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2618 Aluminum vs. K1A Magnesium

2618 aluminum belongs to the aluminum alloys classification, while K1A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.

For each property being compared, the top bar is 2618 aluminum and the bottom bar is K1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
43
Elongation at Break, % 5.8
13
Fatigue Strength, MPa 110
39
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
17
Shear Strength, MPa 260
55
Tensile Strength: Ultimate (UTS), MPa 420
180
Tensile Strength: Yield (Proof), MPa 350
51

Thermal Properties

Latent Heat of Fusion, J/g 390
350
Maximum Temperature: Mechanical, °C 210
120
Melting Completion (Liquidus), °C 640
650
Melting Onset (Solidus), °C 550
650
Specific Heat Capacity, J/kg-K 880
1000
Thermal Conductivity, W/m-K 160
120
Thermal Expansion, µm/m-K 22
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
30
Electrical Conductivity: Equal Weight (Specific), % IACS 110
170

Otherwise Unclassified Properties

Base Metal Price, % relative 11
13
Density, g/cm3 2.9
1.6
Embodied Carbon, kg CO2/kg material 8.3
24
Embodied Energy, MJ/kg 150
170
Embodied Water, L/kg 1150
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23
17
Resilience: Unit (Modulus of Resilience), kJ/m3 850
30
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 47
73
Strength to Weight: Axial, points 40
31
Strength to Weight: Bending, points 42
43
Thermal Diffusivity, mm2/s 62
75
Thermal Shock Resistance, points 19
11

Alloy Composition


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Aluminum (Al), % 92.4 to 94.9
0
Copper (Cu), % 1.9 to 2.7
0
Iron (Fe), % 0.9 to 1.3
0
Magnesium (Mg), % 1.3 to 1.8
98.7 to 99.6
Nickel (Ni), % 0.9 to 1.2
0
Silicon (Si), % 0.1 to 0.25
0
Titanium (Ti), % 0.040 to 0.1
0
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0 to 0.15
0 to 0.3