The LK (Russian: ЛК, from Russian: Лунный корабль, romanized: Lunniy korabyl, lit. 'lunar craft'; GRAU index: 11F94) was a lunar module (lunar lander designed for human spaceflight) developed in the 1960s as a part of several Soviet crewed lunar programs. Its role was analogous to the American Apollo Lunar Module (LM).

2011年3月18日 · During the 1960s, the Lunar Spacecraft, in Russian "Lunnyi Korabl" or LK, was conceived as a part of the L3 lunar expeditionary complex to be carried aloft by the N1 rocket. From the outset, Soviet designers understood that despite being the largest launch vehicle developed by the USSR, it could only carry two-person crew on a lunar mission and ...

Chelomei proposed his own spacecraft designated LK, which could be launched on a mission around the Moon by a single UR-500 rocket. The launch vehicle was also identified within the industry as 8K82K. Thus, the project of Chelomei's circumlunar mission received the index 8K82K-LK. The development of the LK spacecraft

Practically immediately after the Soviet Union sent the first cosmonaut into orbit, the Moon became the destination for human space flight. In May 1961, President Kennedy proclaimed the lunar landing on the surface of the Moon before 1970, as the main goal for NASA. However, the Soviet government was slow to respond to the US challenge.

The LK ('Lunniy korabl' - lunar craft) was the Soviet lunar lander - the Russian counterpart of the American LM Lunar Module. Manned Lunar lander test satellite, Russia. Launched 1970 - 1971. AKA: 11F94;T2K. Status: Operational 1970. First Launch: 1970-11-24. Last Launch: 1971-08-12. Number: 3 . Thrust: 20.10 kN (4,519 lbf).

LK-700 was a Soviet direct ascent lunar lander program proposed in 1964. [1] It was developed by Vladimir Chelomey as an alternative to the N1-L3 program. It was also a further development of the LK-1 lunar flyby spacecraft.

2023年1月14日 · LK (Lunnyi Korabl) was the soviet crewed lunar lander. It had only space for one cosmonaut, which had to enter the LK by EVA. It was a one stage design, with the same stage providing landing and lift off operation. At lunar lift off, the landing gear was discarded. The propulsion consisted of 2 independent punp-fed engined.

The L3 complex itself, with a total mass of 95 metric tons, would consist of a fourth stage (Block G) for the N1 to take the L3 from low earth orbit to trans-lunar trajectory; a lunar orbiter with a Soyuz re-entry capsule for return to earth (LOK); a lunar lander (LK) for the landing of a single cosmonaut on the surface of the moon; and a ...

The LK-1 was the spacecraft designed by Chelomei for the original Soviet manned lunar flyby project. The re-entry vehicle and propulsion systems would continue in development for the LK-700 lunar lander and TKS space station resupply vehicle.

The LK ("Lunniy korabl" - lunar craft) was the Soviet lunar lander - the Russian counterpart of the American LM Lunar Module. The LK was to have landed a Soviet citizen on the moon before the Americans, winning the moon race. This was not to be, for various reasons.