RD-0149

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

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.

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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