R05255 Alloy vs. 4032 Aluminum
R05255 alloy belongs to the otherwise unclassified metals classification, while 4032 aluminum belongs to the aluminum alloys. There are 20 material properties with values for both materials. Properties with values for just one material (11, 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 R05255 alloy and the bottom bar is 4032 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 73 |
| Elongation at Break, % | 20 | |
| 6.7 |
| Poisson's Ratio | 0.34 | |
| 0.33 |
| Shear Modulus, GPa | 70 | |
| 28 |
| Tensile Strength: Ultimate (UTS), MPa | 540 | |
| 390 |
| Tensile Strength: Yield (Proof), MPa | 450 | |
| 320 |
Thermal Properties
| Latent Heat of Fusion, J/g | 140 | |
| 570 |
| Specific Heat Capacity, J/kg-K | 140 | |
| 900 |
| Thermal Conductivity, W/m-K | 59 | |
| 140 |
| Thermal Expansion, µm/m-K | 6.6 | |
| 19 |
Otherwise Unclassified Properties
| Density, g/cm3 | 17 | |
| 2.6 |
| Embodied Water, L/kg | 630 | |
| 1030 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 100 | |
| 25 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 530 | |
| 700 |
| Stiffness to Weight: Axial, points | 6.3 | |
| 15 |
| Stiffness to Weight: Bending, points | 11 | |
| 53 |
| Strength to Weight: Axial, points | 9.1 | |
| 41 |
| Strength to Weight: Bending, points | 8.9 | |
| 45 |
| Thermal Diffusivity, mm2/s | 25 | |
| 59 |
| Thermal Shock Resistance, points | 31 | |
| 20 |
Alloy Composition
Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
| Aluminum (Al), % | 0 | |
| 81.1 to 87.2 |
| Carbon (C), % | 0 to 0.010 | |
| 0 |
| Chromium (Cr), % | 0 | |
| 0 to 0.1 |
| Copper (Cu), % | 0 | |
| 0.5 to 1.3 |
| Hydrogen (H), % | 0 to 0.0015 | |
| 0 |
| Iron (Fe), % | 0 to 0.010 | |
| 0 to 1.0 |
| Magnesium (Mg), % | 0 | |
| 0.8 to 1.3 |
| Molybdenum (Mo), % | 0 to 0.020 | |
| 0 |
| Nickel (Ni), % | 0 to 0.010 | |
| 0.5 to 1.3 |
| Niobium (Nb), % | 0 to 0.5 | |
| 0 |
| Nitrogen (N), % | 0 to 0.010 | |
| 0 |
| Oxygen (O), % | 0 to 0.015 | |
| 0 |
| Silicon (Si), % | 0 to 0.0050 | |
| 11 to 13.5 |
| Tantalum (Ta), % | 95.9 to 98 | |
| 0 |
| Titanium (Ti), % | 0 to 0.010 | |
| 0 |
| Tungsten (W), % | 2.0 to 3.5 | |
| 0 |
| Zinc (Zn), % | 0 | |
| 0 to 0.25 |
| Residuals, % | 0 | |
| 0 to 0.15 |