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RD-0149
Kosberg LOx/LNG rocket engine. upper stage. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Variant of RD-0141 with larger nozzle.

AKA: RD-0134. Status: Developed 1998-on. Date: 1998-. Thrust: 49.00 kN (11,015 lbf). Unfuelled mass: 150 kg (330 lb). Specific impulse: 370 s. Height: 1.58 m (5.17 ft).

Engine: 150 kg (330 lb). Thrust to Weight Ratio: 33.33.

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