![]() ![]() ![]() Module consisted off following major elements: In 1965, the development of the landing mechanism was subcontracted to KB Arsenal. ( 231) It would be likely deployed immediately after the jettisoning of the protective shroud in preparation for landing in the lunar orbit. In its launch configuration, the stowed landing gear would have a span of 2.26 meters. In turn, LPA consisted of a lattice-structured main body with a diameter of 2.27 meters and a four-legged lunar landing device, ( Lunnoe Posadochnoe Ustroistvo, LPU). However, structurally, the spacecraft would be subdivided into the Lunar Landing Aggregate, ( Lunnyi Posadochnyi Agregat, LPA) and the Lunar Ascent Vehicle, ( Lunnyi Vzletnyi Apparat, LVA). The LK spacecraft consisted of the lunar module itself and the Block E propulsion Block D would jettison and crash onto the lunar surface, after which Block E's engine would take over.Ī full-scale prototype of the LK lander used for training shows a possible early configuration of the spacecraft. ![]() The initial descent to the Moon would be propelled by the Block D stage attached to LK. Also unlike in Apollo, the same propulsion unit of the Block E would be used for the final phase of the descent on the lunar surface and for a takeoff. However, unlike in Apollo, no internal tunnel between LOK and LK existed, therefore back-and-forth movement of a crew member between two ships would have to be done in spacesuit, via the same hatch in LK, which would be used to walk on the lunar surface. The LK and depart toward Earth onboard the LOK. Following the moonwalker's transfer back from LK to LOK, both cosmonauts would jettison The Moon onboard LK and link up with LOK. Similar to the American Apollo missions, LK was designed to separate from a lunar orbital spacecraft (LOK),Ī descent to the lunar surface and, hopefully, a successful "moonwalk," the cosmonaut would blast off from ![]()
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