MAR-M 509

MAR-M 509

MAR-M 509 is a vacuum-melted cobalt-based cast high-temperature alloy that exhibits excellent high-temperature strength, low creep rate, good oxidation resistance, and thermal shock resistance through carbide strengthening and solid solution strengthening. Its high chromium content (approximately 23%) combined with carbide-forming elements such as tungsten, tantalum, and titanium enables the alloy to maintain good mechanical properties and heat corrosion resistance at temperatures up to 1050°C. MAR-M 509 is widely used in high-temperature stationary components of aircraft engines and industrial gas turbines, such as turbine guide vanes and guides.
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Description
Technical Parameters

Products Features

High-Temperature Oxidation Resistance

Excellent High-Temperature Strength and Creep Resistance

MAR-M 509 possesses outstanding tensile strength, yield strength, and creep resistance at high temperatures due to solid solution strengthening (tungsten) in the cobalt matrix and dispersion strengthening by carbides (MC and M₂₃C₆ types). The alloy's long-term strength at 900°C is 40-50 MPa higher than that of the comparable alloy X-40, with an improved temperature capability of 40-50°C. It is suitable for stationary components such as turbine guide vanes and guides that are subjected to prolonged high-temperature stress.

High-Temperature Corrosion Resistance

Good Oxidation and Heat Corrosion Resistance

The high chromium content (approximately 23%) promotes the formation of a dense and stable Cr₂O₃ oxide film on the alloy surface, effectively preventing matrix oxidation in high-temperature oxidizing atmospheres. Additionally, the addition of elements such as tantalum and tungsten further enhances the alloy's heat corrosion resistance. The cobalt matrix offers good resistance to hot corrosion media such as sulfur and vanadium, making it particularly suitable for high-temperature environments in aircraft engines and industrial gas turbines.

High Stability

Good Microstructural Stability and Thermal Shock Resistance

MAR-M 509 maintains stable carbide structure during long-term high-temperature service and exhibits good thermal shock resistance. Even under conditions of frequent temperature fluctuations, its mechanical properties remain stable, making it suitable for hot-end components in aircraft engines and gas turbines that experience frequent start-up and shutdown cycles.

Good Processability

Casting and Machining Properties

MAR-M 509 is primarily formed using precision casting (investment casting) processes, which are suitable for manufacturing complex-shaped hot-end components such as turbine guide vanes and guides. The alloy has generally acceptable machining properties and is recommended to be machined with hard metal cutting tools. Its weldability is limited and requires the use of specialized processes.

Technical Specifications

Chemical Composition

 

Element

Standard Requirements

Notes

Co

Remaining quantity(52.5-58.45%)

Matrix elements that provide high-temperature strength, thermal stability, and excellent thermal corrosion resistance

Cr

22.5 --- 24.35%

Form a dense Cr₂O₃ protective film, providing oxidation and thermal corrosion resistance

Ni

9.0 --- 11.0%

Stabilize the austenitic structure, improve toughness and machinability

W

6.5 --- 7.5%

Provides significant solid solution strengthening and carbide strengthening, enhancing high-temperature creep resistance

Ta

3.0 --- 4.0%

Form stable MC-type carbides to enhance high-temperature strength and microstructural stability

C

0.55 --- 0.65%

Forms carbides with chromium, tungsten, and tantalum, serving as the core source of high-temperature strength

Zr

0.3 --- 0.6%

Minor additions to enhance grain boundary strength and creep resistance

Ti

0.15 --- 0.25%

Form carbides to assist in strengthening

Fe

≤ 1.5%

Strict control to ensure purity and organizational stability

Si

≤ 0.4%

Deoxidizer

Mn

≤ 0.1%

Deoxidizer

P

≤ 0.015%

Impurity element

S

≤ 0.015%

Prevent hot brittleness

Physical Properties

 

Property

Value/Range

Test Conditions

Density

8.86 g/cm³

Room Temperature (20°C)

Melting Point

1346 --- 1395°C

---

Coefficient of Thermal Expansion (20-100°C)

12.0 × 10⁻⁶ /K

---

Elastic modulus (Young's modulus)

200 --- 220 GPa

Room Temperature

Thermal Conductivity (20°C)

10 --- 12 W/(m·K)

---

Magnetism

Non-magnetic (weakly magnetic)

Cobalt-based alloys are typically non-magnetic or weakly magnetic at room temperature

Mechanical Properties (Annealed Condition, Typical Values)

 

Property

Typical Value

Specification

Tensile Strength

≥ 725 MPa

AMS 5370 / ASTM B815

Yield Strength (0.2% Offset)

≥ 450 MPa

AMS 5370 / ASTM B815

Elongation

≥ 5.0%

AMS 5370 / ASTM B815

Hardness (Cast Condition)

30-35 HRC(≈ 290-330 HB)

---

Note: This alloy is a cast cobalt-based high-temperature alloy. Low elongation is its typical characteristic, and it is suitable for static or low-strain operating conditions.

High-temperature performance

 
 

High-Temperature Strength Retention (Core Advantage):

MAR-M 509 exhibits excellent ability to maintain strength at high temperatures, with the following typical reference values:

Temperature

Tensile Strength (Typical Value)

Sustained Strength (100h, Typical Value)

Room Temperature

≥ 725 MPa

---

650°C

650 MPa

---

815°C

450 MPa

230 MPa

900°C

350 MPa

150 MPa

980°C

250 MPa

90 MPa

1090°C

150 MPa

38 MPa

Antioxidant Performance:

In oxidizing atmospheres up to 1000-1100°C, MAR-M 509 forms a dense and well-adhered Cr₂O₃ oxide layer on its surface, resulting in a lower oxidation weight gain rate compared to conventional stainless steels and many iron-based heat-resistant steels. In environments involving the combustion of sulfur-containing fuels, its thermal corrosion resistance exceeds that of many iron-based and nickel-based high-temperature alloys.

Microstructural Stability:

During long-term exposure at 800-1050°C, the carbide structure of MAR-M 509 remains stable, ensuring its mechanical properties and toughness during prolonged high-temperature service.

Applicable Media:

High-temperature air, combustion flue gases (containing sulfur and vanadium)

High-temperature oxidizing atmospheres

Thermal corrosion environments (containing Na₂SO₄, V₂O₅, etc.)

High-temperature gases (flow path environment of gas turbines)

Note: MAR-M 509 is primarily intended for use in high-temperature gaseous media environments and is not suitable for aqueous corrosion environments.

Steel Plate Processing
Steel Coil Processing
Steel Pipe Processing
Steel Bar Processing
 

MAR-M 509 is specifically designed for extreme high-temperature, oxidation, and thermal corrosion environments, and is recommended for use in the following areas:

 

Application Fields

  •  

    Aerospace: Turbine guide vanes, guides, turbine stator blades, combustion chamber components, and high-temperature seals of aircraft engines.

  •  

    Industrial Gas Turbines: Hot-end stator components such as turbine guide vanes, guides, transition pieces, and seal rings.

  •  

    Power Generation: High-temperature stator components and hot gas path components of gas turbines.

  •  

    Marine Engines: Turbine guide vanes and hot-end components of advanced marine engines.

  •  

    High-Temperature Industrial Furnaces: High-temperature load-bearing components such as furnace rolls, radiation tubes, heat treatment fixtures, and baskets (operating temperature ≤ 1050°C).

Delivery and Customization

We offer flexible and reliable supply chain solutions to ensure you receive MAR-M 509 materials that perfectly match your project requirements.

Form

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Sheet/Plate
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Bar/Rod
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Pipe / Tube
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Strip/Sheet Coil
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Wire/Wire Rod
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Precision Castings (Investment Casting)

Conventional Range

Thickness: 0.5 - 100 mm
Width: ≤ 1500 mm

Diameter Φ6-500mm

Outer diameter Φ10-300mm

Thickness: 0.1 – 3.0 mm
Width: 10 – 600 mm

Diameter Φ0.5-10mm

Customize according to the drawings

Customization Capability

Special thick/thin rolling, extra wide plates; special surface treatment, fixed-length cutting

Large-sized forged bars (up to Φ800 mm), special-shaped bars

Large-diameter thick-walled pipes, special alloy composition; Pipe end processing (beveling, fixed length)

Different hardness conditions, special heat treatment, acid-washed surface

Special surface treatment, precision drawing

Core morphology. Suitable for complex-shaped hot-end components such as turbine guide vanes, guides, and seal rings

Why Choose Us? - Reliable Engineering Technology. Dependable Delivery.

We are not just a supplier, but a trusted materials partner for you in China.

Sample Support & Quick Response

Vertically Integrated Production

Own 20,000㎡ facility with 10+ automated lines (8,000+ tons/year). In-house tooling & die center enables rapid customization and effective cost control - no middleman markup.

Full Traceability

Strict Quality Control at Every Stage

Full traceability across key QC checkpoints throughout production. 100% compliant with ASTM/ASME, EN, and GB standards. Material test reports available with every shipment.

Professional Logistics & Packaging

Reliable Delivery & Export Packaging

10+ years exporting to Europe, North America, Southeast Asia & Middle East with waterproof and anti-rust protection, combined with flexible shipping options ensures safe and on-time arrival.

Complete Export Documentation

Sample Validation Before Mass Production

We provide free samples for quality verification, allowing you to place bulk orders only after approval. We ensure consistency from sample to mass production by accurate dimensional measurement and transparent manufacturing.

FAQ

Q: What are the main advantages of MAR-M 509?

 

Q: What heat treatment is required for MAR-M 509?

 

Q: What is the maximum operating temperature?

 

Q: What is the difference between MAR-M 509 and X-40?

 

 

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