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Lunokhod LEK
Part of L5
Lunokhod LEK
Lunokhod LEK
Credit: © Mark Wade
Russian manned lunar rover. Study 1973. Lunar rover for the Vulkan Lunar Expedition. The rover provided pressurized quarters for 2 crew, allowing trips up to 200 km from the lunar base at a top speed of 5 km/hr.

AKA: Manned Vulkan-launched version. Status: Study 1973. Gross mass: 8,200 kg (18,000 lb). Height: 8.00 m (26.20 ft).

The 2.25 metric ton generating station provided 8 kW of solar power to run the motor. Each 12 day trip would use 200 kg of life support consumables.

Crew Size: 2. Habitable Volume: 25.00 m3. Electric System: 8.00 average kW.



Family: Lunar Rovers, Moon. Country: Russia. Spacecraft: LEK Lunar Expeditionary Complex. Launch Vehicles: Energia, Vulkan. Agency: Korolev bureau. Bibliography: 367, 89.
Photo Gallery

Soviet Lunar LandersSoviet Lunar Landers
Landing stages for Soviet lunar expeditions. Top row, left to right: L3 original version; LK; LK-3; LK-700; two versions of the L3M; LEK for Energia-launched lunar landing. Bottom row, lunar base elements: Chelomei KLE; Chelomei Heavy Lunokhod; Barmin DLB base module; LZM, LZhM, Lunokhod, and LEK for Glushko LEK Vulkan-launched lunar base.
Credit: © Mark Wade


Lunokhod DLBLunokhod DLB
Credit: © Mark Wade


Lunokhod LEKLunokhod LEK
Credit: © Mark Wade



1975 January 1 - .
1977 December 1 - . Launch Vehicle: N1.
1978 January 1 - .

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