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AZ91E Magnesium vs. ASTM A369 Grade FP12

AZ91E magnesium belongs to the magnesium alloys classification, while ASTM A369 grade FP12 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 ASTM A369 grade FP12.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
140
Elastic (Young's, Tensile) Modulus, GPa 46
190
Elongation at Break, % 2.5 to 6.2
20
Fatigue Strength, MPa 81 to 85
170
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 18
73
Shear Strength, MPa 89 to 150
300
Tensile Strength: Ultimate (UTS), MPa 160 to 260
470
Tensile Strength: Yield (Proof), MPa 96 to 130
250

Thermal Properties

Latent Heat of Fusion, J/g 350
250
Maximum Temperature: Mechanical, °C 130
430
Melting Completion (Liquidus), °C 600
1470
Melting Onset (Solidus), °C 500
1430
Specific Heat Capacity, J/kg-K 990
470
Thermal Conductivity, W/m-K 84
45
Thermal Expansion, µm/m-K 27
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10 to 12
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 52 to 60
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 12
2.8
Density, g/cm3 1.7
7.9
Embodied Carbon, kg CO2/kg material 22
1.6
Embodied Energy, MJ/kg 160
21
Embodied Water, L/kg 990
52

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.4 to 12
81
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 190
160
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 69
24
Strength to Weight: Axial, points 25 to 42
17
Strength to Weight: Bending, points 37 to 53
17
Thermal Diffusivity, mm2/s 49
12
Thermal Shock Resistance, points 9.0 to 15
14

Alloy Composition

Aluminum (Al), % 8.1 to 9.3
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
0.8 to 1.3
Copper (Cu), % 0 to 0.015
0
Iron (Fe), % 0 to 0.0050
96.8 to 98.4
Magnesium (Mg), % 88.8 to 91.3
0
Manganese (Mn), % 0.17 to 0.35
0.3 to 0.61
Molybdenum (Mo), % 0
0.44 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 0.5
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0.4 to 1.0
0
Residuals, % 0 to 0.3
0