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Laser Powder Bed Fusion (L-PBF) · Hastelloy X (UNS N06002)

L-PBF Hastelloy X

Solid-solution-strengthened nickel for gas-path components above 700 °C. The workhorse for printed combustor and aft-turbine hardware.

Allowables
UTS760 – 900MPa
Yield380 – 480MPa
Elongation25 – 45%
Fatigue (R = -1, 10⁷)220 – 310MPa
Density8.22g/cm³

Condition: Solution annealed 1175 °C / 1 h / WQ

When to pick this combination

Hastelloy X is the default when service temperature crosses Inconel 718's 650 °C ceiling. It runs comfortably to 900 °C in oxidising service and is the dominant alloy for printed combustor liners and afterburner hardware.

  • Service 650–900 °C
  • Combustor and exhaust hardware
  • Cyclic thermal duty without HIP+aging penalty
  • Replacement of wrought N06002 sheet fabrications

Typical defects and how the model accounts for them

Hot cracking at thin-wall to bulk transitions is the dominant defect. ForgeCast flags any abrupt thickness jump > 3× as a cracking-risk feature and recommends fillet radii ≥ 1 mm to redistribute solidification stress.

Required post-processing

The allowables above assume the full post-processing chain. Skipping any step degrades the row by 15–35 %.

  • Stress relief: 900 °C / 2 h / Ar
  • EDM from plate
  • Solution: 1175 °C / 1 h / water quench
  • HIP: 1175 °C / 100 MPa / 4 h (optional for fatigue-critical)
  • Machine sealing surfaces
  • No precipitation age — solid-solution strengthening only

Suggested build parameters

Starting recipe; tune against first-article inspection on geometry-sensitive features.

  • Layer: 40 μm
  • Laser: 270 W
  • Scan: 1000 mm/s
  • Hatch: 100 μm
  • Build plate: 100 °C

Frequently asked questions

Why no precipitation age?

Hastelloy X derives strength from solid-solution Mo/Cr/W, not γ′ or γ″ precipitates. Aging it would actually embrittle the alloy through carbide precipitation at grain boundaries.

Sources

  1. AMS 5754 — Hastelloy X sheet, strip, plate
  2. Haynes International Hastelloy X technical brochure

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