Application
Aerospace
Replacing nickel-based superalloys with SiCf/SiC ceramic matrix composites reduces weight by 60% and increases temperature resistance by over 200°C, improving thrust-to-weight ratio and reducing cooling air consumption.
Material Adaptation & Solutions
For the integrated thermal protection and load-bearing requirements of reusable spacecraft and hypersonic vehicles, SiCf/SiC ceramic matrix composites replace conventional alloys, achieving a 60% weight reduction and an increase in temperature resistance of over 200°C, balancing thermal protection and structural load-bearing while significantly reducing cooling gas consumption.
Typical Components
Thermal Protection Structures
Integrated thermal protection and load-bearing structural components for hypersonic aerodynamic heating environments.
Control Surface and Cabin Structural Components
Maintains dimensional stability and structural integrity under coupled high-temperature and high-vibration conditions.
High-Temperature Engine Components
Used in the high-temperature sections of aerospace propulsion systems, replacing alloy components with high density and limited temperature resistance.
