336.0 Aluminum vs. SAE-AISI 5130 Steel
336.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 5130 steel belongs to the iron alloys. 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 336.0 aluminum and the bottom bar is SAE-AISI 5130 steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 110 to 130 | |
| 150 to 190 |
| Elastic (Young's, Tensile) Modulus, GPa | 75 | |
| 190 |
| Elongation at Break, % | 0.5 | |
| 12 to 22 |
| Fatigue Strength, MPa | 80 to 93 | |
| 230 to 330 |
| Poisson's Ratio | 0.33 | |
| 0.29 |
| Shear Modulus, GPa | 28 | |
| 73 |
| Shear Strength, MPa | 190 to 250 | |
| 310 to 390 |
| Tensile Strength: Ultimate (UTS), MPa | 250 to 320 | |
| 500 to 640 |
| Tensile Strength: Yield (Proof), MPa | 190 to 300 | |
| 330 to 530 |
Thermal Properties
| Latent Heat of Fusion, J/g | 570 | |
| 250 |
| Maximum Temperature: Mechanical, °C | 210 | |
| 420 |
| Melting Completion (Liquidus), °C | 570 | |
| 1460 |
| Melting Onset (Solidus), °C | 540 | |
| 1420 |
| Specific Heat Capacity, J/kg-K | 890 | |
| 470 |
| Thermal Conductivity, W/m-K | 120 | |
| 45 |
| Thermal Expansion, µm/m-K | 19 | |
| 12 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 29 | |
| 7.2 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 95 | |
| 8.3 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 2.2 |
| Density, g/cm3 | 2.8 | |
| 7.8 |
| Embodied Carbon, kg CO2/kg material | 7.9 | |
| 1.4 |
| Embodied Energy, MJ/kg | 140 | |
| 19 |
| Embodied Water, L/kg | 1010 | |
| 50 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 1.1 to 1.6 | |
| 74 to 98 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 250 to 580 | |
| 290 to 750 |
| Stiffness to Weight: Axial, points | 15 | |
| 13 |
| Stiffness to Weight: Bending, points | 51 | |
| 24 |
| Strength to Weight: Axial, points | 25 to 32 | |
| 18 to 23 |
| Strength to Weight: Bending, points | 32 to 38 | |
| 18 to 21 |
| Thermal Diffusivity, mm2/s | 48 | |
| 12 |
| Thermal Shock Resistance, points | 12 to 16 | |
| 16 to 20 |
Alloy Composition
| Aluminum (Al), % | 79.1 to 85.8 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.28 to 0.33 |
| Chromium (Cr), % | 0 | |
| 0.8 to 1.1 |
| Copper (Cu), % | 0.5 to 1.5 | |
| 0 |
| Iron (Fe), % | 0 to 1.2 | |
| 97.2 to 98.1 |
| Magnesium (Mg), % | 0.7 to 1.3 | |
| 0 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0.7 to 0.9 |
| Nickel (Ni), % | 2.0 to 3.0 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.035 |
| Silicon (Si), % | 11 to 13 | |
| 0.15 to 0.35 |
| Sulfur (S), % | 0 | |
| 0 to 0.040 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 0.35 | |
| 0 |