Hastelloy X per GE B50TF24 Nickel Alloy
GE B50TF24 is a GE Aviation Specification for Hastelloy X.
HASTELLOY X (UNS N06002) is a nickel-chromium-iron-molybdenum alloy that possesses an exceptional combination of oxidation resistance, fabricability and high-temperature strength. It has also been found to be exceptionally resistant to stresscorrosion cracking in petrochemical applications. X alloy exhibits good ductility after prolonged exposure at temperatures of 1200, 1400, 1600°F (650, 760 and 870°C) for 16,000 hours
Product Forms & Size Range
Fighter Jet Metals supplies Hastelloy X per GE B50TF24 in multiple forms for aerospace and industrial applications
All products are produced under strict GE B50TF24 quality standards, ensuring full traceability and performance compliance.
HASTELLOY X Round Bar diameters range from 0.125″ to 14.00″ diameter.
Hastelloy X Flat Bar comes in a variety of thicknesses and widths. For more information please request a quote.
HASTELLOY X Plate Thickness ranges from 0.1875″ to 6.50″ Thick.
HASTELLOY X Sheet Thicknesses range from 0.002″ to .150″ Thick.
What is GE B50TF24 ?
GE B50TF24 is a GE Aviation specification for Hastelloy X (UNS N06002) covering bar, flat bar, plate, and sheet forms used in aerospace and high-temperature industrial applications. This nickel-chromium-iron-molybdenum alloy combines outstanding oxidation resistance, fabricability, and high-temperature strength, making it ideal for jet engine and turbine components exposed to extreme thermal and corrosive environments.
Applications of Hastelloy X per GE B50TF24
Hastelloy X can be used in the construction of heat exchangers for power plants and other energy production facilities. Its good corrosion resistance makes it well-suited for use in environments where heat exchangers are exposed to corrosive gases or liquids.
Hastelloy X can also be used in the construction of boiler components, such as tubes and headers, that are exposed to high temperatures and corrosive environments.
The high temperature strength of Hastelloy X makes it well-suited for use in the construction of turbine blades for gas turbine engines.
Hastelloy X can be used in the construction of fuel cells, which are devices that convert chemical energy into electricity. Its corrosion resistance makes it well-suited for use in fuel cells that are exposed to corrosive gases.
Hastelloy X per GE B50TF24 can be used in the construction of jet engine components, such as blades and vanes, that are exposed to high temperatures and corrosive environments.
Specifications
SHEET & PLATE
Covers Hastelloy X per AMS 5536, defining requirements for sheet, coil, and plate forms used in high-temperature aerospace and industrial components.
BARS & FORGINGS
Specifies Hastelloy X per AMS 5754, governing bars, forgings, and rings for critical service in gas turbines and heat-resistant applications.
GE AVIATION
Outlines GE’s internal standards for nickel-base alloys used in combustion zones, turbine assemblies, and exhaust components.
SNECMA / SAFRAN
Defines Safran’s material specifications for nickel alloys used in aircraft engines and high-temperature structural parts.
ROLLS ROYCE
Establishes requirements for Hastelloy X alloys utilized in Rolls-Royce aerospace and power generation systems.
OTHER SPECS
Includes additional proprietary and industrial standards covering corrosion- and heat-resistant nickel alloys for specialized applications.
Certified Material for Critical Service
All Hastelloy X per GE B50TF24 supplied by Fighter Jet Metals comes with full test reports, heat numbers, and traceability to the specification. Additional project or OEM requirements can be accommodated on request.
Dual certification with related standards such as AMS 5754 and AMS 5536 is also available, allowing integration of GE B50TF24 material into broader nickel-alloy or stainless-steel packages for complex aerospace or industrial projects.