RD-0141

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RD-0141

Part of RD-0120

Kosberg LOx/LNG rocket engine. stage 1. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Obviously variant of RD-0141 with larger nozzle.

Status: Developed 1998-on. Date: 1998-. Thrust: 2,251.00 kN (506,044 lbf). Unfuelled mass: 1,973 kg (4,349 lb). Specific impulse: 353 s. Specific impulse sea level: 323 s. Height: 3.35 m (10.99 ft).

Engine: 1,973 kg (4,349 lb). Thrust to Weight Ratio: 116.32.

Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau. Bibliography: 403.

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