RD-58Z
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Aft view of the Block D lunar crasher stage and its 11D68 engine. The Block D would have taken the LK lunar lander to near the surface of the moon. This stage remains in use today atop the Proton rocket.
Credit: © Mark Wade
Kosberg Lox/Kerosene rocket engine. Zenit stage 3. Developed 1981-1990.
Engine: 300 kg (660 lb). Chamber Pressure: 78.00 bar. Area Ratio: 189. Thrust to Weight Ratio: 24.13.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Stages
- Zenit-V
- Agency
- Korolev bureau