RD-0229M
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg LOx/LNG rocket engine. Vozdushnyy Start stage 1. Developed 1997. Derivative of RD-0229 for the propellants LOX and liquid natural gas (methane). Initial candidate for stage 1 propulsion of Vozdushnyy Start project by Kompomash.
Related
- Country
- Russia
- Propellants
- Lox/LNG
- Agency
- Kosberg bureau