An alpha-beta titanium alloy characterized by its strength-to-mass ratio and corrosion resistance. It is used in jet engines, gas turbines, pressure vessels, biomechanics parts, etc.

Made from an alloy of scandium, aluminum and magnesium. It is the only alloy to replace high-strength 7000 series aluminum and is stronger than titanium. It has excellent properties such as weldability and low thermal expansion, is suitable for anodizing, and has excellent corrosion resistance. It withstands high mechanical stress and is suitable for heavily loaded safety-critical parts that require low weight.

An ultra-low carbon alloy with very high strength and hardness properties derived from intermetallic compounds rather than carbon content. A material in which nickel is the main component, and cobalt, molybdenum, and titanium are secondary intermetallic compounds. It is ideal for high pressure die casting (HPDC) inserts and mold applications such as injection molding.

A precipitation hardening, nickel-base alloy that exhibits excellent tensile strength under extreme pressure and heat. It has rupture strength at temperatures up to 980°C and features excellent fatigue, creep and corrosion resistance in extreme environments. It is ideal for parts such as gas turbines in the aerospace and defense and chemical industries.

A nickel-based superalloy with high strength and heat resistance properties, offering strong protection against corrosion and oxidation. It can withstand high stress and a wide temperature range in and out of water, and can withstand corrosion even when exposed to strongly acidic environments. Ideal for nuclear power plant and shipbuilding applications.

A nickel, chromium, ion and molybdenum alloy with excellent formability and weldability. Easy to process due to localized corrosion resistance and oxidation resistance up to 2200°C. Often used in high temperature and corrosive environments, it is ideal for gas turbines, transition ducts, afterburners, spray bars, etc.

An alloy containing chromium, molybdenum, tungsten, and iron that is resistant to corrosion by seawater and has excellent weldability. It can withstand general corrosion, localized corrosion, chemicals mixed by various industries, and is also excellent against pitting corrosion, drafts, and stress corrosion cracking. It is often used in high-chloride, high-temperature corrosive environments such as exhaust gas cleaning equipment, nuclear fuel reprocessing, sour gas processing, and agricultural chemical production.

Developed by NASA to manufacture parts requiring high strength dispersion and high conductivity. The use of chromium and niobium in the alloy maintains strength at high temperatures and provides excellent creep resistance and low cycle fatigue life. Suitable for rocket engine parts that can be re-cooled, such as fuel injection nozzles and combustion chamber linings.

Developed for high temperature applications, it offers a unique combination of creep strength, thermal stability, weldability and workability not found in commercially available materials.

It is a lightweight, corrosion-resistant material with excellent weldability and dynamic load capacity. It is ideal for applications that require a combination of low weight and resistance to mechanical and thermal loads. It is a material primarily used in aerospace, energy, defense, and automotive.

It offers high strength and ductility, excellent thermal and electrical conductivity, and simplified post-processing. It is active in aerospace, defense, and motor sports.