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AZ91E Magnesium vs. ASTM A182 Grade F6b

AZ91E magnesium belongs to the magnesium alloys classification, while ASTM A182 grade F6b belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (7, 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 ASTM A182 grade F6b.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
260
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.5 to 6.2
18
Fatigue Strength, MPa 81 to 85
440
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 18
76
Shear Strength, MPa 89 to 150
530
Tensile Strength: Ultimate (UTS), MPa 160 to 260
850
Tensile Strength: Yield (Proof), MPa 96 to 130
710

Thermal Properties

Latent Heat of Fusion, J/g 350
280
Maximum Temperature: Mechanical, °C 130
750
Melting Completion (Liquidus), °C 600
1450
Melting Onset (Solidus), °C 500
1400
Specific Heat Capacity, J/kg-K 990
480
Thermal Conductivity, W/m-K 84
25
Thermal Expansion, µm/m-K 27
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
2.8
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
3.2

Otherwise Unclassified Properties

Base Metal Price, % relative 12
8.0
Density, g/cm3 1.7
7.8
Embodied Carbon, kg CO2/kg material 22
2.2
Embodied Energy, MJ/kg 160
30
Embodied Water, L/kg 990
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
140
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
1280
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 69
25
Strength to Weight: Axial, points 25 to 42
30
Strength to Weight: Bending, points 37 to 53
26
Thermal Diffusivity, mm2/s 49
6.7
Thermal Shock Resistance, points 9.0 to 15
31

Alloy Composition

Aluminum (Al), % 8.1 to 9.3
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 0 to 0.015
0 to 0.5
Iron (Fe), % 0 to 0.0050
81.2 to 87.1
Magnesium (Mg), % 88.8 to 91.3
0
Manganese (Mn), % 0.17 to 0.35
0 to 1.0
Molybdenum (Mo), % 0
0.4 to 0.6
Nickel (Ni), % 0 to 0.0010
1.0 to 2.0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0