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Superalloy
Applications
It is suitable for manufacturing aviation engine combustion chamber components, honeycomb structures, diffusers, exhaust nozzles, and other hot end components for long-term use below 900 ℃.
Material characteristics
Loosse Density: ≥4.4 g/cm³
Tap Density: ≥5.0 g/cm³
Tensile Strength: ≥700 MPa
Yield strength: ≥300 MPa
Elongation/%：≥30%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Fuel nozzle
Applications
It is suitable for manufacturing high-temperature structural components such as aviation engine combustion chambers.
Material characteristics
Loosse Density: ≥2.4 g/cm³
Tap Density: ≥2.8 g/cm³
Tensile Strength: ≥800 MPa
Yield strength: ≥400 MPa
Elongation/%：≥30%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Cyclone
Applications
It is suitable for making high-temperature components such as combustion chamber flame tubes and guide vanes for aircraft engines.
Material characteristics
Loosse Density: ≥4.5 g/cm³
Tap Density: ≥5.2 g/cm³
Tensile Strength: ≥850 MPa
Yield strength: ≥400 MPa
Elongation/%：≥40%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Guide Vane
Applications
It is suitable for manufacturing components such as aerospace engine casings, guide vanes, mounting edges and cylinders, fuel manifolds, etc.
Material characteristics
Loosse Density: ≥4.4 g/cm³
Tap Density: ≥5.0 g/cm³
Tensile Strength: ≥830 MPa
Yield strength: ≥410 MPa
Elongation/%：≥35%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Aircraft shell
Applications
It is suitable for printing components such as turbine disks, rings, blades, shafts, fasteners, and elastic elements in the aviation, aerospace, nuclear, and petrochemical industries.
Material characteristics
Loosse Density: ≥4.4 g/cm³
Tap Density: ≥5.0 g/cm³
Tensile Strength: ≥1300 MPa
Yield strength: ≥1100 MPa
Elongation/%：≥15%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Rocket Nozzle
Applications
It is suitable for manufacturing high-temperature welded structural components such as aviation engine combustion chambers and after-burner chambers.
Material characteristics
Loosse Density: ≥4.4 g/cm³
Tap Density: ≥5.0 g/cm³
Tensile Strength: ≥1050 MPa
Yield strength: ≥700 MPa
Elongation/%：≥15%
（Heat-Treated，Room Temperature）
Powder morphology diagram
Application Examples
Combustion chamber
