FabDigit

Nickel Alloy Astroloy

UNS N13017

Astroloy is a high-strength Ni-Co-Cr-Mo-Al-Ti superalloy (N13017) with a gamma-prime fraction above 40%, used for critical rotating turbine components.

High cost $$$$

Reference datasheet — Astroloy 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

Astroloy tempers and conditions

Astroloy is supplied in 5 conditions, soft to hard. STA is the default FabDigit quotes; the values on this page are for it.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution treated
Pick when rough machining or hot forming is required before the final ageing cycle; strength is much lower and must be restored by ageing.7201,1002830 HRC—
Powder HIP consolidated, no final ageing
Near-net-shape HIP preforms supplied before final solution/age; used for machining allowance reduction, then heat treated.9501,3002036 HRC1.3 % IACS
investment cast, solution treated and aged
Coarse-grain cast form for static and small rotating parts where creep/stress-rupture at 800–870 °C matters more than ductility or LCF.9651,240738 HRC—
STADefault
Solution treated and aged
Standard wrought/forged disc condition (≈1150 °C solution, 870 °C stabilize, 980 °C + 650 °C/760 °C ageing) for maximum room- and mid-temperature strength.1,0501,4151640 HRC—
powder consolidated (HIP/extruded-forged) and fully heat treated
Choose for turbine discs needing the highest low-cycle-fatigue life and uniform fine-grain properties in large sections.1,1601,5201843 HRC—

What is Astroloy?

Astroloy is a high-strength Ni-Co-Cr-Mo-Al-Ti superalloy (N13017) with a gamma-prime fraction above 40%, used for critical rotating turbine components. It is available as wrought STA, cast-plus-STA, and powder-metallurgy HIP or as-HIP material, with STA values of 1050 MPa yield, 1415 MPa tensile, 16% elongation and 40 HRC at service temperatures to 815 °C. Machinability (12), weldability (10) and formability (8) are all poor, so parts are isothermally forged or HIP-consolidated and then finish-ground. Waspaloy or Haynes 282 are more fabricable where the full strength level is not required. Astroloy has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,250°C (2,282 °F). Astroloy has a yield strength of 1,050 MPa (152 ksi) and a tensile strength of 1,415 MPa (205 ksi) — stronger than 97% of nickel alloy grades. Elongation at break is 16% and the elastic modulus is 213 GPa (30.9 Msi).

What is Astroloy used for?

  • turbine discs
  • high-pressure turbine blades
  • critical rotating hardware

Advantages

  • High strength — 1,050 MPa (152 ksi), better than 97% of nickel alloy grades

Limitations

  • Difficult to weld — 10/100, worse than 94% of nickel alloy grades
  • High embodied carbon — 16 kg CO₂/kg, worse than 93% of nickel alloy grades
  • Needs corrosion protection — 62/100, worse than 87% of nickel alloy grades
  • Limited formability — 8/100, worse than 87% of nickel alloy grades
  • Limited ductility — 16%, worse than 79% of nickel alloy grades

Astroloy properties

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

Physical3

Astroloy has a density of 7.91 g/cm³ (0.286 lb/in³), lighter than 89% of nickel alloy grades. It melts at 1,250°C (2,282 °F).

Density7.91 g/cm³0.29 lb/in³
Melting Point (Solidus)1,250°C2,282 °F
Liquidus Temperature1,340°C2,444 °F

Mechanical16

Astroloy has a yield strength of 1,050 MPa (152 ksi) and a tensile strength of 1,415 MPa (205 ksi) — stronger than 97% of nickel alloy grades. Elongation at break is 16% and the elastic modulus is 213 GPa (30.9 Msi).

Elastic (Young's) Modulus213 GPa30.9 Msi
Shear Modulus82 GPa11.9 Msi
Bulk Modulus178 GPa25.8 Msi
Poisson's Ratio0.3
Tensile Strength (Ultimate)1,415 MPa205 ksi
Yield Strength (0.2% offset)1,050 MPa152 ksi
Elongation at Break16%
Reduction in Area18%
Compressive Strength1,080 MPa157 ksi
Shear Strength880 MPa128 ksi
Fatigue Strength (Endurance Limit)620 MPa89.9 ksi
Fracture Toughness (K_IC)85 MPa·√m77.4 ksi·√in
Charpy V-Notch Impact (RT)25 J18.4 ft·lbf
Hardness, Brinell375 HB
Hardness, Rockwell C40 HRC
Hardness, Vickers400 HV

Thermal6

Astroloy is rated for continuous service to 815°C (1,499 °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 12 µm/m·K (6.67 µin/in·°F).

Thermal Conductivity11 W/m·K6.4 BTU/hr·ft·°F
Specific Heat Capacity420 J/kg·K0.1 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12 µm/m·K6.7 µin/in·°F
Latent Heat of Fusion290 J/g125 BTU/lb
Max Service Temperature (continuous)815°C1,499 °F
Min Service Temperature-200°C-328 °F

Electrical3

Astroloy conducts electricity at 1.3 % IACS, worse than 89% of nickel alloy grades.

Electrical Conductivity1.3 % IACS
Electrical Resistivity1.31×10⁻⁶ Ω·m51.6 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is good (62/100), worse than 87% of nickel alloy grades.

Galvanic Potential (seawater, vs SCE)-0.15 V
Corrosion ResistanceGood62/100
Chemical Resistance SummaryGood oxidation resistance to ~900 °C from Cr₂O₃/Al₂O₃ scale; moderate resistance to sulphidation and Na₂SO₄ hot corrosion (lower Cr than Waspaloy); resists most neutral and reducing media but attacked by hot halides and oxidising acids.

Sustainability4

Producing a kilogram of Astroloy takes about 240 MJ of energy and emits 16 kg of CO₂ — more than 96% of nickel alloy grades. Typical recycled content is 15%.

Embodied Energy (primary production)240 MJ/kg103,182 BTU/lb
Embodied Carbon (primary production)16 kg CO₂/kg
Embodied Water320 L/kg38.3 gal/lb
Typical Recycled Content15%

Manufacturability8

Astroloy's machinability is not recommended (12/100, worse than 86% of nickel alloy grades); weldability not recommended (10/100); formability not recommended (8/100).

MachinabilityNot recommended12/100
Machinability Rating (AISI 1212 = 100 %)8%
WeldabilityNot recommended10/100
Formability (cold)Not recommended8/100
CastabilityFair35/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100
Anodizing Responsen/a — nickel alloy; use passivation, shot peening or diffusion/thermal-barrier coatings instead

Common Calculations5

Specific Strength (UTS / density)calculated179 kN·m/kg
Specific Stiffness (E / density)calculated26.9 MN·m/kg
Modulus of Resiliencecalculated2,588 kJ/m³
Thermal Diffusivitycalculated3.3 mm²/s
Thermal Shock Resistance Indexcalculated6

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. Astroloy 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 scaleAstroloy

Working with Astroloy

Is Astroloy easy to machine?

Very difficult in the aged condition — use rigid setups, low speeds (5–15 m/min carbide, 20–40 m/min ceramic), heavy positive feeds to avoid work-hardened skin, high-pressure coolant; finish grinding and creep-feed grinding are common for slots and fir-trees.

Can Astroloy be welded?

Essentially non-weldable in the fully aged state due to >40% γ′ strain-age cracking; if joining is unavoidable, weld in the solution-treated condition with electron beam or inertia friction welding and re-solution/age immediately.

Can Astroloy be formed, bent or molded?

Hot work only, in a narrow 1050–1150 °C window with tight strain-rate control (isothermal/superplastic forging for P/M billet); cold forming is impractical.

Astroloy 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
C0.04 – 0.10.06
Cr14 – 1615
Co16 – 18.517
Mo4.5 – 5.755.25
Alγ′ former3.5 – 4.54
Tiγ′ former3.35 – 3.853.5
Bgrain-boundary strengthener0.02 – 0.040.03
Zr0 – 0.10.06
Feresidual≤ 10.3
Mn≤ 0.15
Si≤ 0.2
S≤ 0.02
Nibalance

What surface finishes work on Astroloy?

Shot peen critical rotating surfaces for fatigue life; typical finishes are grinding plus passivation, aluminide diffusion or MCrAlY/TBC coatings for hot sections — anodizing does not apply.

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 Astroloy in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
N13017

How much does Astroloy cost?

Astroloy 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.

Astroloy — frequently asked

What is Astroloy used for?

Astroloy is typically used for turbine discs, high-pressure turbine blades and critical rotating hardware. In short: highest-strength disc superalloy; powder-metallurgy HIP route; non-weldable when aged.

What is the yield strength of Astroloy?

Astroloy has a typical yield strength of 1,050 MPa (152 ksi) and a tensile strength of 1,415 MPa (205 ksi) — stronger than 97% of nickel alloy grades. Strength varies by condition: see the 5 listed tempers.

Is Astroloy easy to machine?

Not especially — machinability is rated not recommended (12/100, worse than 86% of nickel alloy grades). Very difficult in the aged condition — use rigid setups, low speeds (5–15 m/min carbide, 20–40 m/min ceramic), heavy positive feeds to avoid work-hardened skin, high-pressure coolant; finish grinding and creep-feed grinding are common for slots and fir-trees.

Can Astroloy be welded?

Not readily — weldability is rated not recommended (10/100). Essentially non-weldable in the fully aged state due to >40% γ′ strain-age cracking; if joining is unavoidable, weld in the solution-treated condition with electron beam or inertia friction welding and re-solution/age immediately.

What surface finishes work on Astroloy?

Shot peen critical rotating surfaces for fatigue life; typical finishes are grinding plus passivation, aluminide diffusion or MCrAlY/TBC coatings for hot sections — anodizing does not apply.

Can Astroloy be formed, bent or molded?

Hot work only, in a narrow 1050–1150 °C window with tight strain-rate control (isothermal/superplastic forging for P/M billet); cold forming is impractical.

What is the maximum service temperature of Astroloy?

Astroloy is rated for continuous use to about 815°C (1,499 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between Astroloy-STA and Astroloy-SOL?

STA is the default condition — standard wrought/forged disc condition (≈1150 °C solution, 870 °C stabilize, 980 °C + 650 °C/760 °C ageing) for maximum room- and mid-temperature strength. SOL: pick when rough machining or hot forming is required before the final ageing cycle; strength is much lower and must be restored by ageing. Yield strength is 1,050 MPa in STA versus 720 MPa in SOL.

How much does Astroloy cost?

Astroloy 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 Specialty Handbook: Heat-Resistant Materials (Superalloys) — ASM International (1997)
  2. Superalloys II — High-Temperature Materials for Aerospace and Industrial Power — Wiley (1987)
  3. AMS 5880 / UNS N13017 nickel alloy bar and forgings — SAE International (2018)
  4. ASM Handbook Vol.16 Machining — Machining of Nickel Alloys — ASM International (1989)

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.