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EN 1.4615 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4615 stainless steel belongs to the iron alloys classification, while EN-MC21120 magnesium belongs to the magnesium alloys. There are 31 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 1.4615 stainless steel and the bottom bar is EN-MC21120 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 150
63 to 75
Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 50
2.2 to 6.7
Fatigue Strength, MPa 190
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 360
110 to 160
Tensile Strength: Ultimate (UTS), MPa 500
200 to 270
Tensile Strength: Yield (Proof), MPa 200
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 280
350
Maximum Temperature: Mechanical, °C 840
130
Melting Completion (Liquidus), °C 1400
600
Melting Onset (Solidus), °C 1360
490
Specific Heat Capacity, J/kg-K 480
990
Thermal Conductivity, W/m-K 15
76
Thermal Expansion, µm/m-K 17
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 2.8
22
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 140
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 99
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 18
31 to 43
Strength to Weight: Bending, points 18
43 to 53
Thermal Diffusivity, mm2/s 4.1
44
Thermal Shock Resistance, points 11
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 14 to 16
0
Copper (Cu), % 2.0 to 4.0
0 to 0.030
Iron (Fe), % 63.1 to 72.5
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 7.0 to 9.0
0.1 to 0.5
Molybdenum (Mo), % 0 to 0.8
0
Nickel (Ni), % 4.5 to 6.0
0 to 0.0020
Nitrogen (N), % 0.020 to 0.060
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.2
Sulfur (S), % 0 to 0.010
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010