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RD-0154
RD-0154
RD-0154
Credit: KBKhA
Kosberg LOx/Kerosene rocket engine. Design concept 2007. Engine proposed to replace RD-110 in Avrora improved version of Soyuz launch vehicle. The single chamber engine had a deployable nozzle extension for improved vacuum specific impulse.

Status: Design concept 2007. Date: 1998-. Thrust: 294.30 kN (66,161 lbf). Specific impulse: 363 s. Specific impulse sea level: 363 s.

Engine: 536 kg (1,181 lb). Chamber Pressure: 155.00 bar.



Subtopics

RD-0143A Kosberg LOx/LNG rocket engine. Vozdushnyy Start stage 1. Design concept 1998-. Proposed single chamber variant of RD-0143. Selected for stage 1 of Vozdushnyy Start project by Kompomash.

Country: Russia. Propellants: Lox/Kerosene. Agency: Kosberg bureau. Bibliography: 4484.

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