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4006 Aluminum vs. SAE-AISI 4340M Steel

4006 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 4006 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 45
710
Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 3.4 to 24
6.0
Fatigue Strength, MPa 35 to 110
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 70 to 91
1360
Tensile Strength: Ultimate (UTS), MPa 110 to 160
2340
Tensile Strength: Yield (Proof), MPa 62 to 140
1240

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 160
430
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 620
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 220
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 56
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 180
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
3.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1180
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.1 to 26
120
Resilience: Unit (Modulus of Resilience), kJ/m3 28 to 130
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 11 to 16
84
Strength to Weight: Bending, points 19 to 24
51
Thermal Diffusivity, mm2/s 89
10
Thermal Shock Resistance, points 4.9 to 7.0
70

Alloy Composition

Aluminum (Al), % 97.4 to 98.7
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0 to 0.2
0.7 to 1.0
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0.5 to 0.8
93.3 to 94.8
Magnesium (Mg), % 0 to 0.010
0
Manganese (Mn), % 0 to 0.050
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0.8 to 1.2
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.15
0