11D121
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Korolev GOX/Kerosene rocket engine. N-1 stage 1 (block A) roll control engine. Developed 1969-74. Gimbaling +/- 45 degree. Propellants are fed from main engine (NK-15, NK-33) turbopumps. Chamber Pressure: 71.60 bar.
Related
- Country
- Russia
- Launch Vehicles
- N1F
- Propellants
- GOX/Kerosene
- Stages
- N1F Block A
- Agency
- Korolev bureau