6110A Aluminum vs. ASTM A387 Grade 21 Steel
6110A aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 21 steel belongs to the iron alloys. There are 30 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 6110A aluminum and the bottom bar is ASTM A387 grade 21 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 70 | |
190 |
Elongation at Break, % | 11 to 18 | |
21 |
Fatigue Strength, MPa | 140 to 210 | |
160 to 250 |
Poisson's Ratio | 0.33 | |
0.29 |
Shear Modulus, GPa | 26 | |
74 |
Shear Strength, MPa | 220 to 280 | |
310 to 370 |
Tensile Strength: Ultimate (UTS), MPa | 360 to 470 | |
500 to 590 |
Tensile Strength: Yield (Proof), MPa | 250 to 430 | |
230 to 350 |
Thermal Properties
Latent Heat of Fusion, J/g | 410 | |
260 |
Maximum Temperature: Mechanical, °C | 190 | |
480 |
Melting Completion (Liquidus), °C | 650 | |
1470 |
Melting Onset (Solidus), °C | 600 | |
1430 |
Specific Heat Capacity, J/kg-K | 900 | |
470 |
Thermal Conductivity, W/m-K | 160 | |
41 |
Thermal Expansion, µm/m-K | 23 | |
13 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 42 | |
7.6 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 140 | |
8.8 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
4.1 |
Density, g/cm3 | 2.8 | |
7.9 |
Embodied Carbon, kg CO2/kg material | 8.4 | |
1.8 |
Embodied Energy, MJ/kg | 150 | |
23 |
Embodied Water, L/kg | 1170 | |
62 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 47 to 58 | |
84 to 110 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 450 to 1300 | |
140 to 320 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 50 | |
24 |
Strength to Weight: Axial, points | 36 to 47 | |
18 to 21 |
Strength to Weight: Bending, points | 41 to 48 | |
18 to 20 |
Thermal Diffusivity, mm2/s | 65 | |
11 |
Thermal Shock Resistance, points | 16 to 21 | |
14 to 17 |
Alloy Composition
Aluminum (Al), % | 94.8 to 98 | |
0 |
Carbon (C), % | 0 | |
0.050 to 0.15 |
Chromium (Cr), % | 0.050 to 0.25 | |
2.8 to 3.3 |
Copper (Cu), % | 0.3 to 0.8 | |
0 |
Iron (Fe), % | 0 to 0.5 | |
94.4 to 96 |
Magnesium (Mg), % | 0.7 to 1.1 | |
0 |
Manganese (Mn), % | 0.3 to 0.9 | |
0.3 to 0.6 |
Molybdenum (Mo), % | 0 | |
0.9 to 1.1 |
Phosphorus (P), % | 0 | |
0 to 0.025 |
Silicon (Si), % | 0.7 to 1.1 | |
0 to 0.5 |
Sulfur (S), % | 0 | |
0 to 0.025 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 0 to 0.2 | |
0 |
Zirconium (Zr), % | 0 to 0.2 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |