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Manufacturer Name: RD-0144. Designer: Kosberg. Developed in: 1998-. Application: upper stage. Propellants: Lox/LNG Thrust(vac): 15,000 kgf. Thrust(vac): 147.00 kN. Isp: 374 sec. Mass Engine: 250 kg. Length: 1.2 m. Chambers: 1. Country: Russia. Status: Developed 1998-on. References: 403 . Comments: Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Radiation cooled nozzle extension.
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Last update 12 March 2001.
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