- Source: LK-1
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
Kata Kunci Pencarian:
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6.745
8.1
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7.2
6.494
6.013
8.383
7.045
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