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GST No. 27AAECK9442R1ZP
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HastelloyX is a wrought nickel base alloy with excellent high temperature strength and oxidation resistance. All of the product forms are excellent in terms of forming and welding. Although HastelloyX is primarily noted for heat and oxidation resistance it also has good resistance to chloride stress-corrosion cracking and has good resistance to carburization, excellent resistance to reducing or carburizing atmospheres. Alloy X is one of the most widely used nickel base super alloys for gas turbine engine components.
Applications:
HastelloyX finds use in petrochemical process equipment and gas turbines in the hot combustor zone sections. Also used for structural components in industrial furnace applications because of the excellent oxidation resistance.
HastelloyX is recommended especially for use in furnace applications because it has unusual resistance to oxidizing, reducing, and neutral atmospheres. Furnace rolls made of this alloy were still in good condition after operating for 8700 hours at 2150 Deg. F. Furnace trays, used to support heavy loads, have been exposed to temperatures up to 2300 Deg. F. in an oxidizing atmosphere without bending or warping. Alloy X is equally suitable for use in jet engine tailpipes, afterburner components, turbine blades, nozzle vanes, cabin heaters, and other aircraft parts.
Gas turbine combustion cans and ducting, heat-treating equipment.
Alloy X has wide use in gas turbine engines for combustion zone components such as transition duct, combustor cans, spray bars and flame holders as well as in afterburners, tailpipes and cabin heaters. It is recommended for use in industrial furnace applications because it has unusual resistance to oxidizing, reducing and neutral atmospheres. Furnace rolls of this alloy were still in good condition after operating for 8,700 hours at 2150 degrees F (1177 degrees C).HastelloyX is also used in the chemical process industry for retorts, muffles, catalyst support grids, furnace baffles, tubing for pyrolysis operations and flash drier components.
Useful Properties for Aircraft and Furnace Parts -HastelloyXis recommended especially for use in furnace applications because it has unusual resistance to oxidizing, reducing, and neutral atmospheres. Furnace rolls made of this alloy were still in good condition after operation for 8,700 hours at 2150 Deg. F (1177 Deg. C).
Minimum Order Quantity: 10 Kg
Product Brochure
| Alloy Grade | B2 |
| Grade | Hastelloy X |
| Material | Hastelloy X |
| Usage/Application | Industry |
Hastelloy X, designated as UNS N06002, is a high-performance nickel-based alloy primarily developed for extreme environments involving high temperatures, oxidation, and stress. Produced in multiple product forms—such as rods, sheets, bars, tubes, and plates—Hastelloy X plates are especially prized for their strength, thermal stability, and corrosion resistance in elevated temperature operations. These characteristics make Hastelloy X an essential material in critical components for aerospace engines, gas turbines, heat treatment furnaces, and petrochemical reactors.
This document delivers a complete technical guide on Hastelloy X plates, covering their chemical composition, mechanical and physical properties, fabrication and welding characteristics, applications, corrosion behavior, thermal performance, industry specifications, and commercial considerations.
Chemical Composition (% by Weight)| Element | Content (%) |
|---|---|
| Nickel (Ni) | 47.0 min |
| Chromium (Cr) | 20.5 – 23.0 |
| Iron (Fe) | 17.0 – 20.0 |
| Molybdenum (Mo) | 8.0 – 10.0 |
| Cobalt (Co) | 0.5 – 2.5 |
| Tungsten (W) | 0.2 – 1.0 |
| Manganese (Mn) | 1.0 max |
| Silicon (Si) | 1.0 max |
| Carbon (C) | 0.05 – 0.15 |
| Aluminum (Al) | 0.50 max |
| Titanium (Ti) | 0.15 max |
| Sulfur (S) | 0.03 max |
The alloy's austenitic microstructure contributes to its high ductility and stability even at elevated temperatures above 1000°C.
Room Temperature Properties (Annealed Condition)
| Property | Value |
|---|---|
| Tensile Strength | 690 – 827 MPa (100–120 ksi) |
| Yield Strength (0.2% offset) | 276 – 345 MPa (40–50 ksi) |
| Elongation (% in 50 mm) | 30–45% |
| Hardness (Rockwell B) | 80–95 |
| Modulus of Elasticity | ~214 GPa |
| Impact Toughness | Excellent even at sub-zero temperatures |
| Property | Value |
|---|---|
| Density | 8.22 g/cm³ |
| Melting Point | 1260 – 1355°C |
| Coefficient of Expansion | 13.3 µm/m·K (20–1000°C) |
| Thermal Conductivity | 9.1 W/m·K at 100°C |
| Electrical Resistivity | 1.3 µΩ·m |
| Specific Heat Capacity | 0.44 J/g·K |
Its lower thermal conductivity compared to steels and super-austenitic alloys enables Hastelloy X to act as a thermal barrier material.
WeldabilityHastelloy X is readily weldable using most standard processes, including:
GTAW (TIG)
GMAW (MIG)
SMAW (Stick)
Electron Beam and Laser Welding
Weldments exhibit excellent strength, but post-weld heat treatment may be used to relieve residual stress and optimize grain structure, especially in critical applications.
ASTM Standards
ASTM B435: Plate, sheet, and strip
ASTM B572: Bar and forging stock
ASTM B619/B622: Seamless pipe and tube
ASTM B366: Fittings made from Hastelloy X
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Minimum Order Quantity: 5 Kg
Product Brochure
| Size/Diameter | AS PER ORDER, 5MM - 200MM |
| Shape | Round |
| Brand | IMPORTED |
| Grade | X |
| Material Grade | HASTELLOY X |
| Usage/Application | Manufacturing |
| Test Certificate | AVAILABLE |
| Payment Terms | ADVANCE |
| Finishing | BRIGHT |
| Density | 8.9% |
| Color | BRIGHT |
| Material | HASTELLOY X |
INTRODUCTION Hastelloy X Round Bar (UNS N06002, W.Nr. 2.4665) is a nickel–chromium–iron–molybdenum-based superalloy widely known for its exceptional strength, oxidation resistance, and outstanding performance at elevated temperatures up to 1200 °C (2200 °F).
It is one of the most versatile high-temperature alloys, primarily used in the aerospace, gas turbine, chemical processing, power generation, and petrochemical industries.
The round bar form of Hastelloy X provides machinability, fabrication flexibility, and excellent weldability, making it an ideal raw material for producing shafts, fasteners, turbine components, furnace rolls, pressure vessels, heat treatment fixtures, and chemical plant equipment.
| Element | Content (%) | Function |
|---|---|---|
| Nickel (Ni) | Balance (~47–50) | Base metal, corrosion & heat resistance |
| Chromium (Cr) | 20.5 – 23.0 | Provides oxidation resistance |
| Iron (Fe) | 17.0 – 20.0 | Solid solution strengthening |
| Molybdenum (Mo) | 8.0 – 10.0 | Improves creep & corrosion resistance |
| Tungsten (W) | 0.2 – 1.0 | Enhances creep strength |
| Cobalt (Co) | ≤ 2.5 | Improves hot strength |
| Carbon (C) | 0.05 – 0.15 | Enhances creep strength at high temperatures |
| Manganese (Mn) | ≤ 1.0 | Improves workability |
| Silicon (Si) | ≤ 1.0 | Improves oxidation resistance |
| Phosphorus (P) | ≤ 0.04 | Controlled to reduce brittleness |
| Sulfur (S) | ≤ 0.03 | Controlled to improve weldability |
| Property | Typical Value |
|---|---|
| Tensile Strength | 750 – 850 MPa |
| Yield Strength (0.2% offset) | ≥ 350 MPa |
| Elongation | ≥ 30% |
| Hardness | ~ 80 – 95 HRB (Annealed) |
| Impact Strength | Excellent at room and elevated temperature |
| Creep Strength | Outstanding up to 815 °C (1500 °F) |
Density: 8.22 g/cm³
Melting Point: 1355 – 1400 °C
Thermal Conductivity: 9.1 W/m·K at 20 °C
Electrical Resistivity: 1.29 µΩ·m
Elastic Modulus: 205 GPa
Thermal Expansion: 14.2 µm/m·K at 20–1000 °C
UNS Number: N06002
Werkstoff Nr.: 2.4665
EN Standard: NiCr22Fe18Mo
ASTM Standards:
ASTM B572 – Bars, rods, wires of UNS N06002
ASTM B435 – Plate, sheet, strip
ASTM B366 – Fittings.
Mechanical Testing – Tensile, hardness, impact.
Chemical Analysis – Optical Emission Spectrometry.
Microstructure Examination – To confirm grain structure.
Non-Destructive Tests – Ultrasonic, Eddy current.
Corrosion Tests – Oxidation, carburization testing.
Additional Information:
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