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4145 Aluminum vs. K1A Magnesium

4145 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 4145 aluminum and the bottom bar is K1A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
43
Elongation at Break, % 2.2
13
Fatigue Strength, MPa 48
39
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
17
Shear Strength, MPa 69
55
Tensile Strength: Ultimate (UTS), MPa 120
180
Tensile Strength: Yield (Proof), MPa 68
51

Thermal Properties

Latent Heat of Fusion, J/g 540
350
Maximum Temperature: Mechanical, °C 160
120
Melting Completion (Liquidus), °C 590
650
Melting Onset (Solidus), °C 520
650
Specific Heat Capacity, J/kg-K 880
1000
Thermal Conductivity, W/m-K 100
120
Thermal Expansion, µm/m-K 21
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
30
Electrical Conductivity: Equal Weight (Specific), % IACS 84
170

Otherwise Unclassified Properties

Base Metal Price, % relative 10
13
Density, g/cm3 2.8
1.6
Embodied Carbon, kg CO2/kg material 7.6
24
Embodied Energy, MJ/kg 140
170
Embodied Water, L/kg 1040
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
17
Resilience: Unit (Modulus of Resilience), kJ/m3 31
30
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
73
Strength to Weight: Axial, points 12
31
Strength to Weight: Bending, points 19
43
Thermal Diffusivity, mm2/s 42
75
Thermal Shock Resistance, points 5.5
11

Alloy Composition


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Aluminum (Al), % 83 to 87.4
0
Chromium (Cr), % 0 to 0.15
0
Copper (Cu), % 3.3 to 4.7
0
Iron (Fe), % 0 to 0.8
0
Magnesium (Mg), % 0 to 0.15
98.7 to 99.6
Manganese (Mn), % 0 to 0.15
0
Silicon (Si), % 9.3 to 10.7
0
Zinc (Zn), % 0 to 0.2
0
Zirconium (Zr), % 0
0.4 to 1.0
Residuals, % 0 to 0.15
0 to 0.3