Astroloy M,Astroloy M,UNS N13017, Wire,,E FORU

British Specs:，American Specs:AMS 5882 Forgings，German Specs:

**Product Introduction: Astroloy M (UNS N13017) Wire** **Astroloy M (UNS N13017) Wire** is a premium powder metallurgy nickel-based superalloy in wire form, specifically engineered for extreme environment applications in aerospace, power generation, and specialized industrial sectors. Manufactured through advanced powder metallurgy processes followed by precision drawing and thermal treatments, this wire product delivers exceptional performance in applications requiring superior high-temperature strength, excellent creep resistance, and outstanding microstructural stability. The wire configuration of Astroloy M serves as a critical material for welding, additive manufacturing, and component fabrication where conventional materials cannot meet the demanding requirements of modern high-temperature engineering applications operating up to 980°C (1800°F). --- #### **Key Features & Advantages** * **Exceptional High-Temperature Performance**: Maintains mechanical integrity and properties at temperatures up to 980°C (1800°F) * **Superior Weld Metal Properties**: Excellent as filler metal for joining superalloys in critical applications * **Precision Diameter Control**: Consistent dimensional accuracy with excellent surface finish * **Excellent Formability**: Suitable for complex component fabrication and additive manufacturing processes * **Superior Microstructural Homogeneity**: PM processing ensures uniform, segregation-free structure * **Optimized for Additive Manufacturing**: Ideal feedstock for directed energy deposition (DED) processes --- #### **Chemical Composition (Typical Weight %)** | Element | Content (%) | Element | Content (%) | |---------|-------------|---------|-------------| | **Nickel (Ni)** | Balance | **Molybdenum (Mo)** | 4.5 - 5.5 | | **Chromium (Cr)** | 14.0 - 16.0 | **Aluminum (Al)** | 4.0 - 4.5 | | **Cobalt (Co)** | 16.0 - 18.0 | **Titanium (Ti)** | 3.4 - 3.8 | | **Carbon (C)** | 0.02 - 0.06 | **Boron (B)** | 0.015 - 0.030 | | **Zirconium (Zr)** | 0.025 - 0.050 | **Iron (Fe)** | ≤ 0.50 | | **Manganese (Mn)** | ≤ 0.10 | **Silicon (Si)** | ≤ 0.10 | | **Sulfur (S)** | ≤ 0.015 | **Copper (Cu)** | ≤ 0.10 | --- #### **Physical Properties** | Property | Metric Unit | Imperial Unit | |----------|-------------|---------------| | **Density** | 8.0 g/cm³ | 0.289 lb/in³ | | **Melting Range** | 1330 - 1380 °C | 2425 - 2515 °F | | **Thermal Expansion Coefficient** | 12.8 μm/m·°C (20-100°C) | 7.1 × 10⁻⁶ in/in·°F | | **Modulus of Elasticity** | 210 GPa | 30.5 × 10⁶ psi | | **Thermal Conductivity** | 11.5 W/m·K (100°C) | 80 Btu·in/hr·ft²·°F | | **Specific Heat** | 420 J/kg·K (20°C) | 0.10 Btu/lb·°F | --- #### **Mechanical Properties (Typical for Wire in Aged Condition)** | Property | Value (Metric) | Value (Imperial) | |----------|----------------|------------------| | **Tensile Strength, Ultimate** | 1300 - 1500 MPa | 189 - 218 ksi | | **Tensile Strength, Yield (0.2% Offset)** | 1000 - 1200 MPa | 145 - 174 ksi | | **Elongation at Break** | 12 - 20 % | 12 - 20 % | | **Hardness (Deposited Metal)** | 35 - 42 HRC | 35 - 42 HRC | --- #### **International Standards** * **AWS A5.14/A5.14M**: Specification for nickel-alloy bare welding electrodes and rods * **AMS 6306**: Powder metallurgy nickel-base superalloy products * **AMS 5832**: Wire for welding of corrosion and heat-resistant alloys * **UNS N13017**: Unified Numbering System designation * **OEM Specifications**: Compliant with major aerospace manufacturers' standards --- #### **Product Applications** **Welding & Fabrication:** - Repair and joining of turbine blades and vanes - Fabrication of high-temperature components - Repair of gas turbine engine components - Cladding of high-temperature surfaces - Build-up of worn superalloy components **Additive Manufacturing:** - Wire Arc Additive Manufacturing (WAAM) - Directed Energy Deposition (DED) processes - Laser metal deposition with wire - Component repair and refurbishment - Fabrication of large-scale superalloy components **Aerospace & Defense:** - Rocket engine component fabrication - Jet engine repair and maintenance - High-temperature structural components - Turbine component manufacturing - Exhaust system components **Specialized Applications:** - Nuclear component fabrication - High-temperature tooling manufacturing - Specialized industrial component production - Research and development applications --- **Available Wire Specifications:** - **Diameters**: 0.8mm - 2.4mm (0.032" - 0.094") - **Surface Finish**: Bright or cleaned finish - **Spool Sizes**: Standard 5-15kg spools - **Custom packaging available** --- **Disclaimer:** *Astroloy is a trademark associated with various high-performance alloy manufacturers. The information provided is for reference purposes only. Astroloy M wire properties are dependent on diameter, heat treatment, and specific application requirements. Professional engineering consultation and strict adherence to relevant specifications are essential for critical applications. Always consult manufacturer's technical data sheets for specific requirements and performance characteristics.*

Packing of Standard Packing: Typical bulk packaging includes palletized plastic 5 gallon/25 kg. pails, fiber and steel drums to 1 ton super sacks in full container (FCL) or truck load (T/L) quantities. Research and sample quantities and hygroscopic, oxidizing or other air sensitive materials may be packaged under argon or vacuum. Solutions are packaged in polypropylene, plastic or glass jars up to palletized 3092 gallon liquid totes Special package is available on request.