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5449 Aluminum vs. 6101A Aluminum

Both 5449 aluminum and 6101A 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 5449 aluminum and the bottom bar is 6101A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
68
Elongation at Break, % 4.0 to 17
11
Fatigue Strength, MPa 78 to 120
80
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 130 to 190
130
Tensile Strength: Ultimate (UTS), MPa 210 to 330
220
Tensile Strength: Yield (Proof), MPa 91 to 260
190

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 190
160
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 590
630
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 140
200
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
55
Electrical Conductivity: Equal Weight (Specific), % IACS 110
180

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.8
2.7
Embodied Carbon, kg CO2/kg material 8.5
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 29
24
Resilience: Unit (Modulus of Resilience), kJ/m3 60 to 480
280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 22 to 33
23
Strength to Weight: Bending, points 29 to 39
30
Thermal Diffusivity, mm2/s 56
84
Thermal Shock Resistance, points 9.4 to 15
10

Alloy Composition


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Aluminum (Al), % 94.1 to 97.8
97.9 to 99.3
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.3
0 to 0.050
Iron (Fe), % 0 to 0.7
0 to 0.4
Magnesium (Mg), % 1.6 to 2.6
0.4 to 0.9
Manganese (Mn), % 0.6 to 1.1
0
Silicon (Si), % 0 to 0.4
0.3 to 0.7
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0 to 0.1