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6066 Aluminum vs. ASTM A182 Grade F122

6066 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F122 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 6066 aluminum and the bottom bar is ASTM A182 grade F122.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 7.8 to 17
23
Fatigue Strength, MPa 94 to 130
320
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 95 to 240
450
Tensile Strength: Ultimate (UTS), MPa 160 to 400
710
Tensile Strength: Yield (Proof), MPa 93 to 360
450

Thermal Properties

Latent Heat of Fusion, J/g 410
270
Maximum Temperature: Mechanical, °C 170
600
Melting Completion (Liquidus), °C 650
1490
Melting Onset (Solidus), °C 560
1440
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 150
24
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
10
Electrical Conductivity: Equal Weight (Specific), % IACS 130
12

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 2.8
8.0
Embodied Carbon, kg CO2/kg material 8.3
3.0
Embodied Energy, MJ/kg 150
44
Embodied Water, L/kg 1160
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 52
140
Resilience: Unit (Modulus of Resilience), kJ/m3 61 to 920
520
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 16 to 39
25
Strength to Weight: Bending, points 23 to 43
22
Thermal Diffusivity, mm2/s 61
6.4
Thermal Shock Resistance, points 6.9 to 17
19

Alloy Composition

Aluminum (Al), % 93 to 97
0 to 0.020
Boron (B), % 0
0 to 0.0050
Carbon (C), % 0
0.070 to 0.14
Chromium (Cr), % 0 to 0.4
10 to 11.5
Copper (Cu), % 0.7 to 1.2
0.3 to 1.7
Iron (Fe), % 0 to 0.5
81.3 to 87.7
Magnesium (Mg), % 0.8 to 1.4
0
Manganese (Mn), % 0.6 to 1.1
0 to 0.7
Molybdenum (Mo), % 0
0.25 to 0.6
Nickel (Ni), % 0
0 to 0.5
Niobium (Nb), % 0
0.040 to 0.1
Nitrogen (N), % 0
0.040 to 0.1
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.9 to 1.8
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0 to 0.010
Tungsten (W), % 0
1.5 to 2.5
Vanadium (V), % 0
0.15 to 0.3
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0