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17D58E
Part of DST engine series Family
Isayev N2O4/UDMH rocket engine. In Production. Small attitude control thruster used in Briz, Briz-M upper stage propulsion system S5.98M.

Status: In Production. Thrust: 13 N (3 lbf). Specific impulse: 247 s. Burn time: 3,200 s.

Minimum impulse 0.068 kg-s. Specific impulse also reported as 270 sec.

Oxidizer to Fuel Ratio: 2.



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. Bibliography: 293, 409.

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