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
Press Fed 5748k
TRW N2O4/UDMH rocket engine. Study 1968. 1960's designs for 'big dumb booster'. Used on LCLV launch vehicle.

Status: Study 1968. Thrust: 56,368.00 kN (12,672,030 lbf). Specific impulse: 267 s. Specific impulse sea level: 245 s. Diameter: 6.10 m (20.00 ft).

Thrust (sl): 51,723.200 kN (11,627,838 lbf). Thrust (sl): 5,274,382 kgf. Chamber Pressure: 20.41 bar. Area Ratio: 6. Thrust to Weight Ratio: 0. Coefficient of Thrust vacuum: 5.59884325570492. Coefficient of Thrust sea level: 5.30484325570492.



Family: Storable liquid. Country: USA. Launch Vehicles: LCLV. Propellants: N2O4/UDMH. Stages: LCLV-1. Agency: TRW.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use