Lunniy Orbitalny Korabl drawing | |
| Manufacturer | OKB-1 |
|---|---|
| Designer | Sergei Korolev |
| Country of origin | Soviet Union |
| Operator | Soviet space program |
| Applications | Crewedcislunar flight andlunar orbit |
| Specifications | |
| Launch mass | 9,850 kilograms (21,720 lb) |
| Crew capacity | 2 |
| Dimensions | 10.06 meters (33.0 ft) length 2.93 meters (9.6 ft) diameter |
| Regime | Low Earth orbit Cislunar space Lunar orbit |
| Production | |
| Status | Canceled |
| Built | 6 |
| Launched | 5 |
| Failed | 4 |
| Maiden launch | December 2, 1970 |
| Last launch | November 23, 1972 |
| Related spacecraft | |
| Derived from | Soyuz 7K-OK |
| Derivatives | Soyuz 7K-L1 lunar flyby Soyuz 7K-OKS space station shuttle |
| Flown with | LK lander |

TheSoyuz 7K-LOK, or simplyLOK (Russian:Лунный Орбитальный Корабль,romanized: Lunniy Orbitalny Korabl meaning "Lunar Orbital Craft") was aSovietcrewed spacecraft designed to take humans from Earth to orbit the Moon, developed in parallel to the7K-L1. The LOK would carry two cosmonauts, acting as amother ship for theLK lander which would land one crew member to the surface. It was part of theN1-L3 programme which also included the LK lander and theN1 rocket.[1]
Like the 7K-OK model, the 7K-LOK was divided into three sections, an ellipsoid Orbital Module, the "headlight"-shaped Descent Module, and a cylindrical equipment module. Like the 7K-OK, the 7K-LOK was capable of physically docking with another spacecraft, but lacked the transfer tunnel used on theApollo (spacecraft), thus forcing the cosmonaut to make aspacewalk from the 7K-LOK's orbital module to the LK Lander using the newKrechet space suit (the predecessor to theOrlan space suits used today on theInternational Space Station).
Another change to the 7K-LOK was the elimination of the solar panels used on the 7K-OK, replacing them withfuel cells similar to those found on the Apollo CSM. Additionally, a "cupola" located on the Orbital Module, allowed the cosmonaut in the 7K-LOK to perform the docking procedure with the LK Lander after lunar liftoff. Only the Descent Module from the 7K-L1, with a thicker, reinforced heatshield, is used on the 7K-LOK and like the 7K-L1, is capable of doing a "skip reentry" so that the Soyuz could be recovered in the Soviet Union.
Theinformation display systems (IDS) on the LOK were different from those of the Soyuz-7K. The Descent Module was equipped with the "Uran" control panel and the Orbital Module featured the "Orion" approach control panel.
Only three uncrewed 7K-LOKs were flown in the short lifespan of thefailed Soviet lunar program.