EN 1.6554 Steel vs. 355.0 Aluminum
EN 1.6554 steel belongs to the iron alloys classification, while 355.0 aluminum belongs to the aluminum 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 1.6554 steel and the bottom bar is 355.0 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 230 to 280 | |
72 to 83 |
Elastic (Young's, Tensile) Modulus, GPa | 190 | |
71 |
Elongation at Break, % | 17 to 21 | |
1.5 to 2.6 |
Fatigue Strength, MPa | 380 to 520 | |
55 to 70 |
Poisson's Ratio | 0.29 | |
0.33 |
Shear Modulus, GPa | 73 | |
27 |
Tensile Strength: Ultimate (UTS), MPa | 780 to 930 | |
200 to 260 |
Tensile Strength: Yield (Proof), MPa | 550 to 790 | |
150 to 190 |
Thermal Properties
Latent Heat of Fusion, J/g | 250 | |
470 |
Maximum Temperature: Mechanical, °C | 420 | |
180 |
Melting Completion (Liquidus), °C | 1460 | |
620 |
Melting Onset (Solidus), °C | 1420 | |
560 |
Specific Heat Capacity, J/kg-K | 470 | |
890 |
Thermal Conductivity, W/m-K | 40 | |
150 to 170 |
Thermal Expansion, µm/m-K | 13 | |
22 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 7.6 | |
38 to 43 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 8.7 | |
120 to 140 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 3.4 | |
9.5 |
Density, g/cm3 | 7.9 | |
2.7 |
Embodied Carbon, kg CO2/kg material | 1.7 | |
8.0 |
Embodied Energy, MJ/kg | 22 | |
150 |
Embodied Water, L/kg | 53 | |
1120 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 140 to 150 | |
2.7 to 5.9 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 810 to 1650 | |
150 to 250 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 24 | |
51 |
Strength to Weight: Axial, points | 27 to 33 | |
20 to 27 |
Strength to Weight: Bending, points | 24 to 27 | |
28 to 33 |
Thermal Diffusivity, mm2/s | 11 | |
60 to 69 |
Thermal Shock Resistance, points | 23 to 27 | |
9.1 to 12 |
Alloy Composition
Aluminum (Al), % | 0 | |
90.3 to 94.1 |
Carbon (C), % | 0.23 to 0.28 | |
0 |
Chromium (Cr), % | 0.7 to 0.9 | |
0 to 0.25 |
Copper (Cu), % | 0 to 0.3 | |
1.0 to 1.5 |
Iron (Fe), % | 94.6 to 97.3 | |
0 to 0.6 |
Magnesium (Mg), % | 0 | |
0.4 to 0.6 |
Manganese (Mn), % | 0.6 to 0.9 | |
0 to 0.5 |
Molybdenum (Mo), % | 0.2 to 0.3 | |
0 |
Nickel (Ni), % | 1.0 to 2.0 | |
0 |
Phosphorus (P), % | 0 to 0.030 | |
0 |
Silicon (Si), % | 0 to 0.6 | |
4.5 to 5.5 |
Sulfur (S), % | 0 to 0.025 | |
0 |
Titanium (Ti), % | 0 | |
0 to 0.25 |
Vanadium (V), % | 0 to 0.030 | |
0 |
Zinc (Zn), % | 0 | |
0 to 0.35 |
Residuals, % | 0 | |
0 to 0.15 |