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
Plug-Nozzle SERV
Notional LOx/LH2 rocket engine. Study 1971. Used on Shuttle SERV launch vehicle.

Status: Study 1971. Thrust: 31,980.20 kN (7,189,435 lbf). Specific impulse: 455 s. Specific impulse sea level: 367 s. Burn time: 249 s.

Thrust (sl): 25,794.900 kN (5,798,924 lbf). Thrust (sl): 2,630,386 kgf.

Country: USA. Launch Vehicles: SERV. Propellants: Lox/LH2. Stages: Shuttle SERV-1.
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