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2124 Aluminum vs. 6101A Aluminum

Both 2124 aluminum and 6101A aluminum are aluminum alloys. They have a moderately high 94% of their average alloy composition in common.

For each property being compared, the top bar is 2124 aluminum and the bottom bar is 6101A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
68
Elongation at Break, % 5.7
11
Fatigue Strength, MPa 130
80
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
26
Shear Strength, MPa 280
130
Tensile Strength: Ultimate (UTS), MPa 490
220
Tensile Strength: Yield (Proof), MPa 430
190

Thermal Properties

Latent Heat of Fusion, J/g 390
400
Maximum Temperature: Mechanical, °C 190
160
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 500
630
Specific Heat Capacity, J/kg-K 880
900
Thermal Conductivity, W/m-K 150
200
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
55
Electrical Conductivity: Equal Weight (Specific), % IACS 110
180

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.5
Density, g/cm3 3.0
2.7
Embodied Carbon, kg CO2/kg material 8.2
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27
24
Resilience: Unit (Modulus of Resilience), kJ/m3 1290
280
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
51
Strength to Weight: Axial, points 45
23
Strength to Weight: Bending, points 46
30
Thermal Diffusivity, mm2/s 58
84
Thermal Shock Resistance, points 21
10

Alloy Composition


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Aluminum (Al), % 91.3 to 94.7
97.9 to 99.3
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 3.8 to 4.9
0 to 0.050
Iron (Fe), % 0 to 0.3
0 to 0.4
Magnesium (Mg), % 1.2 to 1.8
0.4 to 0.9
Manganese (Mn), % 0.3 to 0.9
0
Silicon (Si), % 0 to 0.2
0.3 to 0.7
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0 to 0.1