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ISO-WD32350 Magnesium vs. EN 1.5410 Steel

ISO-WD32350 magnesium belongs to the magnesium alloys classification, while EN 1.5410 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-WD32350 magnesium and the bottom bar is EN 1.5410 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 45
190
Elongation at Break, % 5.7 to 10
20 to 25
Fatigue Strength, MPa 120 to 130
290 to 330
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Tensile Strength: Ultimate (UTS), MPa 250 to 290
560 to 620
Tensile Strength: Yield (Proof), MPa 140 to 180
400 to 480

Thermal Properties

Latent Heat of Fusion, J/g 340
250
Maximum Temperature: Mechanical, °C 95
400
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 130
51
Thermal Expansion, µm/m-K 25
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
2.3
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 23
1.7
Embodied Energy, MJ/kg 160
22
Embodied Water, L/kg 960
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 23
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 380
430 to 610
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 68
24
Strength to Weight: Axial, points 39 to 46
20 to 22
Strength to Weight: Bending, points 50 to 55
19 to 21
Thermal Diffusivity, mm2/s 73
14
Thermal Shock Resistance, points 16 to 18
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0
0 to 0.12
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.060
96.9 to 98.6
Magnesium (Mg), % 95.7 to 97.7
0
Manganese (Mn), % 0.6 to 1.3
1.2 to 1.8
Molybdenum (Mo), % 0
0.2 to 0.4
Nickel (Ni), % 0 to 0.0050
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.1
0 to 0.6
Sulfur (S), % 0
0 to 0.020
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 1.8 to 2.3
0
Residuals, % 0 to 0.3
0