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2618 Aluminum vs. 2117 Aluminum

Both 2618 aluminum and 2117 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 2618 aluminum and the bottom bar is 2117 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
70
Elastic (Young's, Tensile) Modulus, GPa 71
71
Elongation at Break, % 5.8
26
Fatigue Strength, MPa 110
95
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 27
27
Shear Strength, MPa 260
200
Tensile Strength: Ultimate (UTS), MPa 420
300
Tensile Strength: Yield (Proof), MPa 350
170

Thermal Properties

Latent Heat of Fusion, J/g 390
400
Maximum Temperature: Mechanical, °C 210
220
Melting Completion (Liquidus), °C 640
650
Melting Onset (Solidus), °C 550
550
Specific Heat Capacity, J/kg-K 880
880
Thermal Conductivity, W/m-K 160
150
Thermal Expansion, µm/m-K 22
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
40
Electrical Conductivity: Equal Weight (Specific), % IACS 110
120

Otherwise Unclassified Properties

Base Metal Price, % relative 11
10
Density, g/cm3 2.9
3.0
Embodied Carbon, kg CO2/kg material 8.3
8.2
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1150
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23
64
Resilience: Unit (Modulus of Resilience), kJ/m3 850
190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
47
Strength to Weight: Axial, points 40
28
Strength to Weight: Bending, points 42
33
Thermal Diffusivity, mm2/s 62
59
Thermal Shock Resistance, points 19
12

Alloy Composition

Aluminum (Al), % 92.4 to 94.9
91 to 97.6
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 1.9 to 2.7
2.2 to 4.5
Iron (Fe), % 0.9 to 1.3
0 to 0.7
Magnesium (Mg), % 1.3 to 1.8
0.2 to 1.0
Manganese (Mn), % 0
0.4 to 1.0
Nickel (Ni), % 0.9 to 1.2
0
Silicon (Si), % 0.1 to 0.25
0.2 to 0.8
Titanium (Ti), % 0.040 to 0.1
0 to 0.25
Zinc (Zn), % 0 to 0.1
0 to 0.25
Zirconium (Zr), % 0
0 to 0.25
Residuals, % 0
0 to 0.15