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Engine Model: RD-0142. Manufacturer Name: RD-0142. Designer: Kosberg. Developed in: 1998-. Application: stage 2. Propellants: Lox/LNG. Thrust(vac): 2,353.000 kN (528,975 lbf). Isp: 369 sec. Mass Engine: 2,058 kg (4,537 lb). Length: 4.51 m (14.79 ft). Chambers: 1. Thrust to Weight Ratio: 116.56. Country: Russia. Status: Developed 1998-on.

Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Obviously variant of RD-0141 with larger nozzle.

Bibliography:

  • Novosti kosmonavtiki, Issue 3, 1999.
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