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Nickel Alloy K403-HIP (Hot isostatic pressed)

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Choose for high-reliability rotating blades: hot isostatic pressing at ~1200 °C / 120–150 MPa / 4 h closes casting microporosity, raising elongation to 7.5 % and both fatigue and creep life.

High cost $$$$

Values for the HIP condition

Other K403 tempers and conditions

K403 is listed in 4 conditions; see the grade overview at K403.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
FDefault
As fabricated
Pick as the default delivery state for vacuum investment cast turbine blades and nozzle guide vanes used straight from the mould, accepting 5 % elongation and very poor machinability (score 12).830940538 HRC1.3 % IACS
Solution treated 1210 °C / 4 h, air cool
Use when dendritic segregation must be homogenised and γ′ size adjusted by solution treatment at 1210 °C / 4 h and air cool, lifting elongation to 6 % and giving more consistent creep and ductility.840960639 HRC1.3 % IACS
HIPThis page
Hot isostatic pressed
Choose for high-reliability rotating blades: hot isostatic pressing at ~1200 °C / 120–150 MPa / 4 h closes casting microporosity, raising elongation to 7.5 % and both fatigue and creep life.8509857.539 HRC1.3 % IACS
Hot isostatic pressed, solution treated and aged
Specify for critical long-life hot-section parts; densification followed by solution treatment and ageing refines γ′ morphology for the best overall balance of 1000 MPa tensile and 8 % elongation.8651,000840 HRC1.3 % IACS

What is K403-HIP?

K403-HIP is K403 in the HIP condition — choose for high-reliability rotating blades: hot isostatic pressing at ~1200 °C / 120–150 MPa / 4 h closes casting microporosity, raising elongation to 7.5 % and both fatigue and creep life. K403-HIP has a yield strength of 850 MPa (123 ksi) and a tensile strength of 985 MPa (143 ksi) — stronger than 89% of nickel alloy grades. Elongation at break is 7.5% and the elastic modulus is 202 GPa (29.3 Msi). K403-HIP has a density of 8.2 g/cm³ (0.296 lb/in³), lighter than 63% of nickel alloy grades. It melts at 1,290°C (2,354 °F). F is the default condition FabDigit quotes; HIP is available on request or by drawing note.

Advantages

  • High strength — 850 MPa (123 ksi), better than 89% of nickel alloy grades

Limitations

  • Limited formability — 4/100, worse than 93% of nickel alloy grades
  • Difficult to weld — 12/100, worse than 90% of nickel alloy grades
  • Limited ductility — 7.5%, worse than 87% of nickel alloy grades
  • Low fracture toughness — 68 MPa·√m (61.9 ksi·√in), worse than 86% of nickel alloy grades
  • Hard to polish — 60/100, worse than 84% of nickel alloy grades

K403-HIP properties

Typical room-temperature values for K403-HIP; 22 are specific to this condition. Other listed values are K403 reference data and may not represent this condition. Bars are the position among nickel alloy grades.

Physical3

K403-HIP has a density of 8.2 g/cm³ (0.296 lb/in³), lighter than 63% of nickel alloy grades. It melts at 1,290°C (2,354 °F).

Density8.2 g/cm³0.3 lb/in³
Melting Point (Solidus)1,290°C2,354 °F
Liquidus Temperature1,350°C2,462 °F

Mechanical16

K403-HIP has a yield strength of 850 MPa (123 ksi) and a tensile strength of 985 MPa (143 ksi) — stronger than 89% of nickel alloy grades. Elongation at break is 7.5% and the elastic modulus is 202 GPa (29.3 Msi).

Elastic (Young's) Modulus202 GPa29.3 Msi
Shear Modulus77 GPa11.2 Msi
Bulk Modulus167 GPa24.2 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)985 MPa143 ksi
Yield Strength (0.2% offset)850 MPa123 ksi
Elongation at Break7.5%
Reduction in Area10%
Compressive Strength1,350 MPa196 ksi
Shear Strength650 MPa94.3 ksi
Fatigue Strength (Endurance Limit)350 MPa50.8 ksi
Fracture Toughness (K_IC)68 MPa·√m61.9 ksi·√in
Charpy V-Notch Impact (RT)14 J10.3 ft·lbf
Hardness, Brinell360 HB
Hardness, Rockwell C39 HRC
Hardness, Vickers385 HV

Thermal6

K403-HIP is rated for continuous service to 950°C (1,742 °F). It conducts heat at 11 W/m·K (6.36 BTU/hr·ft·°F), worse than 60% of nickel alloy grades. Thermal expansion is 11.6 µm/m·K (6.44 µin/in·°F).

Thermal Conductivity11 W/m·K6.4 BTU/hr·ft·°F
Specific Heat Capacity440 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.6 µm/m·K6.4 µin/in·°F
Latent Heat of Fusion285 J/g123 BTU/lb
Max Service Temperature (continuous)950°C1,742 °F
Min Service Temperature-196°C-321 °F

Electrical3

K403-HIP conducts electricity at 1.3 % IACS, worse than 89% of nickel alloy grades.

Electrical Conductivity1.3 % IACS
Electrical Resistivity1.3×10⁻⁶ Ω·m51.2 µΩ·in
Magnetic Responseweakly magnetic

Chemical & Environmental3

Corrosion resistance is very good (72/100), worse than 71% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceVery good72/100
Chemical Resistance Summary—

Sustainability4

Producing a kilogram of K403-HIP takes about 230 MJ of energy and emits 14.5 kg of CO₂ — more than 91% of nickel alloy grades. Typical recycled content is 25%.

Embodied Energy (primary production)230 MJ/kg98,882 BTU/lb
Embodied Carbon (primary production)14.5 kg CO₂/kg
Embodied Water300 L/kg35.9 gal/lb
Typical Recycled Content25%

Manufacturability8

K403-HIP's machinability is not recommended (12/100, worse than 86% of nickel alloy grades); weldability not recommended (12/100); formability not recommended (4/100).

MachinabilityNot recommended12/100
Machinability Rating (AISI 1212 = 100 %)8%
WeldabilityNot recommended12/100
Formability (cold)Not recommended4/100
CastabilityVery good70/100
Brazeability / SolderabilityFair45/100
PolishabilityGood60/100
Anodizing Response—

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

Working with K403-HIP

Is K403 easy to machine?

Extremely difficult to cut: airfoil surfaces are produced near net shape by precision casting, and fir-tree roots by creep-feed grinding, EDM or ECM. For turning and milling use solid carbide or ceramic tooling at low speed with heavy feed and ample high-pressure coolant.

Can K403 be welded?

Poor fusion weldability, as Al+Ti above 8% promotes strain-age cracking. Repair is limited to preheated vacuum brazing or laser/micro-plasma cladding followed immediately by heat treatment, and must be qualified under the applicable airworthiness repair procedure.

Can K403 be formed, bent or molded?

Vacuum induction melted master alloy is vacuum investment cast in ceramic shells with controlled pouring and cooling rates to suppress shrinkage porosity; HIP is applied for densification when required. The alloy cannot be forged or cold formed.

What surface finishes work on K403?

The normal route is HIP, grit blasting or chemical cleaning, then fluorescent penetrant and X-ray inspection, followed by aluminide or MCrAlY coating. Film-cooling holes are produced by EDM or laser drilling.

K403 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
C0.11 – 0.180.15
Cr10 – 1211
Co4.5 – 65.2
W4.8 – 5.55.1
Mo3.8 – 4.54.1
Algamma-prime forming element5.3 – 5.95.6
Tigamma-prime forming element2.3 – 2.92.6
Bgrain boundary strengthening0.01 – 0.020.02
Zr≤ 0.060.03
Cetrace rare earth, melt purification≤ 0.02—
Feimpurity≤ 2—
Mnimpurity≤ 0.4—
Siimpurity≤ 0.4—
Pimpurity≤ 0.02—
Simpurity≤ 0.01—
Nibalance—

K403-HIP — frequently asked

What is K403-HIP used for?

K403-HIP is typically used for turbine blades, guide vanes and industrial gas turbine hot parts. In short: equiaxed 950 °C blade alloy; cast near-net airfoils; very low machinability.

What is the yield strength of K403-HIP?

K403-HIP has a typical yield strength of 850 MPa (123 ksi) and a tensile strength of 985 MPa (143 ksi) — stronger than 89% of nickel alloy grades. Strength varies by condition: see the 4 listed tempers.

Is K403-HIP easy to machine?

Not especially — machinability is rated not recommended (12/100, worse than 86% of nickel alloy grades). Extremely difficult to cut: airfoil surfaces are produced near net shape by precision casting, and fir-tree roots by creep-feed grinding, EDM or ECM. For turning and milling use solid carbide or ceramic tooling at low speed with heavy feed and ample high-pressure coolant.

Can K403-HIP be welded?

Not readily — weldability is rated not recommended (12/100). Poor fusion weldability, as Al+Ti above 8% promotes strain-age cracking. Repair is limited to preheated vacuum brazing or laser/micro-plasma cladding followed immediately by heat treatment, and must be qualified under the applicable airworthiness repair procedure.

What surface finishes work on K403-HIP?

The normal route is HIP, grit blasting or chemical cleaning, then fluorescent penetrant and X-ray inspection, followed by aluminide or MCrAlY coating. Film-cooling holes are produced by EDM or laser drilling.

Can K403-HIP be formed, bent or molded?

Vacuum induction melted master alloy is vacuum investment cast in ceramic shells with controlled pouring and cooling rates to suppress shrinkage porosity; HIP is applied for densification when required. The alloy cannot be forged or cold formed.

What is the maximum service temperature of K403-HIP?

K403-HIP is rated for continuous use to about 950°C (1,742 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between K403-F and K403-HIP?

F is the default condition — pick as the default delivery state for vacuum investment cast turbine blades and nozzle guide vanes used straight from the mould, accepting 5 % elongation and very poor machinability (score 12). HIP: choose for high-reliability rotating blades: hot isostatic pressing at ~1200 °C / 120–150 MPa / 4 h closes casting microporosity, raising elongation to 7.5 % and both fatigue and creep life. Yield strength is 830 MPa in F versus 850 MPa in HIP.

Sources

  1. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels, and High-Performance Alloys (cast Ni superalloys) — ASM International (1990)
  2. Superalloys II (C.T. Sims et al.) — Wiley (1987)

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.