Phone: 1-800-521-0332
Email: CLICK HERE to email us
Chat CLICK HERE to chat live

X-750

Product Information

Alloy X-750 is a nickel chromium alloy similar to Alloy 600 but made precipitation hardenable by additions of aluminum and titanium. It has goodresistance to corrosion and oxidation along with high tensile and creep-rupture properties at temperatures to 1300°F. Its excellent relaxation resistance is useful for high temperature springs and bolts. Used in gas turbines, rocket engines, nuclear reactors, pressure vessels, tooling, and aircraft structures.

Common Trade Names

Inconel X-750

Inventory

X-750 Sheet

Specifications

UNS: N07750 W. Nr./EN: 2.4669 ASTM: B 637 NACE: MR0175 ISO: 15156-3

Chemical Composition, %

  Ni Cr C Mn Cu Si S Fe
MIN 70.00 14.00 -- -- -- -- -- 5.00
MAX -- 17.00 0.08 1.00 0.50 0.50 0.01 9.00

Features

  • Good mechanical properties at high temperatures
  • Good formability
  • Good oxidation resistance

Applications

  • Oil and gas production
  • Gas turbine engines
  • Nuclear engineering

Physical Properties

Density: 0.299 lb/in3
Melting Point: 2540- 2600°F
Poisson's Ratio: 0.30
Electrical Resistivity: 731 Ohm-circ mil/ft

Temperature, °F 68 392 752 800 1000 1112
Coefficient* of Thermal Expansion, in/in°F x 10-6 - 7.1 7.7 9.2 10.1 8.3
Thermal Conductivity
Btu • ft/ft2 • hr • °F
6.8 -- -- -- -- --
Modulus of Elasticity, Dynamic psi x 106 32.1 30.5 28.6 23.9 20.3 26.2

* 70°F to indicated temperature.

Mechanical Properties

Minimum Specified Properties, ASTM A 240

Ultimate Tensile Strength, ksi 120
0.2% Yield Strength, ksi 60
Elongation, % 30
Hardness MAX, Brinell --

Typical Tensile & Impact Properties, Bar ¾ equalized and precipitation treated hot-rolled, 1625°F 24 hours, AC + 1300°F for 20 hours, AC

Temperature,°F 600 800 1000 1100 1200 1350 1500
Ultimate Tensile Strength, ksi 169.0 166.0 163.5 159.0 143.0 107.0 65.4
0.2% Yield Strength, ksi 116.5 114.0 115.0 112.0 110.0 98.3 64.7

Back to Top
Page Description: Rolled Alloys
Keywords: Rolled Alloys, RA330, Alloy