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1200 Aluminum vs. 2618 Aluminum

Both 1200 aluminum and 2618 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 1200 aluminum and the bottom bar is 2618 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 23 to 48
120
Elastic (Young's, Tensile) Modulus, GPa 69
71
Elongation at Break, % 1.1 to 28
5.8
Fatigue Strength, MPa 25 to 69
110
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 54 to 100
260
Tensile Strength: Ultimate (UTS), MPa 85 to 180
420
Tensile Strength: Yield (Proof), MPa 28 to 160
350

Thermal Properties

Latent Heat of Fusion, J/g 400
390
Maximum Temperature: Mechanical, °C 170
210
Melting Completion (Liquidus), °C 660
640
Melting Onset (Solidus), °C 650
550
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 230
160
Thermal Expansion, µm/m-K 23
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 58
37
Electrical Conductivity: Equal Weight (Specific), % IACS 190
110

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
11
Density, g/cm3 2.7
2.9
Embodied Carbon, kg CO2/kg material 8.2
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.0 to 19
23
Resilience: Unit (Modulus of Resilience), kJ/m3 5.7 to 180
850
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
47
Strength to Weight: Axial, points 8.7 to 19
40
Strength to Weight: Bending, points 16 to 26
42
Thermal Diffusivity, mm2/s 92
62
Thermal Shock Resistance, points 3.8 to 8.1
19

Alloy Composition

Aluminum (Al), % 99 to 100
92.4 to 94.9
Copper (Cu), % 0 to 0.050
1.9 to 2.7
Iron (Fe), % 0 to 1.0
0.9 to 1.3
Magnesium (Mg), % 0
1.3 to 1.8
Manganese (Mn), % 0 to 0.050
0
Nickel (Ni), % 0
0.9 to 1.2
Silicon (Si), % 0 to 1.0
0.1 to 0.25
Titanium (Ti), % 0 to 0.050
0.040 to 0.1
Zinc (Zn), % 0 to 0.1
0 to 0.1
Residuals, % 0
0 to 0.15