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ASTM A182 Grade F122 vs. 7010 Aluminum

ASTM A182 grade F122 belongs to the iron alloys classification, while 7010 aluminum belongs to the aluminum 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 ASTM A182 grade F122 and the bottom bar is 7010 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 23
3.9 to 6.8
Fatigue Strength, MPa 320
160 to 190
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
26
Shear Strength, MPa 450
300 to 340
Tensile Strength: Ultimate (UTS), MPa 710
520 to 590
Tensile Strength: Yield (Proof), MPa 450
410 to 540

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 600
200
Melting Completion (Liquidus), °C 1490
630
Melting Onset (Solidus), °C 1440
480
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 24
150
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 10
40
Electrical Conductivity: Equal Weight (Specific), % IACS 12
120

Otherwise Unclassified Properties

Base Metal Price, % relative 12
10
Density, g/cm3 8.0
3.0
Embodied Carbon, kg CO2/kg material 3.0
8.3
Embodied Energy, MJ/kg 44
150
Embodied Water, L/kg 100
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 140
22 to 33
Resilience: Unit (Modulus of Resilience), kJ/m3 520
1230 to 2130
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 25
47 to 54
Strength to Weight: Bending, points 22
47 to 52
Thermal Diffusivity, mm2/s 6.4
58
Thermal Shock Resistance, points 19
22 to 26

Alloy Composition

Aluminum (Al), % 0 to 0.020
87.9 to 90.6
Boron (B), % 0 to 0.0050
0
Carbon (C), % 0.070 to 0.14
0
Chromium (Cr), % 10 to 11.5
0 to 0.050
Copper (Cu), % 0.3 to 1.7
1.5 to 2.0
Iron (Fe), % 81.3 to 87.7
0 to 0.15
Magnesium (Mg), % 0
2.1 to 2.6
Manganese (Mn), % 0 to 0.7
0 to 0.1
Molybdenum (Mo), % 0.25 to 0.6
0
Nickel (Ni), % 0 to 0.5
0 to 0.050
Niobium (Nb), % 0.040 to 0.1
0
Nitrogen (N), % 0.040 to 0.1
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.12
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0 to 0.060
Tungsten (W), % 1.5 to 2.5
0
Vanadium (V), % 0.15 to 0.3
0
Zinc (Zn), % 0
5.7 to 6.7
Zirconium (Zr), % 0 to 0.010
0.1 to 0.16
Residuals, % 0
0 to 0.15