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5019 Aluminum vs. 6101A Aluminum

Both 5019 aluminum and 6101A aluminum are aluminum alloys. They have a moderately high 95% of their average alloy composition in common.

For each property being compared, the top bar is 5019 aluminum and the bottom bar is 6101A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 2.2 to 18
11
Fatigue Strength, MPa 100 to 160
80
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 170 to 210
130
Tensile Strength: Ultimate (UTS), MPa 280 to 360
220
Tensile Strength: Yield (Proof), MPa 120 to 300
190

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 540
630
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 130
200
Thermal Expansion, µm/m-K 24
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
55
Electrical Conductivity: Equal Weight (Specific), % IACS 98
180

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 9.0
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.6 to 40
24
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 650
280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
51
Strength to Weight: Axial, points 29 to 38
23
Strength to Weight: Bending, points 35 to 42
30
Thermal Diffusivity, mm2/s 52
84
Thermal Shock Resistance, points 13 to 16
10

Alloy Composition


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Aluminum (Al), % 91.5 to 95.3
97.9 to 99.3
Chromium (Cr), % 0 to 0.2
0
Copper (Cu), % 0 to 0.1
0 to 0.050
Iron (Fe), % 0 to 0.5
0 to 0.4
Magnesium (Mg), % 4.5 to 5.6
0.4 to 0.9
Manganese (Mn), % 0.1 to 0.6
0
Silicon (Si), % 0 to 0.4
0.3 to 0.7
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0 to 0.1