Encyclopedia Astronautica
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

L-2 Linear Aerospike Booster
L-2 Linear Aerospike
L-2 Linear Aerospike
L-1 Linear Aerospike Booster
Credit: Boeing / Rocketdyne
Rocketdyne LOx/Kerosene rocket engine. Gas generator, pump-fed. Thrust and specific impulse values are at sea level.

Date: 1971. Thrust: 444.63 kN (99,957 lbf). Specific impulse: 455 s. Specific impulse sea level: 455 s.

Thrust (sl): 444.630 kN (99,957 lbf). Thrust (sl): 45,340 kgf.

Country: USA. Propellants: Lox/Kerosene. Agency: Rocketdyne.



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
© 1997-2016 Mark Wade - Contact
© / Conditions for Use