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Manufacturer Name: RD-0140. Designer: Kosberg. Developed in: 1998-. Application: stage 2. Propellants: Lox/LNG Thrust(vac): 212,700 kgf. Thrust(vac): 2,086.00 kN. Isp: 349 sec. Isp (sea level): 300 sec. Mass Engine: 1,689 kg. Length: 5.0 m. Chambers: 1. Country: Russia. Status: Developed 1998-on. References: 403 . Comments: Proposed engine for LOX/liquid natural gas. Gas generator cycle with turbine gas injection into supersonic nozzle.
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Last update 12 March 2001.
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