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Nickel Alloy Inconel X-750-HTH

Precip hard

UNS N07750 · EN 2.4669, NiCr15Fe7TiAl

HTH = equalized 885 °C/24 h + aged 704 °C/20 h

Highest room- and mid-temperature strength condition for bolting, bar and forgings used below ~650 °C.

High cost $$$$

Values for the HTH condition

Other Inconel X-750 tempers and conditions

Inconel X-750 is listed in 7 conditions; see the grade overview at Inconel X-750.

Compare all 7 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest, most formable and weldable condition; used as supply state for forming, deep drawing and machining before ageing.35083045180 HB—
Equalized
Intermediate stabilising treatment for bar/forgings that will be single-aged; gives best RT and mid-temperature strength after ageing.4809003518 HRC1.4 % IACS
STADefault
Solution treated and aged
Standard turbine/aerospace condition (AMS 5667 bar): best balance of RT strength, creep-rupture and stress-relaxation resistance to ~700 °C.8151,2002532 HRC—
HTHThis page
Equalized 885 °C/24 h + aged 704 °C/20 h
Highest room- and mid-temperature strength condition for bolting, bar and forgings used below ~650 °C.8601,2752335 HRC—
Hot rolled / hot finished + aged 732 °C/16 h
Economical bar/rod condition for bolts, studs and general high-temperature hardware below ~600 °C.9001,3002236 HRC1.4 % IACS
Spring hard
Cold-worked wire/strip supplied for coiling or forming; must be aged after forming to develop final spring properties.1,1701,380642 HRC1.4 % IACS
Cold drawn + aged 732 °C/16 h
Final condition for high-temperature springs, clips and seals: highest strength and best stress-relaxation resistance to ~540–650 °C.1,2801,550845 HRC1.4 % IACS

What is Inconel X-750-HTH?

Inconel X-750-HTH is Inconel X-750 in the HTH condition — highest room- and mid-temperature strength condition for bolting, bar and forgings used below ~650 °C. Inconel X-750-HTH has a yield strength of 860 MPa (125 ksi) and a tensile strength of 1,275 MPa (185 ksi) — stronger than 91% of nickel alloy grades. Elongation at break is 23% and the elastic modulus is 214 GPa (31 Msi). Inconel X-750-HTH has a density of 8.28 g/cm³ (0.299 lb/in³), lighter than 55% of nickel alloy grades. It melts at 1,393°C (2,539 °F). STA is the default condition FabDigit quotes; HTH is available on request or by drawing note.

Advantages

  • High strength — 860 MPa (125 ksi), better than 91% of nickel alloy grades

Limitations

  • Difficult to weld — 35/100, worse than 76% of nickel alloy grades

Inconel X-750-HTH properties

Typical room-temperature values for Inconel X-750-HTH; 11 are specific to this condition. Other listed values are Inconel X-750 reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

Inconel X-750-HTH has a density of 8.28 g/cm³ (0.299 lb/in³), lighter than 55% of nickel alloy grades. It melts at 1,393°C (2,539 °F).

Density8.28 g/cm³0.3 lb/in³
Melting Point (Solidus)1,393°C2,539 °F
Liquidus Temperature1,427°C2,601 °F

Mechanical16

Inconel X-750-HTH has a yield strength of 860 MPa (125 ksi) and a tensile strength of 1,275 MPa (185 ksi) — stronger than 91% of nickel alloy grades. Elongation at break is 23% and the elastic modulus is 214 GPa (31 Msi).

Elastic (Young's) Modulus214 GPa31 Msi
Shear Modulus83 GPa12 Msi
Bulk Modulus170 GPa24.7 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,275 MPa185 ksi
Yield Strength (0.2% offset)860 MPa125 ksi
Elongation at Break23%
Reduction in Area30%
Compressive Strength850 MPa123 ksi
Shear Strength730 MPa106 ksi
Fatigue Strength (Endurance Limit)500 MPa72.5 ksi
Fracture Toughness (K_IC)100 MPa·√m91 ksi·√in
Charpy V-Notch Impact (RT)42 J31 ft·lbf
Hardness, Brinell330 HB
Hardness, Rockwell C35 HRC
Hardness, Vickers320 HV

Thermal6

Inconel X-750-HTH is rated for continuous service to 650°C (1,202 °F). It conducts heat at 12 W/m·K (6.93 BTU/hr·ft·°F), better than 65% of nickel alloy grades. Thermal expansion is 12.6 µm/m·K (7 µin/in·°F).

Thermal Conductivity12 W/m·K6.9 BTU/hr·ft·°F
Specific Heat Capacity431 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.6 µm/m·K7 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)650°C1,202 °F
Min Service Temperature-253°C-423 °F

Electrical3

Inconel X-750-HTH conducts electricity at 1.4 % IACS, worse than 65% of nickel alloy grades.

Electrical Conductivity1.4 % IACS
Electrical Resistivity1.22×10⁻⁶ Ω·m48 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is very good (80/100), better than 61% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.05 V
Corrosion ResistanceVery good80/100
Chemical Resistance SummaryExcellent oxidation and hot-gas corrosion resistance to ~870 °C; good in steam, seawater and alkalis; susceptible to attack by hot halides/hydrochloric acid and to sulphidation in high-sulphur gas; aged material can be sensitive to intergranular attack in high-temperature caustic and to SCC in some high-temperature water chemistries.

Sustainability4

Producing a kilogram of Inconel X-750-HTH takes about 190 MJ of energy and emits 13 kg of CO₂ — more than 75% of nickel alloy grades. Typical recycled content is 35%.

Embodied Energy (primary production)190 MJ/kg81,685 BTU/lb
Embodied Carbon (primary production)13 kg CO₂/kg
Embodied Water800 L/kg95.9 gal/lb
Typical Recycled Content35%

Manufacturability8

Inconel X-750-HTH's machinability is not recommended (14/100, worse than 81% of nickel alloy grades); weldability fair (35/100); formability poor (30/100).

MachinabilityNot recommended14/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityFair35/100
Formability (cold)Poor30/100
CastabilityPoor30/100
Brazeability / SolderabilityFair50/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy; use passivation, electropolish or thermal oxide instead

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with Inconel X-750-HTH

Is Inconel X-750 easy to machine?

Machine preferably in the annealed state with rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed and flood coolant; aged material work-hardens sharply and needs sharp edges and no dwelling.

Can Inconel X-750 be welded?

GTAW with matching X-750 or Inconel 718/A-type filler; weld in the annealed condition, keep heat input low and re-solution-treat before ageing to avoid strain-age (post-weld heat treatment) cracking.

Can Inconel X-750 be formed, bent or molded?

Cold form only in the annealed or equalized condition — springback is large and forces are ~2× those for stainless; hot work at 1150–950 °C and re-anneal after heavy deformation.

What surface finishes work on Inconel X-750?

Not anodizable; use pickling/passivation, electropolishing, glass-bead or vapour blast, and vacuum heat treatment for bright surfaces; oxide films from ageing must be removed before brazing or plating.

Inconel X-750 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
Cr14 – 1715.5
Fe5 – 97
Tiγ′ former2.25 – 2.752.5
Alγ′ former0.4 – 10.7
NbNb + Ta0.7 – 1.20.95
Co≤ 10.2
Mn≤ 10.3
Si≤ 0.50.2
Cu≤ 0.50.05
C≤ 0.080.04
S≤ 0.010
NiNi + Co, balance≥ 70 (balance)—

Inconel X-750-HTH — frequently asked

What is Inconel X-750-HTH used for?

Inconel X-750-HTH is typically used for gas turbine blades and bolts, springs at elevated temperature, jet engine seals and nuclear reactor springs. In short: hot spring-temper superalloy; γ′ strength to 704 °C; stronger than 600 series nickel.

What is the yield strength of Inconel X-750-HTH?

Inconel X-750-HTH has a typical yield strength of 860 MPa (125 ksi) and a tensile strength of 1,275 MPa (185 ksi) — stronger than 91% of nickel alloy grades. Strength varies by condition: see the 7 listed tempers.

Is Inconel X-750-HTH easy to machine?

Not especially — machinability is rated not recommended (14/100, worse than 81% of nickel alloy grades). Machine preferably in the annealed state with rigid setups, positive-rake carbide or ceramic tooling, low speed / heavy feed and flood coolant; aged material work-hardens sharply and needs sharp edges and no dwelling.

Can Inconel X-750-HTH be welded?

With care — weldability is rated fair (35/100). GTAW with matching X-750 or Inconel 718/A-type filler; weld in the annealed condition, keep heat input low and re-solution-treat before ageing to avoid strain-age (post-weld heat treatment) cracking.

What surface finishes work on Inconel X-750-HTH?

Not anodizable; use pickling/passivation, electropolishing, glass-bead or vapour blast, and vacuum heat treatment for bright surfaces; oxide films from ageing must be removed before brazing or plating.

Can Inconel X-750-HTH be formed, bent or molded?

Cold form only in the annealed or equalized condition — springback is large and forces are ~2× those for stainless; hot work at 1150–950 °C and re-anneal after heavy deformation.

What is the maximum service temperature of Inconel X-750-HTH?

Inconel X-750-HTH is rated for continuous use to about 650°C (1,202 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Inconel X-750-STA and Inconel X-750-ANN?

STA is the default condition — standard turbine/aerospace condition (AMS 5667 bar): best balance of RT strength, creep-rupture and stress-relaxation resistance to ~700 °C. ANN: softest, most formable and weldable condition; used as supply state for forming, deep drawing and machining before ageing. Yield strength is 815 MPa in STA versus 350 MPa in ANN.

Sources

  1. INCONEL alloy X-750 technical bulletin — Special Metals Corporation (2004)
  2. AMS 5542 — Nickel Alloy Sheet, Strip and Plate, Precipitation Heat Treatable — SAE International (2018)
  3. AMS 5667/5668/5670/5671 — Nickel Alloy Bars, Forgings and Rings (N07750) — SAE International (2017)
  4. ASTM B637 — Precipitation-Hardening Nickel Alloy Bars, Forgings and Forging Stock for High-Temperature Service — ASTM International (2018)
  5. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels, and High-Performance Alloys — ASM International (1990)
  6. GB/T 14992 / GH4145 — SAC (2005)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.