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EN 1.4057 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4057 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 (4, 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 1.4057 stainless steel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
46
Elongation at Break, % 11 to 17
2.2 to 6.7
Fatigue Strength, MPa 320 to 430
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 77
18
Shear Strength, MPa 520 to 580
110 to 160
Tensile Strength: Ultimate (UTS), MPa 840 to 980
200 to 270
Tensile Strength: Yield (Proof), MPa 530 to 790
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 850
130
Melting Completion (Liquidus), °C 1440
600
Melting Onset (Solidus), °C 1390
490
Specific Heat Capacity, J/kg-K 480
990
Thermal Conductivity, W/m-K 25
76
Thermal Expansion, µm/m-K 10
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
11
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
59

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 7.7
1.7
Embodied Carbon, kg CO2/kg material 2.2
22
Embodied Energy, MJ/kg 32
160
Embodied Water, L/kg 120
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 96 to 130
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 700 to 1610
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 30 to 35
31 to 43
Strength to Weight: Bending, points 26 to 28
43 to 53
Thermal Diffusivity, mm2/s 6.7
44
Thermal Shock Resistance, points 30 to 35
11 to 16

Alloy Composition


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Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0.12 to 0.22
0
Chromium (Cr), % 15 to 17
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 77.7 to 83.4
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0 to 1.5
0.1 to 0.5
Nickel (Ni), % 1.5 to 2.5
0 to 0.0020
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
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

Comparable Variants