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7022 Aluminum vs. 6101A Aluminum

Both 7022 aluminum and 6101A 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 7022 aluminum and the bottom bar is 6101A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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