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.
Status: Developed 1994-on. Date: 1994-. Thrust: 245.00 kN (55,078 lbf). Burn time: 20 s.
Chambers: 4. Chamber Pressure: 54.00 bar. Area Ratio: 82.2.