NICKEL X-750 per GE B50YP44
The GE B50YP44 standard specifies the requirements for Nickel X-750, a tough nickel chromium alloy known for its strength, as well as its resistance to corrosion and heat. The spec covers bars and forgings used in the manufacture of aircraft parts, with the aim of providing guaranteed mechanical properties, heat resistance, and dimensional accuracy.
The GE B50YP44 specification ensures Nickel X-750 material meets strict aerospace standards, making it suitable for high-stress, high-temperature components in critical aerospace applications.
Product Forms & Size Range
NICKEL X-750 Round Bar diameters range from 0.125″ to 14.00″ diameter.
NICKEL X-750 Flat Bar comes in a variety of thicknesses and widths. For more information please request a quote.
NICKEL X-750 Plate Thickness ranges from 0.1875″ to 6.50″ Thick.
NICKEL X-750 Sheet / Coil Thicknesses range from 0.002″ to .150″ Thick.
Technical Specifications
- Standard: GE B50YP44
- Alloy Type: Nickel-Chromium with Titanium & Aluminum
- Condition: Precipitation-Hardened (Aged)
- Product Forms: Bars & Forgings
- Service Temperature: Up to 1300°F (700°C)
- Applications: Aerospace components · Gas turbines · Rocket engines · Energy systems
This specification guarantees uniform hardness, fatigue resistance, and corrosion resistance, critical for high-demand aerospace engineering.
NICKEL X-750 SPECIFICATIONS
SHEET & PLATE
Sheets and plates for high-temperature aerospace and industrial applications.
BARS & FORGINGS
Bars and forgings designed for high-strength, creep, and fatigue-resistant components.
GE AVIATION
Engine components requiring high-temperature strength and durability.
Certified Material for Critical Service
Fighter Jet Metals supplies INCONEL X-750 with:
- Full AMS and GE specification compliance
- Heat treatment and mechanical testing documentation
- Nadcap-approved processing
- Aerospace-grade traceability