RD-0110MD
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg LOx/LNG rocket engine. Developed 1994-on. Prototype engine for tests with propellants LOX/liquefied natural gas. Tests performed from 30 April 1998 on, test duration 20s.
Chambers: 4. Chamber Pressure: 54.00 bar. Area Ratio: 82.2.
Related
- Country
- Russia
- Propellants
- Lox/LNG
- Agency
- Kosberg bureau