RD-0214
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/UDMH rocket engine. Proton stage 3 vernier. In Production. Based on RD-0207. Four used as steering engines for Proton Stage 3 in system RD-0212. First flight 1967.
Chambers: 4. Chamber Pressure: 53.00 bar.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- Proton K-3
- Agency
- Kosberg bureau