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RBCC

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RBCC RBCC 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. Date: 1999. Thrust: 111.16 kN (24,989 lbf). Specific impulse: 3,500 s. Specific impulse sea level: 3,500 s. 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. Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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