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ISO-WD32260 Magnesium vs. EN 1.6553 Steel

ISO-WD32260 magnesium belongs to the magnesium alloys classification, while EN 1.6553 steel belongs to the iron alloys. There are 29 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 ISO-WD32260 magnesium and the bottom bar is EN 1.6553 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 4.5 to 6.0
19 to 21
Fatigue Strength, MPa 150 to 190
330 to 460
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Tensile Strength: Ultimate (UTS), MPa 330 to 340
710 to 800
Tensile Strength: Yield (Proof), MPa 230 to 250
470 to 670

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 120
420
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 520
1420
Specific Heat Capacity, J/kg-K 970
470
Thermal Conductivity, W/m-K 110
39
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 140
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 13
2.7
Density, g/cm3 1.9
7.8
Embodied Carbon, kg CO2/kg material 23
1.6
Embodied Energy, MJ/kg 160
21
Embodied Water, L/kg 940
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
130 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 560 to 700
600 to 1190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 63
24
Strength to Weight: Axial, points 48 to 51
25 to 28
Strength to Weight: Bending, points 56 to 58
23 to 24
Thermal Diffusivity, mm2/s 63
10
Thermal Shock Resistance, points 19 to 20
21 to 23

Alloy Composition

Carbon (C), % 0
0.23 to 0.28
Chromium (Cr), % 0
0.4 to 0.8
Copper (Cu), % 0
0 to 0.3
Iron (Fe), % 0
95.6 to 98.2
Magnesium (Mg), % 92.7 to 94.8
0
Manganese (Mn), % 0
0.6 to 1.0
Molybdenum (Mo), % 0
0.15 to 0.3
Nickel (Ni), % 0
0.4 to 0.8
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0
0 to 0.8
Sulfur (S), % 0
0 to 0.025
Vanadium (V), % 0
0 to 0.030
Zinc (Zn), % 4.8 to 6.2
0
Zirconium (Zr), % 0.45 to 0.8
0
Residuals, % 0 to 0.3
0

Comparable Variants