242.0 Aluminum vs. 5252 Aluminum
Both 242.0 aluminum and 5252 aluminum are aluminum alloys. They have a moderately high 93% of their average alloy composition in common. There are 31 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown.
For each property being compared, the top bar is 242.0 aluminum and the bottom bar is 5252 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Brinell Hardness | 70 to 110 | |
68 to 75 |
Elastic (Young's, Tensile) Modulus, GPa | 73 | |
68 |
Elongation at Break, % | 0.5 to 1.5 | |
4.5 to 11 |
Fatigue Strength, MPa | 55 to 110 | |
100 to 110 |
Poisson's Ratio | 0.33 | |
0.33 |
Shear Modulus, GPa | 27 | |
25 |
Shear Strength, MPa | 150 to 240 | |
140 to 160 |
Tensile Strength: Ultimate (UTS), MPa | 180 to 290 | |
230 to 290 |
Tensile Strength: Yield (Proof), MPa | 120 to 220 | |
170 to 240 |
Thermal Properties
Latent Heat of Fusion, J/g | 390 | |
400 |
Maximum Temperature: Mechanical, °C | 210 | |
180 |
Melting Completion (Liquidus), °C | 640 | |
650 |
Melting Onset (Solidus), °C | 530 | |
610 |
Specific Heat Capacity, J/kg-K | 870 | |
910 |
Thermal Conductivity, W/m-K | 130 to 170 | |
140 |
Thermal Expansion, µm/m-K | 22 | |
24 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 33 to 44 | |
34 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 96 to 130 | |
120 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 12 | |
9.5 |
Density, g/cm3 | 3.1 | |
2.7 |
Embodied Carbon, kg CO2/kg material | 8.3 | |
8.7 |
Embodied Energy, MJ/kg | 150 | |
160 |
Embodied Water, L/kg | 1130 | |
1190 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 1.3 to 3.4 | |
12 to 23 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 340 | |
210 to 430 |
Stiffness to Weight: Axial, points | 13 | |
14 |
Stiffness to Weight: Bending, points | 45 | |
51 |
Strength to Weight: Axial, points | 16 to 26 | |
23 to 30 |
Strength to Weight: Bending, points | 23 to 32 | |
31 to 36 |
Thermal Diffusivity, mm2/s | 50 to 62 | |
57 |
Thermal Shock Resistance, points | 8.0 to 13 | |
10 to 13 |
Alloy Composition
Aluminum (Al), % | 88.4 to 93.6 | |
96.6 to 97.8 |
Chromium (Cr), % | 0 to 0.25 | |
0 |
Copper (Cu), % | 3.5 to 4.5 | |
0 to 0.1 |
Iron (Fe), % | 0 to 1.0 | |
0 to 0.1 |
Magnesium (Mg), % | 1.2 to 1.8 | |
2.2 to 2.8 |
Manganese (Mn), % | 0 to 0.35 | |
0 to 0.1 |
Nickel (Ni), % | 1.7 to 2.3 | |
0 |
Silicon (Si), % | 0 to 0.7 | |
0 to 0.080 |
Titanium (Ti), % | 0 to 0.25 | |
0 |
Vanadium (V), % | 0 | |
0 to 0.050 |
Zinc (Zn), % | 0 to 0.35 | |
0 to 0.050 |
Residuals, % | 0 | |
0 to 0.1 |