µm/m-K 26
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
2.0
Electrical Conductivity: Equal Weight (Specific), % IACS 59
2.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
17
Density, g/cm3 1.7
7.7
Embodied Carbon, kg CO2/kg material 22
3.3
Embodied Energy, MJ/kg 160
47
Embodied Water, L/kg 990
160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.0 to 15
39
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
170
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 31 to 43
18
Strength to Weight: Bending, points 43 to 53
18
Thermal Diffusivity, mm2/s 44
3.7
Thermal Shock Resistance, points 11 to 16
11

Alloy Composition

Aluminum (Al), % 8.3 to 9.7
0
Carbon (C), % 0
0.3 to 0.5
Chromium (Cr), % 0
21 to 23
Copper (Cu), % 0 to 0.030
0
Iron (Fe), % 0 to 0.0050
60.4 to 68.7
Magnesium (Mg), % 88.6 to 91.3
0
Manganese (Mn), % 0.1 to 0.5
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.0020
9.0 to 11
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
1.0 to 2.5
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 0.35 to 1.0
0
Residuals, % 0 to 0.010
0