Hastelloy X UNS N06002 is a high-temperature nickel-chromium-iron-molybdenum alloy that is commonly used in the aerospace industry. This material exhibits excellent high-temperature strength, oxidation resistance, and fabricability, making it an ideal choice for aircraft engine components, furnace components, and other high-temperature applications.
Hastelloy X Chemical Composition
Hastelloy X alloy consists of approximately 47% nickel, 22% chromium, 18.5% iron, 9% molybdenum, and 1.5% silicon. It also contains small amounts of manganese, phosphorus, sulfur, and carbon.
UNS N06002 Properties
UNS N06002 material has a density of 8.22 g/cm3 and a melting point of 1280-1350℃. It has a high-temperature strength of up to 870℃ and excellent oxidation resistance in temperatures up to 982℃. This material also has good fabricability and weldability.
UNS N06002 Applications
Hastelloy X material is commonly used in high-temperature applications where strength and resistance to oxidation are critical. Some of the applications where this material is used include:
- Aircraft engine components such as combustors, afterburners, and tailpipes
- Industrial furnace components such as muffles, retorts, and trays
- Gas turbine components such as combustors, transition ducts, and nozzle diaphragms
- Heat exchangers and chemical reactors
- Nuclear reactor components
