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
LR8-RM-5
Reaction Motors. Advanced version of the LR-11, 4 chambers. Engine in the X-1E was modified in 1958 to increase chamber pressure to 20 atm and burn Hydyne fuel.

Status: Out of Production. Thrust: 26.67 kN (5,996 lbf). Height: 1.45 m (4.75 ft). Diameter: 0.46 m (1.50 ft).

Chambers: 4. Thrust (sl): 26.670 kN (5,996 lbf). Thrust (sl): 2,720 kgf. Engine: 157 kg (346 lb). Chamber Pressure: 17.00 bar.



Country: USA. Spacecraft: D-558-2, X-1E. Propellants: Lox/Alcohol. Agency: Reaction Motors.

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