Sintered 6061 Aluminum vs. EN 1.5510 Steel
Sintered 6061 aluminum belongs to the aluminum alloys classification, while EN 1.5510 steel belongs to the iron alloys. There are 29 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 sintered 6061 aluminum and the bottom bar is EN 1.5510 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
190 |
Elongation at Break, % | 0.5 to 6.0 | |
11 to 21 |
Fatigue Strength, MPa | 32 to 62 | |
220 to 330 |
Poisson's Ratio | 0.33 | |
0.29 |
Shear Modulus, GPa | 25 | |
73 |
Tensile Strength: Ultimate (UTS), MPa | 83 to 210 | |
450 to 1600 |
Tensile Strength: Yield (Proof), MPa | 62 to 190 | |
310 to 520 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
250 |
Maximum Temperature: Mechanical, °C | 170 | |
400 |
Melting Completion (Liquidus), °C | 640 | |
1460 |
Melting Onset (Solidus), °C | 610 | |
1420 |
Specific Heat Capacity, J/kg-K | 900 | |
470 |
Thermal Conductivity, W/m-K | 200 | |
51 |
Thermal Expansion, µm/m-K | 23 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 52 | |
7.1 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 170 | |
8.2 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
1.9 |
Density, g/cm3 | 2.7 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
1.4 |
Embodied Energy, MJ/kg | 150 | |
19 |
Embodied Water, L/kg | 1180 | |
47 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 0.68 to 7.0 | |
46 to 260 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 28 to 280 | |
260 to 710 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 51 | |
24 |
Strength to Weight: Axial, points | 8.6 to 21 | |
16 to 57 |
Strength to Weight: Bending, points | 16 to 29 | |
17 to 39 |
Thermal Diffusivity, mm2/s | 81 | |
14 |
Thermal Shock Resistance, points | 3.8 to 9.4 | |
13 to 47 |
Alloy Composition
Aluminum (Al), % | 96 to 99.4 | |
0 |
Boron (B), % | 0 | |
0.00080 to 0.0050 |
Carbon (C), % | 0 | |
0.25 to 0.3 |
Chromium (Cr), % | 0 | |
0 to 0.3 |
Copper (Cu), % | 0 to 0.5 | |
0 to 0.25 |
Iron (Fe), % | 0 | |
97.9 to 99.149 |
Magnesium (Mg), % | 0.4 to 1.2 | |
0 |
Manganese (Mn), % | 0 | |
0.6 to 0.9 |
Phosphorus (P), % | 0 | |
0 to 0.025 |
Silicon (Si), % | 0.2 to 0.8 | |
0 to 0.3 |
Sulfur (S), % | 0 | |
0 to 0.025 |
Residuals, % | 0 to 1.5 | |
0 |