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EN-MC32110 Magnesium vs. EN 1.4913 Stainless Steel

EN-MC32110 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-MC32110 magnesium and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 49
190
Elongation at Break, % 2.2
14 to 22
Fatigue Strength, MPa 80
320 to 480
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 19
75
Shear Strength, MPa 120
550 to 590
Tensile Strength: Ultimate (UTS), MPa 220
870 to 980
Tensile Strength: Yield (Proof), MPa 140
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 330
270
Maximum Temperature: Mechanical, °C 99
700
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 500
1410
Specific Heat Capacity, J/kg-K 950
480
Thermal Conductivity, W/m-K 120
24
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 140
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.0
Density, g/cm3 2.1
7.8
Embodied Carbon, kg CO2/kg material 22
2.9
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 920
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.3
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 210
600 to 1860
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 58
25
Strength to Weight: Axial, points 29
31 to 35
Strength to Weight: Bending, points 38
26 to 28
Thermal Diffusivity, mm2/s 58
6.5
Thermal Shock Resistance, points 12
31 to 34

Alloy Composition

Aluminum (Al), % 0 to 0.2
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), % 2.4 to 3.0
0
Iron (Fe), % 0 to 0.050
84.5 to 88.3
Magnesium (Mg), % 89.3 to 91.9
0
Manganese (Mn), % 0.25 to 0.75
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0 to 0.010
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 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 5.5 to 6.5
0
Residuals, % 0 to 0.010
0