RD-0154
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Kosberg bureau
- Bibliography
- 4484