NICKEL X-750 per GE B50A151A
GE B50A151A is the GE Aviation specification for the Nickel X-750 alloy, which is a nickel-chromium alloy that is renowned for its high strength, resistance to corrosion, and ability to withstand high temperatures. This is a specification for the nickel-chromium alloy in plate and sheet forms for use in critical manufacturing applications in the aerospace sector.
Product Forms & Size Range of B50A151A
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.
GE B50A151A Technical Specifications
- Standard: GE B50A151A
- Alloy Type: Nickel-Chromium with Titanium & Aluminum
- Condition: Precipitation-Hardened (Aged)
- Product Forms: Plate & Sheet
- Service Temperature: Up to 1300°F (700°C)
- Applications: Aerospace Components · Gas Turbines · Rocket Engines · Energy Systems
The specification ensures uniform hardness, superior fatigue performance, and excellent corrosion resistance, critical for aerospace and high-performance applications.
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