RD-0216
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-100 stage 1. Staged combustion cycle. Includes tank pressurization system (RD-0217 without tank press.). First launch November 1963, manufactured until 1974, operational until 1991. First flight 1965.
Chamber Pressure: 147.00 bar.
Subtopics
- RD-0217 Kosberg N2O4/UDMH rocket engine. UR-100, UR-100K stage 1. Out of Production. Staged combustion cycle. Version of RD-0216 without tank pressurization system. Manufacturing until 1974, operational use until 1991.
RD-0235 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.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Taran, UR-100M SLBM, UR-100, UR-100M
- Propellants
- N2O4/UDMH
- Stages
- 8S816
- Agency
- Kosberg bureau