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Manufacturer Name: RD-0142. Designer: Kosberg. Developed in: 1998-. Application: stage 2. Propellants: Lox/LNG Thrust(vac): 239,900 kgf. Thrust(vac): 2,353.00 kN. Isp: 369 sec. Mass Engine: 2,058 kg. Length: 4.5 m. Chambers: 1. Country: Russia. Status: Developed 1998-on. References: 403 . Comments: Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Obviously variant of RD-0141 with larger nozzle.
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Last update 12 March 2001.
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