Astroloy M,Astroloy M Tube,UNS N13017,E FORU

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

### **Product Introduction: Astroloy M (UNS N13017) Tube** **Astroloy M (UNS N13017) Tube** is a premium powder metallurgy nickel-based superalloy product form specifically engineered for extreme service conditions in aerospace, power generation, and specialized industrial applications. Manufactured through advanced powder metallurgy processes followed by precision tube forming techniques, this product delivers exceptional performance where conventional tubing materials cannot meet the demanding requirements of high temperature, high pressure, and corrosive environments. The tube configuration of Astroloy M represents one of the most challenging product forms to manufacture, requiring specialized knowledge in powder metallurgy and thermomechanical processing to maintain the alloy's exceptional properties in thin-walled sections. --- #### **Key Features & Advantages** * **Ultra-High Temperature Capability**: Maintains excellent mechanical properties and structural integrity at temperatures up to 980°C (1800°F) * **Superior Pressure Containment**: Exceptional hoop strength and stress rupture characteristics in thin-walled configurations * **Outstanding Creep Resistance**: Excellent long-term dimensional stability under constant load at elevated temperatures * **Premium Microstructural Homogeneity**: Powder metallurgy manufacturing ensures consistent properties throughout the tube circumference and length * **Excellent Oxidation and Corrosion Resistance**: Withstands aggressive thermal environments and corrosive media * **Optimized Weight-to-Strength Ratio**: Ideal for weight-critical applications requiring maximum performance --- #### **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 HIPed + Heat-Treated Condition)** | Property | Value (Metric) | Value (Imperial) | |----------|----------------|------------------| | **Tensile Strength, Ultimate** | 1400 - 1550 MPa | 203 - 225 ksi | | **Tensile Strength, Yield (0.2% Offset)** | 1100 - 1300 MPa | 160 - 189 ksi | | **Elongation at Break** | 12 - 18 % | 12 - 18 % | | **Stress Rupture Strength (980°C/100h)** | ≥ 110 MPa | ≥ 16.0 ksi | --- #### **International Standards** * **AMS 6306**: Primary specification for powder metallurgy nickel-base superalloy products * **ASTM B829**: Standard specification for seamless nickel and nickel alloy tube * **ASME SB829**: ASME boiler and pressure vessel code specification * **AMS 5580**: General specification for seamless superalloy tube * **UNS N13017**: Unified Numbering System designation * **OEM Specifications**: Custom specifications for aerospace and defense applications --- #### **Product Applications** **Aerospace & Defense:** - Jet engine high-pressure fuel and hydraulic tubing - Rocket engine combustion chamber coolant passages - Turbine bleed air systems - Afterburner fuel manifold systems - Thermal management system components **Power Generation:** - Advanced gas turbine fuel injection systems - Heat exchanger tubes for ultra-supercritical power plants - Nuclear reactor advanced concept heat transfer components **Specialized Industrial:** - High-temperature chemical processing equipment - Pyroprocessing system heat exchanger tubes - Specialized furnace radiant tubes and components - Test and measurement equipment for extreme environments --- **Disclaimer:** *Astroloy is a trademark associated with various high-performance alloy manufacturers. Astroloy M tube represents a specialized application requiring advanced manufacturing capabilities. The information provided is for reference purposes only. Final material properties and performance characteristics depend on specific manufacturing processes, heat treatments, wall thickness, and end-use conditions. Professional engineering consultation and compliance with relevant specifications are essential for critical applications.*

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 3084 gallon liquid totes Special package is available on request.