Osprey® H-X

SuperalloyDatasheet

Powder designed for

  • Additive Manufacturing
  • Metal Injection Moulding (MIM)

Standards

  • UNS N06002
  • EN Number 2.4665

Datasheet updated Apr 6, 2023 6:45 AM CET (supersedes all previous editions)

Disclaimer: Data and recommendations are for guidance only, and the suitability of a powder for a specific process or application can be confirmed only when we know the actual conditions. Continuous development may necessitate changes in technical data without notice. This datasheet is only valid for Osprey® powder.

Osprey® H-X is a nickel-chromium-molybdenum-iron superalloy characterized by high-temperature strength and good resistance to oxidation. The alloy is typically used in aerospace, oil and gas applications. Osprey® H-X is an alloy of the same type as Hastelloy® X and Inconel® alloy HX*.

This metal powder is manufactured by either induction melting under Vacuum Inert Gas Atomization (VIGA) or melting under argon prior to Inert Gas Atomization (IGA), producing a powder with a spherical morphology which provides good flow characteristics and high packing density. In addition, the powder has a low oxygen content and low impurity levels, resulting in a metallurgically clean product with enhanced mechanical performance.

*Hastelloy® is a trademark owned by Haynes International Inc. Inconel is a trademark owned by Huntington Alloys Corporation.

Chemical composition (nominal), %
Ni Fe C Cr Mo Co W Si Mn P S B
Bal. 18 ≤0.15 21.0 9.0 1.0 0.7 ≤0.1 ≤0.1 ≤0.015 ≤0.015 ≤ 0.008

Disclaimer: Data and recommendations are for guidance only, and the suitability of a powder for a specific process or application can be confirmed only when we know the actual conditions. Continuous development may necessitate changes in technical data without notice. This datasheet is only valid for Osprey® powder.