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      LK-1 was a projected Soviet crewed lunar flyby spacecraft. It would be launched on a three-stage Proton launch vehicle. The project started in 1962 under the lead engineer Vladimir Chelomey, with the first flight planned for 1967.
      The LK-1 had its origin in several early 1960s spacecraft projects under the generic names of kosmoplans and raketoplans.
      In 1965 the project was cancelled in favour of the Soyuz 7K-L1 spacecraft.
      Further developments came as the LK-700 direct-descent lunar lander program.


      Configuration



      The spacecraft consisted of the following modules:

      ADU Emergency Engine Unit
      VA Capsule (crew module)
      PAB Equipment-Rocket System Block (service module)
      RB Translunar Injection Stage


      Characteristics


      Crew Size: 2
      Spacecraft delta v: 3,300 m/s
      Electric System: 2.00 average kW.
      Gross mass: 17,000 kg
      Un-fuelled mass: 4,000 kg
      Height: 5.20 m
      Span: 7.27 m


      External links


      Encyclopedia Astronautica:
      LK-1, with an image of an assembled translunar spacecraft


      References

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