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11D458
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.

Status: In Production. Thrust: 392 N (88 lbf). Specific impulse: 252 s. Burn time: 3,200 s.

Subtopics
Isayev TKS attitude Isayev N2O4/UDMH rocket engine. TKS, Almaz. In Production.
Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Proton KM-4 Briz M, Rokot-3 Briz. Agency: Isayev bureau. Bibliography: 409.
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