KTDU-417-B
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev N2O4/UDMH rocket engine. Luna 15-24 used this low thrust engine in system KTDU-417 for soft-landing on the moon. Out of Production. Pressure-fed engine; could be throttled to 2.06 kN.
See entry KTDU-417.
Chambers: 2. Throttled thrust(vac): 2.060 kN (463 lbf). Chamber Pressure: 8.90 bar. Oxidizer to Fuel Ratio: 2.4.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Agency
- Isayev bureau