RD-0235
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg N2O4/UDMH rocket engine. UR-100N / RS-18 (SS-19) stage 2. Main engine based on RD-0217 with larger nozzle for altitude operation. Staged combustion cycle. First flight 1972.
Chamber Pressure: 175.00 bar.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- UR-100N Stage 2N
- Agency
- Kosberg bureau