Astroloy M,Astroloy M Sheet,UNS N13017,E FORU

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

### **Product Introduction: Astroloy M (UNS N13017) Sheet** **Astroloy M (UNS N13017) Sheet** is a premium powder metallurgy nickel-based superalloy supplied in thin sheet form, designed for high-temperature applications requiring exceptional strength-to-weight ratio and superior thermal stability. Manufactured through advanced powder metallurgy processes followed by precision rolling and thermal treatments, this sheet product offers outstanding mechanical properties and microstructural homogeneity that exceed conventional wrought superalloys in extreme service conditions. The sheet form of Astroloy M enables the fabrication of complex components for aerospace and power generation applications where thin-section configurations must withstand temperatures up to 980°C (1800°F) while maintaining structural integrity under thermal cycling and mechanical loads. --- #### **Key Features & Advantages** * **Exceptional High-Temperature Capability**: Maintains superior mechanical properties at temperatures up to 980°C (1800°F) * **Excellent Strength-to-Weight Ratio**: Ideal for thin-section components where weight reduction is critical * **Superior Microstructural Homogeneity**: PM processing ensures uniform, fine-grained structure throughout the sheet * **Outstanding Oxidation Resistance**: Excellent resistance to high-temperature oxidation and corrosion * **Good Formability**: Can be formed into complex shapes in annealed condition before final heat treatment * **Enhanced Thermal Fatigue Resistance**: Withstands repeated thermal cycling without degradation --- #### **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 Heat-Treated Sheet)** | Property | Value (Metric) | Value (Imperial) | |----------|----------------|------------------| | **Tensile Strength, Ultimate** | 1350 - 1550 MPa | 196 - 225 ksi | | **Tensile Strength, Yield (0.2% Offset)** | 1050 - 1250 MPa | 152 - 181 ksi | | **Elongation at Break** | 12 - 18 % | 12 - 18 % | | **Creep Rupture Strength (980°C/100h)** | ≥ 110 MPa | ≥ 16.0 ksi | --- #### **International Standards** * **AMS 6306**: Primary specification for powder metallurgy nickel-base superalloy products * **ASTM B670**: Standard specification for precipitation-hardened nickel alloy plate, sheet, and strip * **AMS 5592**: Specification for thin sheet and strip * **UNS N13017**: Unified Numbering System designation * **OEM Specifications**: Compliant with major aerospace manufacturers' proprietary standards --- #### **Product Applications** **Aerospace & Defense:** - Jet engine thermal protection sheets and heat shields - Combustion chamber liners and afterburner components - Rocket engine thrust chamber assemblies - Turbine blade containment shrouds - High-temperature ducting and exhaust systems **Power Generation:** - Gas turbine combustion chamber components - Heat exchanger plates for advanced power systems - Thermal barrier system substrates - High-temperature furnace components **Specialized Applications:** - Hot forming tooling and fixtures - Nuclear reactor core components - High-temperature test equipment - Specialized processing equipment --- **Disclaimer:** *Astroloy is a trademark associated with various high-performance alloy manufacturers. The information provided is for reference purposes only. Astroloy M sheet properties may vary based on thickness, specific heat treatment, and manufacturing processes. Professional engineering consultation and strict adherence to relevant specifications are essential for critical applications. Always refer to manufacturer's technical data sheets for specific application requirements.*

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 3086 gallon liquid totes Special package is available on request.