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astronautix.com RD-0110MD


Manufacturer Name: RD-0110MD. Designer: Kosberg. Developed in: 1994-. Propellants: Lox/LNG Thrust(vac): 25,000 kgf. Thrust(vac): 245.00 kN. Burn time: 20 sec. Chambers: 4. Chamber Pressure: 54.00 bar. Area Ratio: 82.20. Country: Russia. Status: Developed 1994-on. References: 403 . Comments: Prototype engine for tests with propellants LOX/liquified natural gas. Tests performed from 30 April 1998 on, test duration 20s.
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Last update 12 March 2001.
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