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RD-0134
Part of RD-0120 Family
Kosberg LOx/LNG rocket engine. stage 1. Developed 1998-on. Proposed engine for LOX/liquid natural gas. Staged combustion cycle variant of RD-0139.

Status: Developed 1998-on. Date: 1998-. Thrust: 2,038.00 kN (458,160 lbf). Unfuelled mass: 1,800 kg (3,900 lb). Specific impulse: 358 s. Specific impulse sea level: 316 s. Height: 3.50 m (11.40 ft).

Engine: 1,800 kg (3,900 lb). Thrust to Weight Ratio: 115.44.



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

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