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EN-MC21210 Magnesium vs. EN 1.4913 Stainless Steel

EN-MC21210 magnesium belongs to the magnesium alloys classification, while EN 1.4913 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-MC21210 magnesium and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 44
190
Elongation at Break, % 14
14 to 22
Fatigue Strength, MPa 70
320 to 480
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
75
Shear Strength, MPa 110
550 to 590
Tensile Strength: Ultimate (UTS), MPa 190
870 to 980
Tensile Strength: Yield (Proof), MPa 90
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 350
270
Maximum Temperature: Mechanical, °C 100
700
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 570
1410
Specific Heat Capacity, J/kg-K 1000
480
Thermal Conductivity, W/m-K 120
24
Thermal Expansion, µm/m-K 27
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.0
Density, g/cm3 1.6
7.8
Embodied Carbon, kg CO2/kg material 24
2.9
Embodied Energy, MJ/kg 160
41
Embodied Water, L/kg 980
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 92
600 to 1860
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 72
25
Strength to Weight: Axial, points 32
31 to 35
Strength to Weight: Bending, points 44
26 to 28
Thermal Diffusivity, mm2/s 76
6.5
Thermal Shock Resistance, points 11
31 to 34

Alloy Composition

Aluminum (Al), % 1.6 to 2.6
0 to 0.020
Boron (B), % 0
0 to 0.0015
Carbon (C), % 0
0.17 to 0.23
Chromium (Cr), % 0
10 to 11.5
Copper (Cu), % 0 to 0.010
0
Iron (Fe), % 0 to 0.0050
84.5 to 88.3
Magnesium (Mg), % 96.3 to 98.3
0
Manganese (Mn), % 0.1 to 0.7
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0 to 0.0020
0.2 to 0.6
Niobium (Nb), % 0
0.25 to 0.55
Nitrogen (N), % 0
0.050 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.010
0