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6101A Aluminum vs. 5042 Aluminum

Both 6101A aluminum and 5042 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 6101A aluminum and the bottom bar is 5042 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 11
1.1 to 3.4
Fatigue Strength, MPa 80
97 to 120
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 130
200
Tensile Strength: Ultimate (UTS), MPa 220
340 to 360
Tensile Strength: Yield (Proof), MPa 190
270 to 310

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 160
180
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
570
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 200
130
Thermal Expansion, µm/m-K 23
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 55
33
Electrical Conductivity: Equal Weight (Specific), % IACS 180
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.3
8.8
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24
3.6 to 12
Resilience: Unit (Modulus of Resilience), kJ/m3 280
550 to 720
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
50
Strength to Weight: Axial, points 23
35 to 37
Strength to Weight: Bending, points 30
40 to 42
Thermal Diffusivity, mm2/s 84
53
Thermal Shock Resistance, points 10
15 to 16

Alloy Composition

Aluminum (Al), % 97.9 to 99.3
94.2 to 96.8
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0 to 0.050
0 to 0.15
Iron (Fe), % 0 to 0.4
0 to 0.35
Magnesium (Mg), % 0.4 to 0.9
3.0 to 4.0
Manganese (Mn), % 0
0.2 to 0.5
Silicon (Si), % 0.3 to 0.7
0 to 0.2
Titanium (Ti), % 0
0 to 0.1
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15