Engine Model: RD-0144. Manufacturer Name: RD-0144. Designer: Kosberg. Developed in: 1998-. Application: upper stage. Propellants: Lox/LNG. Thrust(vac): 147.000 kN (33,046 lbf). Isp: 374 sec. Mass Engine: 250 kg (550 lb). Length: 1.20 m (3.92 ft). Chambers: 1. Thrust to Weight Ratio: 60.00. Country: Russia. Status: Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Radiation cooled nozzle extension.
Bibliography:- Novosti kosmonavtiki, Issue 3, 1999.