
Inconel 939 (IN939) is a high-chromium, high-cobalt nickel-based cast superalloy engineered specifically for elevated-temperature service (up to 850°C / 1560°F). It provides exceptional creep rupture strength and hot corrosion resistance in industrial gas turbine blades, vanes, and hot-section castings.
No chemical symbols included; values represent standard nominal weight percentages:
| Element | Nominal Content (%) | Min (%) | Max (%) |
| Nickel | Balance (~48.0) | â | â |
| Chromium | 22.5 | 22.0 | 23.0 |
| Cobalt | 19.0 | 18.0 | 20.0 |
| Titanium | 3.7 | 3.5 | 3.9 |
| Tungsten | 2.0 | 1.8 | 2.2 |
| Aluminum | 1.9 | 1.7 | 2.1 |
| Tantalum | 1.4 | 1.2 | 1.6 |
| Niobium | 1.0 | 0.8 | 1.2 |
| Carbon | 0.15 | 0.13 | 0.17 |
| Zirconium | 0.09 | 0.05 | 0.12 |
| Boron | 0.01 | 0.005 | 0.02 |
Density: 8.15 grams per cubic centimeter
Melting Range: 1310 to 1370 degrees Celsius
Ultimate Tensile Strength: 1100 to 1510 Megapascals
Yield Strength (0.2% Offset): 750 to 1115 Megapascals
Elongation at Break: 10 to 15 percent
Hardness: 38 to 48 Rockwell C
Maximum Service Temperature: 850 degrees Celsius (continuous exposure)
VAC Scrap Grade: Vacuum Induction Melting (VIM) quality scrap. Suitable for direct charge in high-grade superalloy re-melting operations.
Form Factor: Prepared blade solids, cropped turbine roots, and clean solid rounds/turnings. Must be free of coatings (thermal barrier coatings, aluminide coatings), slag, scale, and foreign attachments.
Refining Notes: Contains high levels of reactive elements (titanium and aluminum) along with refractory metals (tungsten, tantalum, and niobium). Requires strict vacuum melt processing to prevent oxidation and inclusions.
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