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11D416
Isayev N2O4/UDMH rocket engine. Study 1968. Three of these engines used for midcourse corrections and soft lunar landing in Block 11 and Block 1V stages of LK-700 manned spacecraft.

Status: Study 1968. Thrust: 16.40 kN (3,687 lbf).



Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Agency: Isayev bureau. Bibliography: 443.

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