11D458
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev N2O4/UDMH rocket engine. In Production. Small attitude control thruster in Briz upper stage propulsion system S5.98M. Total summary impulse 14,112 kg-s. Minimum impulse 4 kg-s. Specific impulse also reported as 275 sec. Oxidizer to Fuel Ratio: 2.0.
Subtopics
- Isayev TKS attitude Isayev N2O4/UDMH rocket engine. TKS, Almaz. In Production.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- Proton KM-4 Briz M, Rokot-3 Briz
- Agency
- Isayev bureau
- Bibliography
- 409