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EN 1.4542 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4542 stainless steel belongs to the iron alloys classification, while EN-MC21120 magnesium belongs to the magnesium 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 1.4542 stainless steel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 5.7 to 20
2.2 to 6.7
Fatigue Strength, MPa 370 to 640
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 550 to 860
110 to 160
Tensile Strength: Ultimate (UTS), MPa 880 to 1470
200 to 270
Tensile Strength: Yield (Proof), MPa 580 to 1300
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 860
130
Melting Completion (Liquidus), °C 1430
600
Melting Onset (Solidus), °C 1380
490
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 16
76
Thermal Expansion, µm/m-K 11
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
11
Electrical Conductivity: Equal Weight (Specific), % IACS 2.8
59

Otherwise Unclassified Properties

Base Metal Price, % relative 13
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 2.7
22
Embodied Energy, MJ/kg 39
160
Embodied Water, L/kg 130
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 62 to 160
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 880 to 4360
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 31 to 52
31 to 43
Strength to Weight: Bending, points 26 to 37
43 to 53
Thermal Diffusivity, mm2/s 4.3
44
Thermal Shock Resistance, points 29 to 49
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0 to 0.070
0
Chromium (Cr), % 15 to 17
0
Copper (Cu), % 3.0 to 5.0
0 to 0.030
Iron (Fe), % 69.6 to 79
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0 to 1.5
0.1 to 0.5
Molybdenum (Mo), % 0 to 0.6
0
Nickel (Ni), % 3.0 to 5.0
0 to 0.0020
Niobium (Nb), % 0 to 0.45
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 0.7
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010