Inconel X-750® is a nickel-chromium alloy that offers high strength and resistance to corrosion and oxidation at temperatures up to 1300ºC. It is available in various mill forms, making it useful for a wide range of applications. Inconel X-750® is commonly used in rocket engine thrust chambers, gas turbine parts, and airframe components.
If you would like more information about our Inconel X750® products, please contact us or request a quote.
INCONEL® alloy X-750 (UNS N07750/W. Nr. 2.4669) is a precipitation-hardenable nickel-chrome alloy with excellent corrosion and oxidation resistance and high strength at temperatures up to 1300°F. Although its precipitation hardening effect decreases above 1300°F, the alloy retains practical strength up to 1800°F. It also exhibits good properties at cryogenic temperatures. The economic benefits and availability of INCONEL® alloy X-750 in all standard mill forms have made it a popular choice for applications in various industries. This alloy is commonly used for rotor blades, wheels, bolts, structural members in gas turbines, as well as rocket engine thrust chambers and hot environment ducting systems in airframes. Other applications include forming tools, heat-treating fixtures, extrusion dies, and test machine grips. INCONEL® alloy X-750 is suitable for spring suspensions and fasteners at temperatures ranging from sub-zero to 1200°F.
Magellan Metals offers nickel alloy Inconel X-750® in a variety of forms, including:
Nickel alloy Inconel X-750® has many different industrial applications, some of which include:
Use the above button to Contact us for more information on Inconel X-750®, call Magellan Metals at (203) 838-5700, or request a quote today.
Chemical Analysis | |
C | .08 max |
MN | 1.00 max |
S | .01 max |
Si | .50 max |
Cr | 14.0 -17.0 |
Ni | 70.0 min |
Cu | 0.50 max |
Co | 1.0 max |
Ti | 2.25-2.75 max |
Al | 0.40- 1.0 |
Fe | 5.0- 9.0 |
NB | 0.70- 1.20 |