17D58E
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 used in Briz, Briz-M upper stage propulsion system S5.98M.
Minimum impulse 0.068 kg-s. Specific impulse also reported as 270 sec.
Oxidizer to Fuel Ratio: 2.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Rokot, Proton/Briz K/M, Proton-M/Briz-M
- Propellants
- N2O4/UDMH
- Stages
- Proton KM-4 Briz M, Rokot-3 Briz
- Agency
- Isayev bureau