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AZ91E Magnesium vs. EN 1.7365 Steel

AZ91E magnesium belongs to the magnesium alloys classification, while EN 1.7365 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 AZ91E magnesium and the bottom bar is EN 1.7365 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
210
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.5 to 6.2
18
Fatigue Strength, MPa 81 to 85
320
Impact Strength: V-Notched Charpy, J 0.79 to 2.8
31
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
74
Tensile Strength: Ultimate (UTS), MPa 160 to 260
700
Tensile Strength: Yield (Proof), MPa 96 to 130
470

Thermal Properties

Latent Heat of Fusion, J/g 350
260
Maximum Temperature: Mechanical, °C 130
510
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 500
1420
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 84
40
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
8.2
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 12
4.4
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
1.8
Embodied Energy, MJ/kg 160
24
Embodied Water, L/kg 990
70

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
110
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
580
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 25 to 42
25
Strength to Weight: Bending, points 37 to 53
22
Thermal Diffusivity, mm2/s 49
11
Thermal Shock Resistance, points 9.0 to 15
20

Alloy Composition

Aluminum (Al), % 8.1 to 9.3
0
Carbon (C), % 0
0.12 to 0.19
Chromium (Cr), % 0
4.0 to 6.0
Copper (Cu), % 0 to 0.015
0 to 0.3
Iron (Fe), % 0 to 0.0050
91.2 to 94.9
Magnesium (Mg), % 88.8 to 91.3
0
Manganese (Mn), % 0.17 to 0.35
0.5 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.65
Nickel (Ni), % 0 to 0.0010
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.8
Sulfur (S), % 0
0 to 0.025
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0