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RD-0144
Kosberg LOx/LNG rocket engine. upper stage. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Radiation cooled nozzle extension.

Status: Developed 1998-on. Date: 1998-. Thrust: 147.00 kN (33,046 lbf). Unfuelled mass: 250 kg (550 lb). Specific impulse: 374 s. Height: 1.20 m (3.92 ft).

Engine: 250 kg (550 lb). Thrust to Weight Ratio: 60.

Subtopics
RD-0145 Kosberg LOx/LNG rocket engine. upper stage. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle. Four-chamber variant of RD-0144.
Country: Russia. Propellants: Lox/LNG. Agency: Kosberg bureau. Bibliography: 403.
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