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Nickel Alloy Inconel 752

UNS N07752

Inconel 752 (UNS N07752; also supplied against N07750) is an age-hardenable Ni-Cr-Fe superalloy related to X-750/751 with an adjusted Al/Ti ratio for higher elevated-temperature strength in turbine and valve service.

High cost $$$$

Reference datasheet — Inconel 752 is not in the instant-quote catalog. Upload your part and an engineer will quote it in this grade or suggest the closest stocked equivalent.

Values for the STA condition

Inconel 752 tempers and conditions

Inconel 752 is supplied in 6 conditions, soft to hard. STA is the default FabDigit quotes; the values on this page are for it.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition — pick it for forming, deep drawing, machining or welding before final ageing.38084042190 HB—
Equalized 885 °C/24 h + aged 704 °C/20 h
Classic exhaust-valve / valve-seat treatment: best combination of hot hardness, relaxation resistance and ductility for 650–815 °C service.7301,1202533 HRC1.4 % IACS
Hot rolled/forged then aged 704 °C/20 h
Economical aged bar/forging condition when full solution treatment is not required and moderate strength suffices.7601,1402034 HRC1.4 % IACS
STADefault
Solution treated and aged
Standard high-strength condition for turbine bolting, discs and heavily loaded parts up to ~870 °C.8201,2102236 HRC—
Cold drawn then aged 704 °C/20 h
Cold-drawn bar/wire with ageing for maximum room-temperature strength in fasteners and small machined parts.1,0001,3101539 HRC1.4 % IACS
Spring hard
Wire/strip condition for high-temperature springs and diaphragms where relaxation resistance to ~650 °C is needed.1,1701,450843 HRC1.4 % IACS

What is Inconel 752?

Inconel 752 (UNS N07752; also supplied against N07750) is an age-hardenable Ni-Cr-Fe superalloy related to X-750/751 with an adjusted Al/Ti ratio for higher elevated-temperature strength in turbine and valve service. It is used for hot valve and turbine hardware and is available as bar, wire, forgings and strip in annealed, equalised-and-aged, hot-rolled, cold-drawn and spring conditions; aged material runs about 820 MPa yield, 1210 MPa tensile, 22 % elongation and 36 HRC, with a maximum service temperature of 870 °C. Machinability 15, formability 25 and weldability 30 make it demanding to process, and it must be welded and formed annealed then re-aged. X-750 is the more widely stocked alternative. Inconel 752 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). Inconel 752 has a yield strength of 820 MPa (119 ksi) and a tensile strength of 1,210 MPa (175 ksi) — stronger than 87% of nickel alloy grades. Elongation at break is 22% and the elastic modulus is 214 GPa (31 Msi).

What is Inconel 752 used for?

  • turbine blades
  • exhaust valves
  • high-temperature springs
  • aerospace fasteners

Advantages

  • High strength — 820 MPa (119 ksi), better than 87% of nickel alloy grades

Limitations

  • Difficult to weld — 30/100, worse than 78% of nickel alloy grades

Inconel 752 properties

Typical room-temperature values for Inconel 752-STA; bars are the position among nickel alloy grades.

Physical3

Inconel 752 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

Mechanical15

Inconel 752 has a yield strength of 820 MPa (119 ksi) and a tensile strength of 1,210 MPa (175 ksi) — stronger than 87% of nickel alloy grades. Elongation at break is 22% and the elastic modulus is 214 GPa (31 Msi).

Elastic (Young's) Modulus214 GPa31 Msi
Shear Modulus82 GPa11.9 Msi
Bulk Modulus175 GPa25.4 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)1,210 MPa175 ksi
Yield Strength (0.2% offset)820 MPa119 ksi
Elongation at Break22%
Reduction in Area28%
Shear Strength730 MPa106 ksi
Fatigue Strength (Endurance Limit)450 MPa65.3 ksi
Fracture Toughness (K_IC)100 MPa·√m91 ksi·√in
Charpy V-Notch Impact (RT)40 J29.5 ft·lbf
Hardness, Brinell340 HB
Hardness, Rockwell C36 HRC
Hardness, Vickers355 HV

Thermal6

Inconel 752 is rated for continuous service to 870°C (1,598 °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 Fusion285 J/g123 BTU/lb
Max Service Temperature (continuous)870°C1,598 °F
Min Service Temperature-196°C-321 °F

Electrical3

Inconel 752 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 (70/100), worse than 77% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.1 V
Corrosion ResistanceVery good70/100
Chemical Resistance SummaryGood oxidation and hot-gas corrosion resistance to ~870 °C; resists mild aqueous and steam environments and caustics. Limited in strongly oxidising acids, hot concentrated HCl/H2SO4, sulphur-bearing hot gases and molten-salt/lead attack; susceptible to strain-age cracking if welded in the aged state.

Sustainability4

Producing a kilogram of Inconel 752 takes about 145 MJ of energy and emits 11.5 kg of CO₂ — less than 77% of nickel alloy grades. Typical recycled content is 40%.

Embodied Energy (primary production)145 MJ/kg62,339 BTU/lb
Embodied Carbon (primary production)11.5 kg CO₂/kg
Embodied Water160 L/kg19.2 gal/lb
Typical Recycled Content40%

Manufacturability8

Inconel 752's machinability is poor (15/100, worse than 76% of nickel alloy grades); weldability poor (30/100); formability poor (25/100).

MachinabilityPoor15/100
Machinability Rating (AISI 1212 = 100 %)12%
WeldabilityPoor30/100
Formability (cold)Poor25/100
CastabilityPoor30/100
Brazeability / SolderabilityFair45/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy, not anodizable; use electropolish, passivation or Ni/Cr plating if a finish is needed

Common Calculations5

Specific Strength (UTS / density)calculated146 kN·m/kg
Specific Stiffness (E / density)calculated25.8 MN·m/kg
Modulus of Resiliencecalculated1,571 kJ/m³
Thermal Diffusivitycalculated3.4 mm²/s
Thermal Shock Resistance Indexcalculated5

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Strength versus weight in the nickel alloy family

Yield strength against density for every nickel alloy grade FabDigit runs. Inconel 752 is highlighted; hover a dot for its name, or open the interactive family chart.

2005001,0006.577.588.59Density (g/cm³)Yield strength (MPa) — log scaleInconel 752

Working with Inconel 752

Is Inconel 752 easy to machine?

Machine in the annealed condition where possible; aged material needs rigid setups, positive-rake carbide or ceramic, 15–30 m/min, heavy flood coolant and constant feed to avoid work hardening.

Can Inconel 752 be welded?

GTAW with Inconel 718/A-286 or matching filler on solution-annealed base metal only; re-solution and re-age after welding to avoid strain-age cracking, and keep heat input low.

Can Inconel 752 be formed, bent or molded?

Cold form only in the annealed state with high forming loads and frequent intermediate anneals; hot work at 1010–1175 °C and finish above 950 °C.

Inconel 752 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
Tireduced vs X-750 to raise Al/Ti ratio; low confidence1.4 – 2.21.8
Alraised vs X-750/751 for γ′ stability; low confidence1.6 – 2.62.1
NbNb+Ta0.7 – 1.20.9
Mn≤ 10.3
Si≤ 0.50.2
C≤ 0.080.04
Cu≤ 0.50.05
Co≤ 10.3
S≤ 0.010
Niplus cobalt, balance≥ 70 (balance)

What surface finishes work on Inconel 752?

Not anodizable — pickle/grit blast to remove tenacious oxide, then electropolish, passivate or apply aluminide/Cr plating for hot-gas or wear surfaces.

Surface treatments FabDigit runs on nickel alloy parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Nickel Alloy Inconel 752 in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
N07752
Similar grades
N07750

How much does Inconel 752 cost?

Inconel 752 is a high-cost nickel alloy ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Inconel 752 — frequently asked

What is Inconel 752 used for?

Inconel 752 is typically used for turbine blades, exhaust valves, high-temperature springs and aerospace fasteners. In short: exhaust valve superalloy; hotter X-750 variant; 870 °C service capability.

What is the yield strength of Inconel 752?

Inconel 752 has a typical yield strength of 820 MPa (119 ksi) and a tensile strength of 1,210 MPa (175 ksi) — stronger than 87% of nickel alloy grades. Strength varies by condition: see the 6 listed tempers.

Is Inconel 752 easy to machine?

Not especially — machinability is rated poor (15/100, worse than 76% of nickel alloy grades). Machine in the annealed condition where possible; aged material needs rigid setups, positive-rake carbide or ceramic, 15–30 m/min, heavy flood coolant and constant feed to avoid work hardening.

Can Inconel 752 be welded?

Not readily — weldability is rated poor (30/100). GTAW with Inconel 718/A-286 or matching filler on solution-annealed base metal only; re-solution and re-age after welding to avoid strain-age cracking, and keep heat input low.

What surface finishes work on Inconel 752?

Not anodizable — pickle/grit blast to remove tenacious oxide, then electropolish, passivate or apply aluminide/Cr plating for hot-gas or wear surfaces.

Can Inconel 752 be formed, bent or molded?

Cold form only in the annealed state with high forming loads and frequent intermediate anneals; hot work at 1010–1175 °C and finish above 950 °C.

What is the maximum service temperature of Inconel 752?

Inconel 752 is rated for continuous use to about 870°C (1,598 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Inconel 752-STA and Inconel 752-ANN?

STA is the default condition — standard high-strength condition for turbine bolting, discs and heavily loaded parts up to ~870 °C. ANN: softest condition — pick it for forming, deep drawing, machining or welding before final ageing. Yield strength is 820 MPa in STA versus 380 MPa in ANN.

How much does Inconel 752 cost?

Inconel 752 is a high-cost nickel alloy ($$$$), pricier than about 78% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Sources

  1. ASM Handbook Vol.2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials (Ni-Cr-Fe age-hardenable alloys) — ASM International (1990)
  2. ASTM B637 — Precipitation-Hardening Nickel Alloy Bars, Forgings and Forging Stock for High-Temperature Service — ASTM (2018)
  3. UNS N07752 / N07750 alloy designations, Metals & Alloys in the Unified Numbering System — SAE/ASTM (2017)
  4. INCONEL alloy X-750 and alloy 751 technical bulletins (property analogues) — Special Metals Corporation (2004)
  5. ASM Handbook Vol.6 — Welding, Brazing and Soldering (Ni-base precipitation-hardened alloys) — ASM International (1993)

Property data is compiled from published supplier and standards handbooks and normalised for comparison; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.