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6360 Aluminum vs. 5051A Aluminum

Both 6360 aluminum and 5051A aluminum are aluminum alloys. They have a very high 98% of their average alloy composition in common.

For each property being compared, the top bar is 6360 aluminum and the bottom bar is 5051A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 9.0 to 18
18 to 21
Fatigue Strength, MPa 31 to 67
51 to 61
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 76 to 130
110
Tensile Strength: Ultimate (UTS), MPa 120 to 220
170
Tensile Strength: Yield (Proof), MPa 57 to 170
56

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 160
190
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 630
610
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 210
150
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
39
Electrical Conductivity: Equal Weight (Specific), % IACS 180
130

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
8.5
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 19
24 to 27
Resilience: Unit (Modulus of Resilience), kJ/m3 24 to 210
23
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 13 to 23
17 to 18
Strength to Weight: Bending, points 20 to 30
25
Thermal Diffusivity, mm2/s 86
63
Thermal Shock Resistance, points 5.5 to 9.9
7.6

Alloy Composition

Aluminum (Al), % 97.8 to 99.3
96.1 to 98.6
Chromium (Cr), % 0 to 0.050
0 to 0.3
Copper (Cu), % 0 to 0.15
0 to 0.050
Iron (Fe), % 0.1 to 0.3
0 to 0.45
Magnesium (Mg), % 0.25 to 0.45
1.4 to 2.1
Manganese (Mn), % 0.020 to 0.15
0 to 0.25
Silicon (Si), % 0.35 to 0.8
0 to 0.3
Titanium (Ti), % 0 to 0.1
0 to 0.1
Zinc (Zn), % 0 to 0.1
0 to 0.2
Residuals, % 0
0 to 0.15