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EN AC-45300 Aluminum vs. EN 1.8201 Steel

EN AC-45300 aluminum belongs to the aluminum alloys classification, while EN 1.8201 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 AC-45300 aluminum and the bottom bar is EN 1.8201 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 94 to 120
190
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 1.0 to 2.8
20
Fatigue Strength, MPa 59 to 72
310
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Tensile Strength: Ultimate (UTS), MPa 220 to 290
630
Tensile Strength: Yield (Proof), MPa 150 to 230
450

Thermal Properties

Latent Heat of Fusion, J/g 470
250
Maximum Temperature: Mechanical, °C 170
450
Melting Completion (Liquidus), °C 630
1500
Melting Onset (Solidus), °C 590
1450
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 150
40
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.0
2.5
Embodied Energy, MJ/kg 150
36
Embodied Water, L/kg 1120
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.7 to 5.6
110
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 390
530
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 23 to 29
22
Strength to Weight: Bending, points 30 to 35
20
Thermal Diffusivity, mm2/s 60
11
Thermal Shock Resistance, points 10 to 13
18

Alloy Composition


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Aluminum (Al), % 90.2 to 94.2
0 to 0.030
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0
1.9 to 2.6
Copper (Cu), % 1.0 to 1.5
0
Iron (Fe), % 0 to 0.65
93.6 to 96.2
Lead (Pb), % 0 to 0.15
0
Magnesium (Mg), % 0.35 to 0.65
0
Manganese (Mn), % 0 to 0.55
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0 to 0.25
0
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 4.5 to 5.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0 to 0.25
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0