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The longest serving manned spacecraft in the world, the Soyuz was originally conceived in Sergei Korolev's OKB-1 design bureau for the Soviet effort to explore the Moon at the beginning of the 1960s. However, long after the Moon race was over, the Soyuz continued ferrying Russian crews to the Salyut and Almaz orbital stations, as well as it performed several solo flights and the historic docking with the US Apollo spacecraft in 1975. The origin of the Soyuz spacecraft Unlike one-man Vostok spacecraft, the three-seat Soyuz would be able to conduct active maneuvering, orbital rendezvous and docking. These features were all necessary for a flight around the Moon and for lunar expedition itself. In the early scenario of "circumlunar" flight, the Soyuz would be actually a three-part spacecraft assembled in the low-Earth orbit from components delivered by separate launch vehicles. The 7K spacecraft would carry the crew, while the 9K propulsion stage would be fueled by 11K tankers. The 7K crew vehicle was to be equipped with the S5.35 propulsion system, while S5.36 and S3.37 engines would propel the 9K and 11K vehicles. This plan was later abandoned in favor of a two-launch and, later, one-launch scenario of the circumlunar mission. For the expedition to the lunar surface, Korolev's bureau adopted the plan similar to one used in the Apollo program: a mother spacecraft and a lander would separate in the lunar orbit and the lander would deliver an "expedition" to the surface. The lander would then blast off from the Moon, enter lunar orbit, where it would meet and dock with the mother spacecraft. In this plan, a two-seat Soyuz would play a role of the "mother ship." An "abbreviated" version of the Soyuz spacecraft, designated L1, was developed for the circumlunar flight onboard the Proton rocket. Commonly known as Zond, the L1 spacecraft was essentially Soyuz, where its habitation module was replaced with a smaller instrumentation package. One more variation of Soyuz was also under development in the mid-1960 specifically for the missions in Earth orbit. Designated 7K-OK, it would be used for "rehearsals" of rendezvous operations necessary for the lunar expedition. The early flights In the competitive atmosphere of the Moon Race, the first test flights of the Soyuz were hastily conducted in 1966 with mixed results. Despite earlier problems, Vladimir Komarov blasted off onboard Soyuz-1 on April 23, 1967, for an ambitious mission, calling for orbital rendezvous and docking with the second Soyuz scheduled to follow Soyuz-1. The problems onboard Soyuz-1 forced to cancel the second mission, while Soyuz-1 flight itself ended in a disaster during landing. The problems with the parachute deployment caused the Soyuz-1 reentry capsule hit the ground with a crashing speed, killing Komarov. In the wake of the catastrophe, a series of unmanned missions followed, during which two pairs of vehicles docked in orbit automatically. The manned missions resumed in October 1968. The Soyuz for the station As financial and technical problems held the USSR behind the US in the Moon Race, the leaders of the Soviet space industry had to look for a new direction in the manned space program. Since the end of 1960, the new version of the Soyuz spacecraft emerged, which would transport the crews to the Earth-orbiting space laboratories. In 1971, a three-seat Soyuz delivered the first crew to the original Salyut space station. But a new disaster hit when the first Salyut crew returned from orbit. The sudden depressurization of the reentry capsule killed three cosmonauts onboard. As a result of the tragedy, the designers introduced a protective pressure suits at the expense of one crew seat. Two-seat variants of Soyuz 7K-T spacecraft then continued ferrying crews to Salyut and Almaz space stations. At the TsKBEM design bureau in Podlipki (later Korolev), E.P. Vyatkin was appointed the lead engineer on the Soyuz spacecraft in 1974. He was replaced by V.P. Guzenko in 1976. In the same year, Design Department No. 174, led by L.I. Dulnev, took over all the work on Soyuz. (52) The Soyuz T and TM versions The Soyuz T version of the spacecraft flew its first piloted mission in 1980, and since 1986 the Soyuz TM modification of the spacecraft has been delivering crews to the Mir space station. The modifications featured multiple improvements in the design, including the introduction of the new weight-saving computerized flight-control system and improved emergency escape system. These upgrades allowed to increase the crew to three, while the crewmembers could be still protected with pressure suits. RKK Energia also developed another version of the spacecraft, known as Soyuz TMA, or "anthropometric," to address the issues raised during US-Russian cooperative program. "Anthropometric" upgrades would remove the limitations for the height of the crewmembers onboard the Soyuz and as a result, would allow using the TMA version as a "lifeboat" for the International Space Station. The production of the TMA spacecraft, however, was stalled by non-payments by the Russian government to the RKK Energia at the end of the 1990s. Ironically, NASA, which originally ordered the upgrades also refused to pay for the development of the TMA, until Russia insured the production of the spacecraft. The overview of the Soyuz variants:
SOYUZ MISSION DETAILS: Moon Race era (1966-1970): Soyuz-1 - Soyuz-9
Salyut era (1971-1985): Soyuz-10 - Soyuz T-14
Mir era (1986-2000): Soyuz T-15 - Soyuz TM-30 International Space Station era (2000-present): from Soyuz TM-31
Soyuz TMA series:
PROPOSALS FOR RADICAL SOYUZ UPGRADES:
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