Hastelloy X per PDS 15102QFC Nickel Alloy
PDS 15102QFC is a Product Design Specification specification for Hastelloy X Sheet. 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 PDS 15102QFC in the forms required for manufacturing and high-temperature service applications
All material is supplied in the solution-annealed condition, ensuring uniform mechanical strength, fine grain structure, and superior oxidation resistance.
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 PDS 15102QFC?
PDS 15102QFC describes the material, mechanical, and testing requirements to cover Hastelloy X in sheet and plate product forms, particularly for use in aerospace designs and high-temperature applications. The alloy will correlate to rigid requirements for chemical composition, surface finish, and metallurgical consistency, so design engineers can use this alloy in aircraft, turbines, and energy production equipment where reliability is necessary to obtain long-term thermal stability.
By adhering to the specifications of “PDS 15102QFC,” designers assure themselves all materials used are compliant with industry-validated criteria while providing resistance to corrosive attack, achieving required properties at high temperatures, and also
Applications and Industry Uses
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 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.
Certified Material for Critical Service
All Hastelloy X per PDS 15102QFC supplied by Fighter Jet Metals comes with complete test documentation, heat numbers, and traceability in accordance with project or OEM specifications.
We can coordinate dual certification with related standards, including AMS 5536, AMS 5754, and MSRR 7158, to support integrated material programs across aerospace and industrial platforms.