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
LR39
Reaction Motors LOx/Alcohol rocket engine. Small experimental engine. Single thrust chamber, water cooled, equipped only with spark plug ignition system and propellant flow valves. Test article only built.

AKA: D-50G1;XLR39-RM-1. Thrust: 225 N (50 lbf). Unfuelled mass: 0.66 kg (1.45 lb). Height: 0.22 m (0.73 ft). Diameter: 0.0380 m (0.1240 ft).

Engine: 0.66 kg (1.45 lb). Chamber Pressure: 16.70 bar. Propellant Formulation: Lox/Alcohol+Water mixture with .86 specific gravity. Thrust to Weight Ratio: 34.84.

Country: USA. Propellants: Lox/Alcohol. Agency: Reaction Motors.
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