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2618 Aluminum vs. 1200 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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