N08800 Stainless Steel vs. EN AC-43500 Aluminum
N08800 stainless steel belongs to the iron alloys classification, while EN AC-43500 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 N08800 stainless steel and the bottom bar is EN AC-43500 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 72 |
| Elongation at Break, % | 4.5 to 34 | |
| 4.5 to 13 |
| Fatigue Strength, MPa | 150 to 390 | |
| 62 to 100 |
| Poisson's Ratio | 0.28 | |
| 0.33 |
| Shear Modulus, GPa | 77 | |
| 27 |
| Tensile Strength: Ultimate (UTS), MPa | 500 to 1000 | |
| 220 to 300 |
| Tensile Strength: Yield (Proof), MPa | 190 to 830 | |
| 140 to 170 |
Thermal Properties
| Latent Heat of Fusion, J/g | 300 | |
| 550 |
| Maximum Temperature: Mechanical, °C | 1100 | |
| 170 |
| Melting Completion (Liquidus), °C | 1390 | |
| 600 |
| Melting Onset (Solidus), °C | 1360 | |
| 590 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 900 |
| Thermal Conductivity, W/m-K | 12 | |
| 140 |
| Thermal Expansion, µm/m-K | 14 | |
| 22 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.7 | |
| 38 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.9 | |
| 130 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 30 | |
| 9.5 |
| Density, g/cm3 | 8.0 | |
| 2.6 |
| Embodied Carbon, kg CO2/kg material | 5.3 | |
| 7.8 |
| Embodied Energy, MJ/kg | 76 | |
| 150 |
| Embodied Water, L/kg | 200 | |
| 1070 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 42 to 160 | |
| 12 to 26 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 96 to 1740 | |
| 130 to 200 |
| Stiffness to Weight: Axial, points | 14 | |
| 16 |
| Stiffness to Weight: Bending, points | 24 | |
| 54 |
| Strength to Weight: Axial, points | 18 to 35 | |
| 24 to 33 |
| Strength to Weight: Bending, points | 18 to 28 | |
| 32 to 39 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 60 |
| Thermal Shock Resistance, points | 13 to 25 | |
| 10 to 14 |
Alloy Composition
| Aluminum (Al), % | 0.15 to 0.6 | |
| 86.4 to 90.5 |
| Carbon (C), % | 0 to 0.1 | |
| 0 |
| Chromium (Cr), % | 19 to 23 | |
| 0 |
| Copper (Cu), % | 0 to 0.75 | |
| 0 to 0.050 |
| Iron (Fe), % | 39.5 to 50.7 | |
| 0 to 0.25 |
| Magnesium (Mg), % | 0 | |
| 0.1 to 0.6 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0.4 to 0.8 |
| Nickel (Ni), % | 30 to 35 | |
| 0 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 9.0 to 11.5 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 |
| Titanium (Ti), % | 0.15 to 0.6 | |
| 0 to 0.2 |
| Zinc (Zn), % | 0 | |
| 0 to 0.070 |
| Residuals, % | 0 | |
| 0 to 0.15 |