SAE-AISI 4130 Steel vs. N08028 Stainless Steel
Both SAE-AISI 4130 steel and N08028 stainless steel are iron alloys. They have a modest 37% of their average alloy composition in common, which, by itself, doesn't mean much. There are 29 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.
For each property being compared, the top bar is SAE-AISI 4130 steel and the bottom bar is N08028 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Brinell Hardness | 200 to 300 | |
| 180 |
| Elastic (Young's, Tensile) Modulus, GPa | 190 | |
| 200 |
| Elongation at Break, % | 13 to 26 | |
| 45 |
| Fatigue Strength, MPa | 320 to 660 | |
| 220 |
| Poisson's Ratio | 0.29 | |
| 0.28 |
| Shear Modulus, GPa | 73 | |
| 80 |
| Shear Strength, MPa | 340 to 640 | |
| 400 |
| Tensile Strength: Ultimate (UTS), MPa | 530 to 1040 | |
| 570 |
| Tensile Strength: Yield (Proof), MPa | 440 to 980 | |
| 240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 250 | |
| 320 |
| Maximum Temperature: Mechanical, °C | 420 | |
| 1100 |
| Melting Completion (Liquidus), °C | 1460 | |
| 1420 |
| Melting Onset (Solidus), °C | 1420 | |
| 1370 |
| Specific Heat Capacity, J/kg-K | 470 | |
| 470 |
| Thermal Conductivity, W/m-K | 43 | |
| 12 |
| Thermal Expansion, µm/m-K | 13 | |
| 16 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 2.4 | |
| 37 |
| Density, g/cm3 | 7.8 | |
| 8.1 |
| Embodied Carbon, kg CO2/kg material | 1.5 | |
| 6.4 |
| Embodied Energy, MJ/kg | 20 | |
| 89 |
| Embodied Water, L/kg | 50 | |
| 240 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 83 to 180 | |
| 210 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 500 to 2550 | |
| 140 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 24 | |
| 24 |
| Strength to Weight: Axial, points | 19 to 37 | |
| 19 |
| Strength to Weight: Bending, points | 19 to 29 | |
| 19 |
| Thermal Diffusivity, mm2/s | 12 | |
| 3.2 |
| Thermal Shock Resistance, points | 16 to 31 | |
| 12 |
Alloy Composition
| Carbon (C), % | 0.28 to 0.33 | |
| 0 to 0.030 |
| Chromium (Cr), % | 0.8 to 1.1 | |
| 26 to 28 |
| Copper (Cu), % | 0 | |
| 0.6 to 1.4 |
| Iron (Fe), % | 97.3 to 98.2 | |
| 29 to 40.4 |
| Manganese (Mn), % | 0.4 to 0.6 | |
| 0 to 2.5 |
| Molybdenum (Mo), % | 0.15 to 0.25 | |
| 3.0 to 4.0 |
| Nickel (Ni), % | 0 | |
| 30 to 34 |
| Phosphorus (P), % | 0 to 0.035 | |
| 0 to 0.030 |
| Silicon (Si), % | 0.15 to 0.35 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 to 0.040 | |
| 0 to 0.030 |