Designer Sergei Korolev Operator Soviet space program Launch mass 9,850 kg Regime Low Earth orbit | Country of origin Soviet Union Crew capacity 2 Manufacturer OKB Derived from Soyuz 7K-OK | |
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Applications Manned cislunar flight and lunar orbit Dimensions 10.06 meters (33.0 ft) length
2.93 meters (9.6 ft) diameter Similar Soyuz 7K‑OK, Soyuz 7K‑L1, Soyuz 7K‑OKS, Soyuz 7K‑T, Soyuz 7K‑L1 No4L | ||
Buzz aldrin s space program manager soyuz 7k lok lunar landing
The Soyuz 7K-LOK, or simply LOK (Russian: Lunniy Orbitalny Korabl meaning "Lunar Orbital Craft") was a Soviet manned spacecraft designed to launch men from Earth to circle the moon and developed in parallel to the 7K-L1. The LOK would carry two cosmonauts into orbit around the Moon, acting as "mother" spacecraft for the LK Lander, which would land one member of the crew to the surface. It was part of the N1-L3 programme which also included the LK lander and the N1 rocket.
Contents
Design
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 the Apollo (spacecraft), thus forcing the cosmonaut to make a spacewalk from the 7K-LOK's orbital module to the LK Lander using the new Krechet space suit (the predecessor to the Orlan space suits used today on the International Space Station).
Another change to the 7K-LOK was the elimination of the solar panels used on the 7K-OK, replacing them with fuel cells similar to those found on the Apollo CSM. Another feature, 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.
The information 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.
Flights
Only three unmanned 7K-LOK's were flown in the short lifespan of the failed Soviet lunar program.
One of them was a dummy 7K-LOK as a Soyuz 7K-L1E modification of a Soyuz 7K-L1 "Zond" spacecraft and was successfully test launched into Low Earth orbit on a Proton rocket designated as Kosmos 382 (Soyuz 7K-L1E No.2) on December 2, 1970. Two other unsuccessful launches of dummy 7K-LOK (Soyuz 7K-L1E No.1) and operational (Soyuz 7K-LOK No.1) with dummy LKs were fulfilled atop the N-1 rocket in its later flights on June 26, 1971 and November 23, 1972 intended for lunar flybys. Both spacecraft were pulled and saved by the launch escape system when those boosters failed. The two aborted flights later proved that the launch-escape system worked when a similar problem on a Soyuz-U forced the Soyuz T-10a to be jettisoned with its cosmonaut crew in 1983 before the booster exploded on the launchpad, destroying it. On two early flights of the N-1, both of them failures, another Soyuz 7K-L1S "Zond-M" modification of the 7K-L1 spacecraft instead of the 7K-LOK or 7K-L1E were used without the dummy LK, and they, along with the booster, were destroyed.
Subsequently, a complete L3 lunar expedition complex with an operational 7K-LOK and LK for an unmanned lunar flyby and landing mission (in preparation of a future manned scenario) was prepared for the fifth launch of a modified N1 rocket in August 1974. The N1-L3 program was cancelled in May 1974 and the Soviets decided to concentrate on the development of space stations, achieving several firsts in the process.
Future
Although never flown, the planned — and discontinued — joint Russian/ESA ACTS missions to the Moon, planned as a response to NASA's Project Constellation, would have seen the resurrection, somewhat, of the 7K-LOK spacecraft, but with the current Soyuz TMA hardware (solar panels, docking & transfer system, etc.) being used.