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11D23
Kosberg N2O4/UDMH rocket engine. Study 1968. Engine used in Block 1 and Block 11 stages of LK-700 manned lunar lander.

Status: Study 1968. Thrust: 230.50 kN (51,818 lbf).



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

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