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
Liberty-1
Notional LOx/Kerosene rocket engine. Development ended 1988. Pressure-fed engine. Used on Liberty launch vehicle.

Status: Development ended 1988. Thrust: 245.20 kN (55,123 lbf). Unfuelled mass: 270 kg (590 lb). Specific impulse: 270 s. Specific impulse sea level: 230 s. Burn time: 157 s. Diameter: 1.58 m (5.18 ft).

Thrust (sl): 208.800 kN (46,940 lbf). Thrust (sl): 21,296 kgf. Engine: 270 kg (590 lb). Area Ratio: 5. Thrust to Weight Ratio: 92.59.



Country: USA. Launch Vehicles: Liberty. Propellants: Lox/Kerosene. Stages: Liberty 1.

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