Material Hastelloy X

Technical Reference Library

Hastelloy X

UNS N06002 Alloy Family Ni-Cr-Fe-Mo Ni (bal.) ~48.6%

Material Overview

Hastelloy X is a nickel-chromium-iron-molybdenum superalloy built around a nickel matrix (roughly 48.6% Ni) with substantial chromium (~21.8%) and iron (~18.5%) additions, plus about 9% molybdenum and a small tungsten and cobalt content for extra elevated-temperature strength. This combination gives Hastelloy X an unusually good balance of oxidation resistance, fabricability, and mechanical strength at high temperature compared to most other Ni-Cr-Fe-Mo alloys.

What sets Hastelloy X apart is specifically its high-temperature oxidation resistance combined with retained strength — it continues to perform well in continuous service well above 1,000°C (1,800°F), which is why it is one of the standard material choices for gas turbine combustor liners, transition ducts, and afterburner components, where the metal is directly exposed to hot combustion gas. It also sees use in furnace hardware and other high-temperature structural applications where oxidation resistance matters as much as strength.

International Designation Equivalents

Standard Designation
UNS N06002
BS HR6, 204
AFNOR NC22FeD

Chemical Composition

Element Content
Nickel (Ni) Balance (~48.6%)
Chromium (Cr) ~21.8%
Iron (Fe) ~18.5%
Molybdenum (Mo) ~9%
Cobalt (Co) ~1.5%
Tungsten (W) ~0.6%
Carbon (C) ~0.1%

Nominal composition; consult mill certification for a specific heat.

Machinability Explained

Hastelloy X is one of the more difficult common nickel superalloys to machine, and its cutting speed range reflects that — it runs noticeably slower than comparable Ni-Cr-Mo grades. Its low thermal conductivity concentrates heat right at the cutting edge instead of carrying it off in the chip, so tool tip temperatures climb quickly, and the alloy work-hardens readily under light or rubbing cuts, which can burnish the surface and complicate the start of the next pass.

The same high-temperature strength that makes Hastelloy X valuable in gas-turbine combustors also works against the tool: the alloy retains a large share of its strength at the elevated temperatures generated during cutting, so cutting forces stay high throughout the operation instead of easing as the material locally softens. High pressure and heat at the tool-chip interface promote galling and built-up edge on grades that are not specifically matched to nickel superalloys.

Because Hastelloy X combines these effects with genuinely lower machinability than many other nickel alloys, conservative speeds, rigid setups, sharp positive-rake geometries, and carbide grades engineered for superalloys are especially important here — pushing speeds or feeds past what the material can handle shows up quickly as accelerated notch and flank wear.

Recommended Cutting Speeds

Operation Vc (m/min) Vc (SFM)
Turning 60 – 85 200 – 280
Milling 45 – 60 150 – 200
Parting 40 – 50 130 – 160
Grooving 55 – 70 180 – 230
Drilling 55 – 70 180 – 230

Values assume favorable cutting conditions: a well-matched insert grade, rigid tool and workpiece clamping, good-quality raw material, short tool overhang, and nominal material hardness. Adjust down for interrupted cuts or poor rigidity.

Recommended FM Carbide Grades by Operation

Turning

Grade Coating ISO Application Range
FM524 CVD S05 – S10
FM2533 CVD S15

Parting / Grooving

Grade Coating ISO Application Range
FM2543 CVD S20
FM2553 CVD S30
FM2533 CVD S10

Milling

Grade Coating ISO Application Range
FM125 PVD S15 – S35

Ready to cut Hastelloy X? Shop FM Carbide inserts matched to this alloy's turning, parting, grooving, and milling requirements.

Shop Turning & Grooving Inserts Shop Milling Inserts

Recommended Insert Cutting-Edge Geometry

Parameter Value
Honing Size 0.02 – 0.05 mm / 0.001 – 0.002"
Rake Angle 13° – 18°
Land Angle Neutral
Land Width 0.10 – 0.20 mm / 0.004 – 0.008"
Ground Insert Recommended