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LK-700 Block 11
Russian manned spacecraft module. Study 1968. Differed from the lateral Block 1 stages in having an engine unit for orientation of the assembly. Main engine of 23,500 kgf and three engines for soft landing / midcourse maneuvers of 1,670 kgf each. Midcourse man oeuvre/lunar braking stage.

AKA: Block 11. Status: Study 1968. Thrust: 279.58 kN (62,852 lbf). Gross mass: 32,226 kg (71,046 lb). Specific impulse: 326 s.

Spacecraft delta v: 3,000 m/s (9,800 ft/sec).



Family: Manned spacecraft module. Country: Russia. Spacecraft: LK-700. Propellants: N2O4/UDMH.

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