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6101A Aluminum vs. 7022 Aluminum

Both 6101A aluminum and 7022 aluminum are aluminum alloys. They have a moderately high 91% of their average alloy composition in common.

For each property being compared, the top bar is 6101A aluminum and the bottom bar is 7022 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
70
Elongation at Break, % 11
6.3 to 8.0
Fatigue Strength, MPa 80
140 to 170
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 26
26
Shear Strength, MPa 130
290 to 320
Tensile Strength: Ultimate (UTS), MPa 220
490 to 540
Tensile Strength: Yield (Proof), MPa 190
390 to 460

Thermal Properties

Latent Heat of Fusion, J/g 400
380
Maximum Temperature: Mechanical, °C 160
200
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
480
Specific Heat Capacity, J/kg-K 900
870
Thermal Conductivity, W/m-K 200
140
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
21
Electrical Conductivity: Equal Weight (Specific), % IACS 180
65

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
10
Density, g/cm3 2.7
2.9
Embodied Carbon, kg CO2/kg material 8.3
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
29 to 40
Resilience: Unit (Modulus of Resilience), kJ/m3 280
1100 to 1500
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
47
Strength to Weight: Axial, points 23
47 to 51
Strength to Weight: Bending, points 30
47 to 50
Thermal Diffusivity, mm2/s 84
54
Thermal Shock Resistance, points 10
21 to 23

Alloy Composition

Aluminum (Al), % 97.9 to 99.3
87.9 to 92.4
Chromium (Cr), % 0
0.1 to 0.3
Copper (Cu), % 0 to 0.050
0.5 to 1.0
Iron (Fe), % 0 to 0.4
0 to 0.5
Magnesium (Mg), % 0.4 to 0.9
2.6 to 3.7
Manganese (Mn), % 0
0.1 to 0.4
Silicon (Si), % 0.3 to 0.7
0 to 0.5
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
4.3 to 5.2
Zirconium (Zr), % 0
0 to 0.2
Residuals, % 0
0 to 0.15