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Hastelloy X750

Hastelloy X750

Nickel (Ni) - 70.0 (+ Cobalt)
Chromium (Cr) - 15.5 Median
(14.0 Min - 17.0 Max)
Iron (Fe) - 7.0 Median
(5.0 Min - 9.0 Max)
Manganese (Mn) - 1.0 Max
Cobalt (Co) - 1.0 Max
Titanium (Ti) - 2.50 Median
(2.25 Min - 2.75 Max)
Other

Key

Nickel
Copper
Chromium
Aluminum
Molybdenum
Iron
Titanium
Manganese
Cobalt
Other
  • Nickel (Ni) 70.0 (+ Cobalt)
  • Copper (Cu) 0.5 Max
  • Chromium (Cr) 15.5 Median
    (14.0 Min - 17.0 Max)
  • Aluminum Al 0.7 Median
    (0.40 Min - 1.00 Max)
  • Iron (Fe) 7.0 Median
    (5.0 Min - 9.0 Max)
  • Manganese (Mn) 1.0 Max
  • Cobalt (Co) 1.0 Max
  • Carbon (C) 0.08 Max
  • Silicon (Si) 0.5 Max
  • Niobium (Nb) 0.95 (+ Tantalum)
  • Sulfur (S) 0.01 Max
  • Titanium (Ti) 2.50

UNS N07750

If you are seeking fasteners with durable performance under extreme heat and corrosive conditions, Hastelloy® X750 is a trusted solution. At Nickel Systems, we supply premium fasteners made from this high-performance alloy to support the most demanding applications. As a true stocking distributor, we maintain an inventory of hard-to-find UNS N07750 fasteners for immediate shipment. Whether you need bolts, nuts or custom fasteners, we make sourcing exotic alloy fasteners straightforward.

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Summary

  • Environment:
    Oxidation Resistant
  • Temperature Limit:
    1300 °F / 704 °C
  • Ultimate Tensile (Typical):
    160 ksi / 1103 mpa

Hastelloy® X750 Specifications & Technical Data

Hastelloy® X750 possesses unique characteristics that are desirable in numerous industrial applications. If your question isn’t answered below, download the complete technical data sheet here.

Specifications

  • ASTM B637 & ASME SB637
  • Plate, Sheet & Strip: AMS 5542/5598
  • Rod & Bar: AMS 5667
  • W-Nr 2.4669

Physical Constants

Density

0.299 lb/in3
8.28 g/cm3
Melting Range

2540-2600°F
1393-1427°C
Curie Temperature As Hot-Rolled -225°F
Triple-Heat-Treated
(2100°F/2 hr, A.C.,+1500°F /24 hr, A.C., + 1300°F/20 hr, A.C.)
-193°F
Magnetic Permeability (70°F, 200H) As Hot-Rolled 1.0020
Triple-Heat-Treated
(2100°F/2 hr, A.C.,+1500°F /24 hr, A.C., + 1300°F/20 hr, A.C.)
1.0035
Emissivity, Oxidized Surface 600°F 0.895
2000°F 0.925
Linear Contraction during Precipitation Treatment (1300°F/20hr), in/in Hot-Rolled 0.00044
20% Cold-Rolled 0.00052
Annealed 0.00026

 

Thermal Properties
Temperature, °F Mean Linear Expansion, in./in./°F x 10-6 from 70°F to Temperature Shown Thermal Conductivity, Btu/in./hr/sq ft/°F Specific Heat Btu/lb/°F Diffusivity, sq ft/hr Electrical Resistivity, ohm/circ mil/ft
-250 6.5 67 0.073 0.150
-200 6.6 70 0.080 0.143
-100 6.7 74 0.090 0.135
70 83 0.103 0.132 731
200 7.0 89 0.109 0.133 739
400 7.2 98 0.116 0.140 746
600 7.5 109 0.120 0.148 761
800 7.8 120 0.125 0.158 771
1000 8.1 131 0.0.130 0.169 783
1200 8.4 143 0.137 0.173 786
1400 8.8 154 0.151 0.172 775
1600 9.3 164 0.171 0.164 761
1800 9.8

a Material heat-treated 2100°F/3 hr, A.C., + 1550°F/24 hr, A.C., + 1300°F/20 hr, A.C.

Effect of Heat Treatment on Room-Temperature Resistivity of Hot-Rolled Bar
Heat Treatment Resistivity, ohm/circ mil/ft
As hot-rolled 759
2000°F/1 hr, A.C. 763
2100°F/1 hr, A.C.+1500°F/24 hr, A.C.+ 1300°F/20 hr, A.C. 724
1800°F/1 hr, A.C.+1350°F/8 hr,F.C. to 1150°F, hold at 1150°F for total time of 18 hr, A.C. 739

 

Modulus of Elasticity
Temperature, °F Modulus of Elasticity, 103 ksi
Tension Torsion
Static Dynamic Static
80 31.0 31.0 11.0
500 28.7 29.1 10.2
1000 25.0 26.7 9.0
1200 23.0 25.5 8.1
1350 21.0 24.4
1500 18.5 23.2
1600 22.1
1800 20.0

aPoisson’s ratio = 0.29

Mechanical Properties

Minimum Specified Properties
Ultimate Tensile Strength, ksi 120
.02% Yield Strength, ksi 60
Elongation, % 30

 

Typical Mechanical Properties – Bar
Size  Ultimate
Tensile Strength ksi
Yield Strength (0.2% Offset) Ksi Elongation in 4D(%) % Reduction of Area
Under 4.0″ 165.0 105 20 25
4.0 ” and over 160 100 15 17

 

Room-Temperature Hardness, Rc, of Hot-Rolled Rod
Diameter, in. Solution Treated (1800°F/1 hr, A.C.) Solution Treated & Precipitation Treated (1800°F/1 hr, A.C., + 1400°F/1 hr, F.C. to 1150°F, A.C., Hold for Total Pecipitation-Treating Time of 6 hr, A.C.)
0.875 21 / 26 36 /37
1.250 31 / 27 38 / 36
1.937 25 / 30 36 / 36

 

High-Temperature Properties of Hot-Rolled SolutionTreated (1800°F/1 hr) 1-in. Round
Temperature, °F Ultimate
Tensile Strength, ksi
Yield Strength (0.2% Offset), Ksi Elongation in 2″ (%) % Reduction of Area
85 174.0 115.0 27.5 41.0
400 168.0 113.2 29.0 40.0
600 160.5 107.5 30.0 37.0
800 159.0 106.5 31.0 42.0

Heat Treatment

AMS 5541 1300°F/20 hr., AC (Constant-temperature precipitation treatment).
AMS 5598 1350°F/8 hr., FC to 1150°F, Hold at 1150°F for total precipitation-treating time of 18 hr., AC (Furnace-cool precipitation treatment).

 

Effect of Heat Treatment on Hardness of Hot-Finished Products
Condition Hardness
BHN Rockwell
As-Rolled or As-Forged 228-298 20C-32C
Hot-Worked+1300°F/24 hr, A.C. 313-400 34C-44C
2100°F/2 hr, A.C. 140-277 77B-29C
2100°F/2 hr+1550°F/24 hr, A.C. 200-277 13C-29C
2100°F/2 hr+1550°F/24 hr, A.C.+ 1300°F/20 hr, A.C. 262-340 26C-37C
1625°F/24 hr, A.C. 200-298 13C-32C
1625°F/24 hr, A.C.+1300°F/20 hr, A.C. 302-363 32C-40C
1800°F/1 hr, A.C.+1350°F/8 hr, F.C. to 1150°F, Hold at 1150°F for Total Time of 18 hr, A.C. 32C-42C

 

Effect of precipitation-hardening conditions on hardness of solution-treated (2100°F) material.

x750 Effect of precipitation-hardening conditions on hardness of solution-treated (2100°F) material.

Overview of Hastelloy® X750

Hastelloy® X750 is a precipitation-hardenable nickel-chromium alloy engineered for high-temperature strength, corrosion resistance and long-term thermal stability.

What Is Hastelloy® X750?

Hastelloy® X750 is a nickel-chromium alloy strengthened with additions of titanium and aluminum. This formulation gives it excellent creep resistance, tensile strength and oxidation resistance, even in environments reaching 1300 degrees Fahrenheit. Although much of the effect of precipitation hardening is lost with increasing temperature, it provides useful mechanical properties in temperatures as high as 1800 degrees Fahrenheit. Its resilience and stability make it ideal for structural components subjected to mechanical stress, high-pressure systems or corrosive processing conditions. Hastelloy X750 also has excellent properties down to cryogenic temperatures.

Hastelloy® X750 Composition

The following are Hastelloy® X750’s chemical constituents as per ASTM standards:

  • Nickel (Ni): 70.00% minimum
  • Chromium (Cr): 14.00%–17.00%
  • Iron (Fe): 5.00%–9.00%
  • Titanium (Ti): 2.25%–2.75%
  • Aluminum (Al): 0.40%–1.00%
  • Niobium and Tantalum (Nb + Ta): 0.70%–1.20%
  • Manganese (Mn): < 1.00%
  • Cobalt (Co): < 1.00%
  • Silicon (Si): < 0.50%
  • Copper (Cu): < 0.50%
  • Carbon (C): < 0.08%
  • Sulfur (S): < 0.01

This composition follows ASTM B637 material specifications for alloy UNS N07750. Some trademarked alloy compositions may vary slightly within the UNS number range. If you require alternate chemistry or proprietary variants, please include those details when requesting a quote.

Other Names for Hastelloy® X750

This material may also appear under the following names:

  • Alloy X750
  • UNS N07750
  • W. Nr. 2.4669
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Hastelloy® X750 Applications

Hastelloy® X750 is an ideal choice for demanding applications in several industries, thanks to its exceptional strength, oxidation-corrosion resistance and thermal stability:

  • Aerospace industry: Turbine blades, airframes, thrust reversers and hot air duct systems requiring thermal stability and structural strength.
  • Rocket engines: Thrust chambers and exhaust nozzles handling extreme temperatures and pressures.
  • Gas turbines: Rotor blades and combustion system components that face prolonged high-temperature exposure.
  • Pressure vessels: Pressure-retaining equipment in chemical processing and power generation, due to its strength and creep resistance.
  • Marine: Fasteners and structural parts exposed to saltwater and stress.
  • Automotive: High-stress exhaust and turbo components requiring resistance to thermal fatigue.
  • Others: Other applications include heat-treating fixtures, forming tools, extrusion dies and test machine grips.

Fasteners and springs made from Hastelloy® X750 perform reliably from cryogenic conditions up to 1200 degrees Fahrenheit.

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Request a Quote for Top-Tier Hastelloy® X750 Fasteners Today

Nickel Systems is your dependable partner in sourcing high-performance fasteners made from Hastelloy® X750. We provide fast turnaround, deep inventory and expert-level knowledge across critical industries. We handle every quote request with personalized attention, and our team is ready to discuss your exact needs and product availability. Contact us today for a free quote.

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