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Nickel Alloy IN-713C-HIP (Hot isostatic pressed)

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UNS N07713 · also Inconel 713C

Pick for fatigue-critical rotating parts: HIP closes interdendritic microporosity and markedly raises ductility and LCF life.

High cost $$$$

Values for the HIP condition

Other IN-713C tempers and conditions

IN-713C is listed in 4 conditions; see the grade overview at IN-713C.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
FDefault
As fabricated
Standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high.740850834 HRC—
Stress relieved
Choose when residual casting stresses or dendritic segregation must be reduced before machining of thin-wall parts.745860833 HRC1.3 % IACS
Solution treated and aged
Use where a uniform, controlled γ′ size and best creep/rupture consistency are specified rather than the as-cast structure.780900636 HRC1.3 % IACS
HIPThis page
Hot isostatic pressed
Pick for fatigue-critical rotating parts: HIP closes interdendritic microporosity and markedly raises ductility and LCF life.7809101035 HRC1.3 % IACS

What is IN-713C-HIP?

IN-713C-HIP is IN-713C in the HIP condition — pick for fatigue-critical rotating parts: HIP closes interdendritic microporosity and markedly raises ductility and LCF life. IN-713C-HIP has a yield strength of 780 MPa (113 ksi) and a tensile strength of 910 MPa (132 ksi) — stronger than 83% of nickel alloy grades. Elongation at break is 10% and the elastic modulus is 207 GPa (30 Msi). IN-713C-HIP has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,260°C (2,300 °F). F is the default condition FabDigit quotes; HIP is available on request or by drawing note.

Advantages

  • High strength — 780 MPa (113 ksi), better than 83% of nickel alloy grades

Limitations

  • Limited formability — 3/100, worse than 97% of nickel alloy grades
  • Difficult to machine — 8/100, worse than 96% of nickel alloy grades
  • Difficult to weld — 12/100, worse than 90% of nickel alloy grades
  • Limited ductility — 10%, worse than 85% of nickel alloy grades
  • Low fracture toughness — 70 MPa·√m (63.7 ksi·√in), worse than 85% of nickel alloy grades

IN-713C-HIP properties

Typical room-temperature values for IN-713C-HIP; 21 are specific to this condition. Other listed values are IN-713C reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

IN-713C-HIP has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,260°C (2,300 °F).

Density7.91 g/cm³0.29 lb/in³
Melting Point (Solidus)1,260°C2,300 °F
Liquidus Temperature1,345°C2,453 °F

Mechanical14

IN-713C-HIP has a yield strength of 780 MPa (113 ksi) and a tensile strength of 910 MPa (132 ksi) — stronger than 83% of nickel alloy grades. Elongation at break is 10% and the elastic modulus is 207 GPa (30 Msi).

Elastic (Young's) Modulus207 GPa30 Msi
Shear Modulus78 GPa11.3 Msi
Bulk Modulus180 GPa26.1 Msi
Poisson's Ratio0.31
Tensile Strength (Ultimate)910 MPa132 ksi
Yield Strength (0.2% offset)780 MPa113 ksi
Elongation at Break10%
Reduction in Area12%
Shear Strength640 MPa92.8 ksi
Fatigue Strength (Endurance Limit)380 MPa55.1 ksi
Fracture Toughness (K_IC)70 MPa·√m63.7 ksi·√in
Hardness, Brinell340 HB
Hardness, Rockwell C35 HRC
Hardness, Vickers358 HV

Thermal6

IN-713C-HIP is rated for continuous service to 980°C (1,796 °F). It conducts heat at 10.9 W/m·K (6.3 BTU/hr·ft·°F), worse than 64% of nickel alloy grades. Thermal expansion is 10.6 µm/m·K (5.89 µin/in·°F).

Thermal Conductivity10.9 W/m·K6.3 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)10.6 µm/m·K5.9 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)980°C1,796 °F
Min Service Temperature-200°C-328 °F

Electrical3

IN-713C-HIP conducts electricity at 1.3 % IACS, worse than 89% of nickel alloy grades.

Electrical Conductivity1.3 % IACS
Electrical Resistivity1.32×10⁻⁶ Ω·m52 µΩ·in
Magnetic Responsenon-magnetic (paramagnetic γ matrix)

Chemical & Environmental3

Corrosion resistance is good (68/100), worse than 82% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood68/100
Chemical Resistance SummaryExcellent dry-air/exhaust-gas oxidation resistance to ~980 °C; moderate resistance to sulfidation and Na₂SO₄/NaCl hot corrosion because of the relatively low Cr content — coatings (aluminide) used for marine/dirty-fuel duty. Poor in hot oxidizing acids.

Sustainability4

Producing a kilogram of IN-713C-HIP takes about 190 MJ of energy and emits 13.5 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)13.5 kg CO₂/kg
Embodied Water400 L/kg47.9 gal/lb
Typical Recycled Content35%

Manufacturability8

IN-713C-HIP's machinability is not recommended (8/100, worse than 96% of nickel alloy grades); weldability not recommended (12/100); formability not recommended (3/100).

MachinabilityNot recommended8/100
Machinability Rating (AISI 1212 = 100 %)7%
WeldabilityNot recommended12/100
Formability (cold)Not recommended3/100
CastabilityExcellent88/100
Brazeability / SolderabilityFair45/100
PolishabilityGood60/100
Anodizing Responsen/a — not anodizable; use diffusion aluminide or Pt-aluminide/MCrAlY coatings for hot-corrosion protection

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

Working with IN-713C-HIP

Is IN-713C easy to machine?

Very difficult: rigid setups, ceramic or whisker-reinforced/coated carbide tools, low speeds with heavy positive rake and flood coolant; grinding, EDM and ECM are common for blade/wheel features.

Can IN-713C be welded?

Effectively non-weldable by fusion (≈6 % Al + Ti causes strain-age and liquation cracking); repairs use vacuum brazing or specialized low-heat-input laser/EB cladding with pre-/post-heat.

Can IN-713C be formed, bent or molded?

Cast-only alloy — vacuum investment casting with excellent fluidity and low hot-tearing tendency; HIP after casting to close interdendritic porosity for rotating parts.

What surface finishes work on IN-713C?

Grit blast plus chemical/abrasive-flow cleaning; hot-corrosion protection by pack/CVD aluminide or MCrAlY plus optional TBC; not anodizable, electroplating rarely used.

IN-713C 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
Clow-carbon variant IN-713LC: 0.03–0.070.08 – 0.20.12
Cr12 – 1412.5
Mo3.8 – 5.24.2
NbNb+Ta1.8 – 2.82
Alγ′ former5.5 – 6.56
Ti0.5 – 10.8
Zr0.05 – 0.150.1
Bgrain-boundary strengthener0.01 – 0.020.01
Fe≤ 2.5—
Si≤ 0.5—
Mn≤ 0.25—
Coresidual, max≤ 1—
S≤ 0.02—
Ni≈74 %balance—

IN-713C-HIP — frequently asked

What is IN-713C-HIP used for?

IN-713C-HIP is typically used for turbocharger turbine wheels, gas turbine blades and aerospace turbine vanes. In short: best-casting turbine superalloy; turbocharger wheel standard; cast only, non-weldable.

What is the yield strength of IN-713C-HIP?

IN-713C-HIP has a typical yield strength of 780 MPa (113 ksi) and a tensile strength of 910 MPa (132 ksi) — stronger than 83% of nickel alloy grades. Strength varies by condition: see the 4 listed tempers.

Is IN-713C-HIP easy to machine?

Not especially — machinability is rated not recommended (8/100, worse than 96% of nickel alloy grades). Very difficult: rigid setups, ceramic or whisker-reinforced/coated carbide tools, low speeds with heavy positive rake and flood coolant; grinding, EDM and ECM are common for blade/wheel features.

Can IN-713C-HIP be welded?

Not readily — weldability is rated not recommended (12/100). Effectively non-weldable by fusion (≈6 % Al + Ti causes strain-age and liquation cracking); repairs use vacuum brazing or specialized low-heat-input laser/EB cladding with pre-/post-heat.

What surface finishes work on IN-713C-HIP?

Grit blast plus chemical/abrasive-flow cleaning; hot-corrosion protection by pack/CVD aluminide or MCrAlY plus optional TBC; not anodizable, electroplating rarely used.

Can IN-713C-HIP be formed, bent or molded?

Cast-only alloy — vacuum investment casting with excellent fluidity and low hot-tearing tendency; HIP after casting to close interdendritic porosity for rotating parts.

What is the maximum service temperature of IN-713C-HIP?

IN-713C-HIP is rated for continuous use to about 980°C (1,796 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between IN-713C-F and IN-713C-STA?

F is the default condition — standard stock condition for turbocharger wheels and small blades; γ′ forms on cooling so as-cast strength is already high. STA: use where a uniform, controlled γ′ size and best creep/rupture consistency are specified rather than the as-cast structure. Yield strength is 740 MPa in F versus 780 MPa in STA.

Sources

  1. AMS 5391 — Nickel Alloy Castings, Investment, 73Ni-13Cr-4.5Mo-6Al-2Nb (IN-713C) — SAE International (2017)
  2. ASM Handbook Vol.1: Properties and Selection — Superalloys — ASM International (1990)
  3. Superalloys: A Technical Guide, 2nd ed. — ASM International (2002)
  4. ASM Specialty Handbook: Heat-Resistant Materials — ASM International (1997)
  5. Cast nickel superalloy grade data (IN-713C / IN-713LC) for turbocharger and turbine castings — investment casting foundries (2023)

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.