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LOK Energia PAO
Russian manned spacecraft module. Study 1988. The LOK provided a pressurized volume for three crew. Within the cabin was a descent module of the same configuration as Soyuz, but almost 50% larger. Equipment-engine section - Lunar orbit maneuver, trans-orbit propulsion, pressurized crew quarters.

AKA: Priborno-agregatniy otsek. Status: Study 1988. Gross mass: 23,200 kg (51,100 lb). Unfuelled mass: 6,100 kg (13,400 lb). Height: 3.50 m (11.40 ft). Diameter: 4.10 m (13.40 ft).

This would separate just prior to reentry in the earth's atmosphere. Forward was a universal docking system.



Family: Manned spacecraft module. Country: Russia. Spacecraft: LOK Energia. Propellants: N2O4/UDMH.

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