GH3536 Bar – Hastelloy X UNS N06002 Nickel Alloy Bar

Short Description:

GH3536 Bar, also known as Hastelloy X / UNS N06002 / Alloy X, is a nickel-chromium-iron-molybdenum high temperature alloy bar with excellent oxidation resistance, high-temperature strength and good fabricability. It is widely used in gas turbine components, combustion chambers, furnace parts, aerospace equipment, petrochemical systems and high-temperature industrial machinery. SASA ALLOY supplies GH3536 bars in hot rolled, forged, peeled, turned, ground and polished conditions with EN 10204 3.1 certificate, PMI testing and full material traceability.


  • Grade: GH3536 / Hastelloy X / UNS N06002 / Alloy X
  • Surface: Hot Rolled / Forged / Peeled / Turned /Polished
  • Specification: Diameter 6-300mm, Length 500-6000mm
  • Diameter 6-300mm, Length 500-6000mm: Gas Turbine / Furnace Parts / Aerospace
  • Product Detail

    Product Tags

    Product Short Description

    GH3536 Bar, also known as Hastelloy X Bar, UNS N06002 Bar and Alloy X Bar, is a nickel-chromium-iron-molybdenum high temperature alloy bar designed for excellent oxidation resistance, high-temperature strength and good fabricability. It provides reliable performance in high-temperature environments and is widely used in gas turbine components, combustion chambers, furnace parts, aerospace equipment, petrochemical systems and industrial heat-resistant components.

    SASA ALLOY supplies GH3536 bars in hot rolled, forged, peeled, turned, ground, polished and machined conditions according to customer requirements. Products can be supplied with chemical composition analysis, mechanical testing, PMI testing, ultrasonic testing, dimensional inspection, surface inspection, EN 10204 3.1 material certificate and full heat number traceability.

    • Product Name: GH3536 Bar – Hastelloy X UNS N06002 Nickel Alloy Bar
    • Material Grade: GH3536 / Hastelloy X / UNS N06002 / Alloy X
    • Product Type: Nickel-Chromium-Iron-Molybdenum High Temperature Alloy Bar
    • Main Feature: Excellent oxidation resistance, high-temperature strength and good thermal stability
    • Applications: Gas turbine, combustion chamber, furnace parts, aerospace, petrochemical and high-temperature equipment

    Product Parameters

    Item Specification
    Product Name GH3536 Bar
    Material Grade GH3536 / Hastelloy X / UNS N06002 / Alloy X
    Material Type Nickel-Chromium-Iron-Molybdenum High Temperature Alloy
    Product Form Round Bar, Forged Bar, Peeled Bar, Turned Bar, Ground Bar, Custom Machined Bar
    Diameter 6 mm – 300 mm or customized
    Length 500 mm – 6000 mm or cut to size
    Surface Condition Hot Rolled, Forged, Peeled, Turned, Ground, Polished, Machined
    Heat Treatment Solution Annealed, Annealed or as required
    Standard UNS N06002, ASTM B572, ASTM B435, AMS 5754, AMS 5536, EN, DIN, JIS, GB or customer specification
    Inspection Chemical Analysis, Mechanical Test, PMI Test, UT Test, Hardness Test, Dimensional Inspection
    Certificate EN 10204 3.1 Material Certificate available
    Processing Service Cutting, Sawing, Turning, Grinding, Polishing, CNC Machining, Custom Size Processing

    Chemical Composition

    GH3536 / Hastelloy X is a nickel-chromium-iron-molybdenum alloy with excellent high-temperature oxidation resistance and good mechanical strength. The following chemical composition is for general reference only. Final composition should be confirmed according to the applicable standard, purchase order and mill test certificate.

    Element Ni Cr Fe Mo Co W C Mn Si P S
    Content % Balance 20.5 – 23.0 17.0 – 20.0 8.0 – 10.0 0.5 – 2.5 0.2 – 1.0 0.05 – 0.15 ≤1.00 ≤1.00 ≤0.040 ≤0.030

    Mechanical Properties

    Mechanical properties of GH3536 Bar may vary depending on diameter, production method, heat treatment condition and applicable standard. The alloy is mainly selected for high-temperature strength, oxidation resistance and stable performance in thermal service environments.

    Condition Tensile Strength Yield Strength Elongation Hardness Typical Use
    Solution Annealed / Typical 690 MPa min 275 MPa min 30% min According to condition High-temperature and oxidation-resistant components
    Forged / Custom According to order requirement According to order requirement According to order requirement According to order requirement Heavy-duty bars and machined components
    Machined / Ground According to drawing According to drawing According to drawing According to drawing Precision machined high-temperature parts

    Note: Final mechanical properties should be confirmed according to ASTM, AMS, customer specification, heat treatment condition and material test certificate.

    Common Size Table

    Diameter Length Surface Availability
    6 – 20 mm 500 – 3000 mm Hot Rolled / Ground / Polished Production / Customized
    20 – 80 mm 1000 – 6000 mm Hot Rolled / Peeled / Turned Production
    80 – 150 mm 1000 – 6000 mm Forged / Turned / Ground Made to Order
    150 – 300 mm Cut to Size Forged / Machined Custom Production

    Different Specifications Comparison

    Type Size Range Surface Condition Typical Use
    GH3536 Round Bar 6 – 100 mm Hot Rolled / Peeled / Ground Gas turbine, furnace parts and industrial components
    GH3536 Forged Bar 80 – 300 mm Forged / Turned / Machined Aerospace, combustion chamber and heavy-duty high-temperature parts
    GH3536 Machined Bar According to drawing Ground / Polished / CNC Machined Precision machined high-temperature components
    GH3536 Cut Bar Cut to length Sawed / Ground Machining blanks and maintenance replacement parts

    Equivalent Standards and International Names

    GH3536 is commonly considered equivalent to Hastelloy X / UNS N06002 type nickel alloy. Customers may search for GH3536 Bar, Hastelloy X Bar, Alloy X Bar, UNS N06002 Bar or nickel-chromium-molybdenum high-temperature alloy bar.

    Country / Standard Common Name Equivalent Grade
    China GH3536 Nickel-Chromium-Iron-Molybdenum High Temperature Alloy
    UNS UNS N06002 Hastelloy X
    Commercial Name Hastelloy X / Alloy X GH3536 Equivalent
    ASTM ASTM B572 / ASTM B435 Nickel Alloy X Bar / Plate Reference
    AMS AMS 5754 / AMS 5536 High Temperature Nickel Alloy

    Production Process Flow

    The production process of GH3536 Bar requires strict control of raw material selection, melting, hot working, heat treatment, machining and inspection to ensure stable high-temperature performance, oxidation resistance and mechanical reliability.

    1. Raw Material Selection
    2. Melting
    3. Ingot / Billet Preparation
    4. Forging / Hot Rolling
    5. Solution Annealing
    6. Straightening
    7. Turning / Peeling
    8. Grinding / Polishing
    9. Inspection
    10. Packing
    11. Delivery
    Process Step Description Quality Control Point
    Raw Material Selection Select qualified GH3536 / Hastelloy X raw materials Raw material certificate and traceability
    Melting Control alloy chemistry and impurity elements Chemical composition analysis
    Forging / Hot Rolling Produce bar shape and improve internal structure Temperature control, forging ratio and dimensional control
    Solution Annealing Heat treatment to stabilize structure and performance Temperature, holding time and cooling method
    Inspection Final inspection before shipment PMI, UT, dimension, surface and certificate review

    Product Inspection

    1. Chemical Composition Inspection

    Chemical composition analysis is performed to verify nickel, chromium, iron, molybdenum and other alloying elements. This helps confirm that the bar meets GH3536 / Hastelloy X / UNS N06002 requirements.

    2. Mechanical Properties Testing

    Tensile strength, yield strength, elongation and hardness can be tested according to customer requirements and applicable standards.

    3. Ultrasonic Testing

    UT testing can be performed to check internal soundness of forged or large-size GH3536 bars, especially for aerospace, gas turbine and critical industrial components.

    4. PMI Testing and Dimensional Inspection

    PMI testing helps verify material grade and prevent material mix-up. Diameter, length, straightness, tolerance and surface condition are inspected before shipment.

    Product Packaging

    SASA ALLOY provides export-grade packaging for GH3536 Bars to protect the material during sea, air and land transportation.

    • Bundle Packing: Suitable for long bars and batch shipments.
    • Plastic Film Protection: Applied to polished or machined surfaces to reduce scratches.
    • Waterproof Wrapping: Used to protect bars from moisture during transportation.
    • Wooden Case Packaging: Suitable for precision machined bars or export shipments.
    • Clear Marking: Grade, heat number, size, quantity and customer PO number can be marked on labels.
    GH3652 Bar Box Packaging
     GH3652 Bar Box Packing
     GH3652 Bar packing

    Applications

    GH3536 Bar is widely used in high-temperature and oxidation-resistant applications where thermal stability, fabricability and mechanical reliability are required.

    Industry Typical Applications Why GH3536 Is Used
    Aerospace Combustion chambers, exhaust components, engine parts Excellent oxidation resistance and high-temperature strength
    Gas Turbine Turbine components, hot gas ducting and support parts Stable performance in high-temperature gas environments
    Industrial Furnace Furnace parts, heat treatment fixtures, radiant tubes Resistance to oxidation and thermal exposure
    Petrochemical High-temperature process components, supports and machined parts Good corrosion resistance and mechanical stability
    Industrial Machinery High-temperature mechanical parts and custom components Good workability and reliable high-temperature performance

    Why Choose SASA ALLOY?

    • Professional supplier of GH3536 / Hastelloy X / UNS N06002 nickel alloy bars
    • Customized diameter, length, surface condition and heat treatment available
    • Support for ASTM, AMS, UNS, EN, DIN, JIS, GB and customer specifications
    • Material traceability with heat number control
    • EN 10204 3.1 material certificate available
    • Chemical analysis, mechanical testing, PMI testing, UT testing and dimensional inspection support
    • Export packaging suitable for international transportation
    • Suitable for aerospace, gas turbine, furnace, petrochemical and high-temperature industrial applications

    FAQ

    What is GH3536 Bar?

    GH3536 Bar is a nickel-chromium-iron-molybdenum high-temperature alloy bar commonly considered equivalent to Hastelloy X / UNS N06002. It is used for oxidation-resistant and high-temperature applications.

    Is GH3536 the same as Hastelloy X?

    GH3536 is commonly regarded as the Chinese designation corresponding to Hastelloy X / UNS N06002 type alloy. Final equivalence should be confirmed by chemical composition, standard and mill test certificate.

    Can SASA ALLOY provide custom size GH3536 bars?

    Yes. SASA ALLOY can supply GH3536 bars in customized diameter, length, surface condition and heat treatment condition according to customer requirements.

    What inspections can be provided?

    Chemical analysis, mechanical testing, PMI testing, UT testing, hardness testing, dimensional inspection and EN 10204 3.1 material certificate can be provided according to order requirements.

    What are the main applications of GH3536 Bar?

    GH3536 Bar is mainly used for aerospace components, combustion chambers, gas turbine parts, furnace components, petrochemical equipment and high-temperature industrial machinery.

    Contact Us

    If you are looking for GH3536 Bar, Hastelloy X Bar, UNS N06002 Bar or customized high-temperature nickel alloy bars, please contact SASA ALLOY with your required grade, standard, diameter, length, heat treatment condition, surface condition, quantity and inspection requirements. Our team can provide professional material solutions for high-temperature nickel alloy applications.


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