RD-0126E
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/LH2 rocket engine. Upper stages. Design concept 1998-. Concept for a cryogenic engine for upper stages. Single annular chamber with straight expansion nozzle, common turbopump.
Engine: 234 kg (515 lb). Chamber Pressure: 70.00 bar.
Related
- Country
- Russia
- Propellants
- Lox/LH2
- Agency
- Kosberg bureau