Aluminum (AlSi10Mg) |
Casting alloy with good strength and hardness. Used for its good combination of mechanical and thermal properties when low specific weight is a requirement. |
Aerospace and automotive production parts |
Maraging Steel (18 Mar 300 / 1.2709) |
Martensitic hardening steel with good toughness, tensile strength and low warping properties. Can be easily machined, hardened, and welded. High malleability allows it to be formed easily for different applications. |
Injection molding tools for series production and other mechanical parts. |
Cobalt Chrome (UNS R31538 / ASTM F75) |
Superalloy with excellent wear and corrosion resistance. Great mechanical properties at elevated temperatures. Wear resistance, corrosion resistance, and biocompatibility make it ideal in surgical implants and other high-wear applications. |
Aerospace and medical (implants) production parts. |
Stainless Steel (316L) |
Austenitic chromium-nickel alloy with high strength and wear resistance. Good elevated temperature strength, formability and weldability. Used for its excellent corrosion resistance including pitting corrosion and chloride environments. |
Aerospace and medical (surgical tools) production parts. |
Stainless Steel (15-5 PH) |
Precipitation-hardened stainless steel with excellent strength, toughness, and hardness. It's good combination of strength, fabricability, ease of heat treatment, and corrosion resistance makes it a popular material that is used in many industries. |
Production parts for various industries. |
Stainless Steel (17-4 PH) |
Precipitation-hardened stainless steel with excellent strength and fatigue properties. It's good combination of strength, fabricability, ease of heat treatment, and corrosion resistance makes it a commonly used steel in many industries. 17-4 PH Stainless steel contains ferrite, while 15-5 Stainless Steel is ferrite-free. |
Production parts for various industries. |
Titanium (Ti6Al4V / Grade 5) |
Excellent mechanical properties and corrosion resistance with a low specific weight. Most common titanium alloy used for its excellent strength-to-weight ratio, fabricability, and ability to heat treat. |
Aerospace and automotive (motorsports) production parts. |
Titanium (Ti6Al4V / Grade 23) |
Excellent mechanical properties and corrosion resistance with low specific weight. Excellent strength-to-weight ratio, fabricability, and biocompatibility. Improved ductility and fatigue strength make it widely used for medical implants. |
Medical (implants) production parts. |
Nickel Alloy (Inconel™ 718 / UNS N07718) |
Super alloy with excellent yield, tensile, and creep-rupture strength at high temperatures. Used for high strength applications in extreme environments. Excellent weldability compared to other nickel-based super alloys. |
Aerospace (high-temperature turbine components) production parts. |
Nickel Alloy (Inconel™ 625 / UNS N06625) |
Superalloy with excellent strength and toughness at high temperatures. High corrosion resistance. Used for high strength applications in extreme environments. Extra resistant to pitting, crevice corrosion, and stress-corrosion cracking in chloride environments. |
Aerospace (high-temperature turbine components) production parts. |
Nickel Alloy (UNS N06002 / Hastelloy X) |
Superalloy with exceptional combination of high-temperature strength, fabricability, and oxidation resistance. Used for high strength applications in extreme environments. Resistant to stress-corrosion cracking in petrochemical environments. Excellent forming and welding characteristics. |
Production parts in severe thermal conditions and high risk of oxidation (combustion chambers, burner and supports in industrial furnaces). |