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EN 1.8201 Steel vs. 4006 Aluminum

EN 1.8201 steel belongs to the iron alloys classification, while 4006 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 EN 1.8201 steel and the bottom bar is 4006 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
28 to 45
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 20
3.4 to 24
Fatigue Strength, MPa 310
35 to 110
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 390
70 to 91
Tensile Strength: Ultimate (UTS), MPa 630
110 to 160
Tensile Strength: Yield (Proof), MPa 450
62 to 140

Thermal Properties

Latent Heat of Fusion, J/g 250
410
Maximum Temperature: Mechanical, °C 450
160
Melting Completion (Liquidus), °C 1500
640
Melting Onset (Solidus), °C 1450
620
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 40
220
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.8
56
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
180

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.0
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 2.5
8.1
Embodied Energy, MJ/kg 36
150
Embodied Water, L/kg 59
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
5.1 to 26
Resilience: Unit (Modulus of Resilience), kJ/m3 530
28 to 130
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 22
11 to 16
Strength to Weight: Bending, points 20
19 to 24
Thermal Diffusivity, mm2/s 11
89
Thermal Shock Resistance, points 18
4.9 to 7.0

Alloy Composition

Aluminum (Al), % 0 to 0.030
97.4 to 98.7
Boron (B), % 0.0010 to 0.0060
0
Carbon (C), % 0.040 to 0.1
0
Chromium (Cr), % 1.9 to 2.6
0 to 0.2
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 93.6 to 96.2
0.5 to 0.8
Magnesium (Mg), % 0
0 to 0.010
Manganese (Mn), % 0.1 to 0.6
0 to 0.050
Molybdenum (Mo), % 0.050 to 0.3
0
Niobium (Nb), % 0.020 to 0.080
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.5
0.8 to 1.2
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0.0050 to 0.060
0
Tungsten (W), % 1.5 to 1.8
0
Vanadium (V), % 0.2 to 0.3
0
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.15