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4007 Aluminum vs. SAE-AISI 4340M Steel

4007 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 4007 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 32 to 44
710
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.1 to 23
6.0
Fatigue Strength, MPa 46 to 88
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
72
Shear Strength, MPa 80 to 90
1360
Tensile Strength: Ultimate (UTS), MPa 130 to 160
2340
Tensile Strength: Yield (Proof), MPa 50 to 120
1240

Thermal Properties

Latent Heat of Fusion, J/g 410
280
Maximum Temperature: Mechanical, °C 170
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 590
1400
Specific Heat Capacity, J/kg-K 890
480
Thermal Conductivity, W/m-K 170
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 42
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 140
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1160
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.4 to 23
120
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 110
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
25
Strength to Weight: Axial, points 12 to 15
84
Strength to Weight: Bending, points 20 to 23
51
Thermal Diffusivity, mm2/s 67
10
Thermal Shock Resistance, points 5.5 to 6.7
70

Alloy Composition

Aluminum (Al), % 94.1 to 97.6
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0.050 to 0.25
0.7 to 1.0
Cobalt (Co), % 0 to 0.050
0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0.4 to 1.0
93.3 to 94.8
Magnesium (Mg), % 0 to 0.2
0
Manganese (Mn), % 0.8 to 1.5
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0.15 to 0.7
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 1.0 to 1.7
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0