LR39
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Country
- USA
- Propellants
- Lox/Alcohol
- Agency
- Reaction Motors