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ISO-WD32250 Magnesium vs. EN 1.4913 Stainless Steel

ISO-WD32250 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 (2, 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 ISO-WD32250 magnesium and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 4.5 to 8.6
14 to 22
Fatigue Strength, MPa 170 to 210
320 to 480
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 17
75
Shear Strength, MPa 180 to 190
550 to 590
Tensile Strength: Ultimate (UTS), MPa 310 to 330
870 to 980
Tensile Strength: Yield (Proof), MPa 240 to 290
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 340
270
Maximum Temperature: Mechanical, °C 120
700
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 550
1410
Specific Heat Capacity, J/kg-K 980
480
Thermal Conductivity, W/m-K 130
24
Thermal Expansion, µm/m-K 26
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.0
Density, g/cm3 1.8
7.8
Embodied Carbon, kg CO2/kg material 24
2.9
Embodied Energy, MJ/kg 160
41
Embodied Water, L/kg 950
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 26
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 630 to 930
600 to 1860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 67
25
Strength to Weight: Axial, points 49 to 51
31 to 35
Strength to Weight: Bending, points 58 to 60
26 to 28
Thermal Diffusivity, mm2/s 72
6.5
Thermal Shock Resistance, points 19 to 20
31 to 34

Alloy Composition


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Aluminum (Al), % 0
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
Iron (Fe), % 0
84.5 to 88.3
Magnesium (Mg), % 94.9 to 97.1
0
Manganese (Mn), % 0
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0
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
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 2.5 to 4.0
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0