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11D445
Melnikov N2O4/UDMH rocket engine. In Production. Propulsion system of the Yantar-2K military satellite descent capsule. Up to 10,000 ignitions. Thrust from 0,065 - 0,012 kN.

Status: In Production. Thrust: 65 N (14 lbf). Burn time: 900 s.



Subtopics

11D446 Melnikov N2O4/UDMH rocket engine. Part of the Yantar-2K spy satellite orbital propulsion system. In production. The orbital maneuvering system of the Yantar-2K consisted of one 11D430, four 11D431, four 11D446, and eight 11D428. Up to 40,000 ignitions.

Family: Storable liquid. People: Melnikov. Country: Russia. Propellants: N2O4/UDMH. Bibliography: 69.

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