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RD-0154


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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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