512.0 Aluminum vs. EN AC-21200 Aluminum
Both 512.0 aluminum and EN AC-21200 aluminum are aluminum alloys. They have a moderately high 94% of their average alloy composition in common.
For each property being compared, the top bar is 512.0 aluminum and the bottom bar is EN AC-21200 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 50 | |
| 120 to 130 | 
| Elastic (Young's, Tensile) Modulus, GPa | 69 | |
| 71 | 
| Elongation at Break, % | 2.0 | |
| 3.9 to 6.2 | 
| Fatigue Strength, MPa | 58 | |
| 110 to 130 | 
| Poisson's Ratio | 0.33 | |
| 0.33 | 
| Shear Modulus, GPa | 26 | |
| 27 | 
| Tensile Strength: Ultimate (UTS), MPa | 130 | |
| 410 to 440 | 
| Tensile Strength: Yield (Proof), MPa | 83 | |
| 270 to 360 | 
Thermal Properties
| Latent Heat of Fusion, J/g | 420 | |
| 390 | 
| Maximum Temperature: Mechanical, °C | 180 | |
| 170 | 
| Melting Completion (Liquidus), °C | 630 | |
| 660 | 
| Melting Onset (Solidus), °C | 590 | |
| 550 | 
| Specific Heat Capacity, J/kg-K | 900 | |
| 880 | 
| Thermal Conductivity, W/m-K | 150 | |
| 130 | 
| Thermal Expansion, µm/m-K | 23 | |
| 23 | 
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 38 | |
| 34 | 
| Electrical Conductivity: Equal Weight (Specific), % IACS | 130 | |
| 100 | 
Otherwise Unclassified Properties
| Base Metal Price, % relative | 9.5 | |
| 10 | 
| Density, g/cm3 | 2.7 | |
| 3.0 | 
| Embodied Carbon, kg CO2/kg material | 8.8 | |
| 8.0 | 
| Embodied Energy, MJ/kg | 150 | |
| 150 | 
| Embodied Water, L/kg | 1160 | |
| 1150 | 
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 2.3 | |
| 16 to 22 | 
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 50 | |
| 500 to 930 | 
| Stiffness to Weight: Axial, points | 14 | |
| 13 | 
| Stiffness to Weight: Bending, points | 51 | |
| 46 | 
| Strength to Weight: Axial, points | 14 | |
| 38 to 40 | 
| Strength to Weight: Bending, points | 22 | |
| 41 to 43 | 
| Thermal Diffusivity, mm2/s | 60 | |
| 49 | 
| Thermal Shock Resistance, points | 6.1 | |
| 18 to 19 | 
Alloy Composition
| Aluminum (Al), % | 90.6 to 95.1 | |
| 93.3 to 95.7 | 
| Chromium (Cr), % | 0 to 0.25 | |
| 0 | 
| Copper (Cu), % | 0 to 0.35 | |
| 4.0 to 5.0 | 
| Iron (Fe), % | 0 to 0.6 | |
| 0 to 0.2 | 
| Lead (Pb), % | 0 | |
| 0 to 0.030 | 
| Magnesium (Mg), % | 3.5 to 4.5 | |
| 0.15 to 0.5 | 
| Manganese (Mn), % | 0 to 0.8 | |
| 0.2 to 0.5 | 
| Nickel (Ni), % | 0 | |
| 0 to 0.050 | 
| Silicon (Si), % | 1.4 to 2.2 | |
| 0 to 0.1 | 
| Tin (Sn), % | 0 | |
| 0 to 0.030 | 
| Titanium (Ti), % | 0 to 0.25 | |
| 0 to 0.1 | 
| Zinc (Zn), % | 0 to 0.35 | |
| 0 to 0.1 | 
| Residuals, % | 0 | |
| 0 to 0.1 |