RBCC
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Credit: Boeing / Rocketdyne
Rocketdyne LOx/LH2 rocket engine. Isp>400s. Rocket Based Combined-Cycle A5 Development Engine; integrated rocket, air-augmented rocket, ramjet, and scramjet propulsion elements into a single flow path.
Rocket Based Combined-Cycle A5 Development Engine. Pressure-fed or pump-fed. The RBCC engine integrates rocket, air-augmented rocket, ramjet, and scramjet propulsion elements into a single flow path. Rocket specific impulse 400 seconds; minimum thrust 600 lbs. Thrust and specific impulse values are at sea level.
Thrust (sl): 111.158 kN (24,989 lbf). Thrust (sl): 11,335 kgf.
Related
- Country
- USA
- Propellants
- Lox/LH2
- Agency
- Rocketdyne