A range of high-performance nickel-based alloys is available to meet the demands of high-temperature and corrosive environments. HX offers exceptional resistance in corrosive, high-temperature applications with its high chromium, molybdenum, and iron content. IN625 is ideal for aircraft engine components below 650°C, providing strength through precipitation hardening with added chromium, molybdenum, and niobium. IN718 excels at up to 700°C, offering superb tensile and fatigue strength for aircraft engines and turbines. K-500 combines nickel-copper alloying for excellent corrosion resistance and high strength in challenging environments.
Nikon SLM Solutions' IN718 is a precipitation-hardenable nickel-chromium-alloy. With excellent tensile, fatigue, creep, and rupture strengths up to 700 °C, IN718 is an important alloy for production of components for aircraft engines, (gas) turbines, and other high temperature applications.
Material characteristicsMonolithic Thrust Chamber
Nikon SLM Solutions' IN625 is a precipitation-hardenable nickel-based material alloyed with chromium, molybdenum, and niobium. IN625 is a typical material for construction of aircraft engine components with service temperatures below 650 °C.
Material characteristicsImpeller
Nikon SLM Solutions' HX is a nickel-based alloy with high contents of chromium, molybdenum, and iron. HX is an important alloy for high temperature applications in corrosive environments for a number of industries.
Material characteristicsNikon SLM Solutions' K-500 is a precipitation-strengthened nickel-copper material that is good for use in challenging environments requiring excellent corrosion resistance or high strength at elevated temperatures.
Material characteristics