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5021 Aluminum vs. 6023 Aluminum

Both 5021 aluminum and 6023 aluminum are aluminum alloys. They have a very high 97% of their average alloy composition in common.

For each property being compared, the top bar is 5021 aluminum and the bottom bar is 6023 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 1.1 to 3.4
11
Fatigue Strength, MPa 85 to 110
120 to 130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 170
210 to 220
Tensile Strength: Ultimate (UTS), MPa 300 to 310
360
Tensile Strength: Yield (Proof), MPa 240 to 270
300 to 310

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 180
160
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 590
580
Specific Heat Capacity, J/kg-K 900
890
Thermal Conductivity, W/m-K 140
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
45
Electrical Conductivity: Equal Weight (Specific), % IACS 120
140

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.6
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.1 to 10
38 to 39
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 550
670 to 690
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
49
Strength to Weight: Axial, points 30 to 32
35 to 36
Strength to Weight: Bending, points 37
40
Thermal Diffusivity, mm2/s 57
67
Thermal Shock Resistance, points 13 to 14
16

Alloy Composition

Aluminum (Al), % 95.2 to 97.7
94 to 97.7
Bismuth (Bi), % 0
0.3 to 0.8
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 0 to 0.15
0.2 to 0.5
Iron (Fe), % 0 to 0.5
0 to 0.5
Magnesium (Mg), % 2.2 to 2.8
0.4 to 0.9
Manganese (Mn), % 0.1 to 0.5
0.2 to 0.6
Silicon (Si), % 0 to 0.4
0.6 to 1.4
Tin (Sn), % 0
0.6 to 1.2
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0
0 to 0.15