Hot Finished N08800 Stainless Steel vs. Hot Worked Nickel 200
Hot finished N08800 stainless steel belongs to the iron alloys classification, while hot worked nickel 200 belongs to the nickel alloys. They have a modest 33% of their average alloy composition in common, which, by itself, doesn't mean much. There are 31 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.
For each property being compared, the top bar is hot finished N08800 stainless steel and the bottom bar is hot worked nickel 200.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 200 | |
| 180 |
| Elongation at Break, % | 34 | |
| 42 |
| Fatigue Strength, MPa | 150 | |
| 120 |
| Poisson's Ratio | 0.28 | |
| 0.31 |
| Shear Modulus, GPa | 77 | |
| 70 |
| Shear Strength, MPa | 340 | |
| 330 |
| Tensile Strength: Ultimate (UTS), MPa | 500 | |
| 480 |
| Tensile Strength: Yield (Proof), MPa | 190 | |
| 150 |
Thermal Properties
| Curie Temperature, °C | -120 | |
| 360 |
| Latent Heat of Fusion, J/g | 300 | |
| 290 |
| Maximum Temperature: Mechanical, °C | 1100 | |
| 900 |
| Melting Completion (Liquidus), °C | 1390 | |
| 1460 |
| Melting Onset (Solidus), °C | 1360 | |
| 1440 |
| Specific Heat Capacity, J/kg-K | 480 | |
| 450 |
| Thermal Conductivity, W/m-K | 12 | |
| 69 |
| Thermal Expansion, µm/m-K | 14 | |
| 13 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 1.7 | |
| 18 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 1.9 | |
| 18 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 30 | |
| 65 |
| Density, g/cm3 | 8.0 | |
| 8.9 |
| Embodied Carbon, kg CO2/kg material | 5.3 | |
| 11 |
| Embodied Energy, MJ/kg | 76 | |
| 150 |
| Embodied Water, L/kg | 200 | |
| 230 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 130 | |
| 150 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 96 | |
| 58 |
| Stiffness to Weight: Axial, points | 14 | |
| 11 |
| Stiffness to Weight: Bending, points | 24 | |
| 21 |
| Strength to Weight: Axial, points | 18 | |
| 15 |
| Strength to Weight: Bending, points | 18 | |
| 15 |
| Thermal Diffusivity, mm2/s | 3.0 | |
| 17 |
| Thermal Shock Resistance, points | 13 | |
| 14 |
Alloy Composition
| Aluminum (Al), % | 0.15 to 0.6 | |
| 0 |
| Carbon (C), % | 0 to 0.1 | |
| 0 to 0.15 |
| Chromium (Cr), % | 19 to 23 | |
| 0 |
| Copper (Cu), % | 0 to 0.75 | |
| 0 to 0.25 |
| Iron (Fe), % | 39.5 to 50.7 | |
| 0 to 0.4 |
| Manganese (Mn), % | 0 to 1.5 | |
| 0 to 0.35 |
| Nickel (Ni), % | 30 to 35 | |
| 99 to 100 |
| Phosphorus (P), % | 0 to 0.045 | |
| 0 |
| Silicon (Si), % | 0 to 1.0 | |
| 0 to 0.35 |
| Sulfur (S), % | 0 to 0.015 | |
| 0 to 0.010 |
| Titanium (Ti), % | 0.15 to 0.6 | |
| 0 |