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5052 Aluminum vs. ASTM A369 Grade FP11

5052 aluminum belongs to the aluminum alloys classification, while ASTM A369 grade FP11 belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 5052 aluminum and the bottom bar is ASTM A369 grade FP11.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 46 to 83
140
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.1 to 22
20
Fatigue Strength, MPa 66 to 140
160
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 120 to 180
300
Tensile Strength: Ultimate (UTS), MPa 190 to 320
470
Tensile Strength: Yield (Proof), MPa 75 to 280
240

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 190
430
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.6
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1190
52

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.7 to 69
80
Resilience: Unit (Modulus of Resilience), kJ/m3 41 to 590
150
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 19 to 33
17
Strength to Weight: Bending, points 27 to 38
17
Thermal Diffusivity, mm2/s 57
11
Thermal Shock Resistance, points 8.3 to 14
14

Alloy Composition

Aluminum (Al), % 95.8 to 97.7
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0.15 to 0.35
1.0 to 1.5
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
96.1 to 97.7
Magnesium (Mg), % 2.2 to 2.8
0
Manganese (Mn), % 0 to 0.1
0.3 to 0.6
Molybdenum (Mo), % 0
0.44 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0.5 to 1.0
Sulfur (S), % 0
0 to 0.025
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0