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EN 1.4923 Stainless Steel vs. EN-MC21120 Magnesium

EN 1.4923 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 (5, 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 1.4923 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, % 12 to 21
2.2 to 6.7
Fatigue Strength, MPa 300 to 440
84 to 96
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 540 to 590
110 to 160
Tensile Strength: Ultimate (UTS), MPa 870 to 980
200 to 270
Tensile Strength: Yield (Proof), MPa 470 to 780
130 to 170

Thermal Properties

Latent Heat of Fusion, J/g 270
350
Maximum Temperature: Mechanical, °C 740
130
Melting Completion (Liquidus), °C 1450
600
Melting Onset (Solidus), °C 1410
490
Specific Heat Capacity, J/kg-K 480
990
Thermal Conductivity, W/m-K 24
76
Thermal Expansion, µm/m-K 11
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
11
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
59

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 2.9
22
Embodied Energy, MJ/kg 41
160
Embodied Water, L/kg 100
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 150
5.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 1580
180 to 320
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
69
Strength to Weight: Axial, points 31 to 35
31 to 43
Strength to Weight: Bending, points 26 to 28
43 to 53
Thermal Diffusivity, mm2/s 6.5
44
Thermal Shock Resistance, points 30 to 34
11 to 16

Alloy Composition

Aluminum (Al), % 0
8.3 to 9.7
Carbon (C), % 0.18 to 0.24
0
Chromium (Cr), % 11 to 12.5
0
Copper (Cu), % 0
0 to 0.030
Iron (Fe), % 83.5 to 87.1
0 to 0.0050
Magnesium (Mg), % 0
88.6 to 91.3
Manganese (Mn), % 0.4 to 0.9
0.1 to 0.5
Molybdenum (Mo), % 0.8 to 1.2
0
Nickel (Ni), % 0.3 to 0.8
0 to 0.0020
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Vanadium (V), % 0.25 to 0.35
0
Zinc (Zn), % 0
0.35 to 1.0
Residuals, % 0
0 to 0.010

Comparable Variants