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AM100A Magnesium vs. EN 1.1158 Steel

AM100A magnesium belongs to the magnesium alloys classification, while EN 1.1158 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 AM100A magnesium and the bottom bar is EN 1.1158 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 1.0 to 6.8
23 to 24
Fatigue Strength, MPa 48 to 70
170 to 220
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 90 to 150
300 to 320
Tensile Strength: Ultimate (UTS), MPa 160 to 270
470 to 500
Tensile Strength: Yield (Proof), MPa 78 to 140
240 to 310

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 140
400
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 460
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 73
49
Thermal Expansion, µm/m-K 25
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 59
8.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
2.1
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
1.4
Embodied Energy, MJ/kg 160
19
Embodied Water, L/kg 1000
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.3 to 15
89 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 66 to 210
150 to 250
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 70
24
Strength to Weight: Axial, points 25 to 44
17 to 18
Strength to Weight: Bending, points 38 to 54
17 to 18
Thermal Diffusivity, mm2/s 43
13
Thermal Shock Resistance, points 9.7 to 17
15 to 16

Alloy Composition


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Aluminum (Al), % 9.3 to 10.7
0
Carbon (C), % 0
0.22 to 0.29
Chromium (Cr), % 0
0 to 0.4
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0
97.6 to 99.38
Magnesium (Mg), % 87.9 to 90.6
0
Manganese (Mn), % 0.1 to 0.35
0.4 to 0.7
Molybdenum (Mo), % 0
0 to 0.1
Nickel (Ni), % 0 to 0.010
0 to 0.4
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.3
0 to 0.4
Sulfur (S), % 0
0 to 0.035
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.3
0