Soyuz-U

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Soyuz-U (Soyuz-U/Ikar; Soyuz-U/Fregat)
The Soyuz TMA-3 vehicle launches from the Baikonur Cosmodrome in Kazakhstan October 18, 2003
The Soyuz TMA-3 vehicle launches from the Baikonur Cosmodrome in Kazakhstan October 18, 2003
Function Orbital carrier rocket
Manufacturer TsSKB-Progress
Country of origin Soviet Union (Russia)
Size
Height 51.1 m for Soyuz-U; 47.3 m for Soyuz-U/Ikar and 46.7 m for Soyuz-U/Fregat
Diameter 3 m [1]
Mass 313,000 kg (Soyuz-U); 308,000 kg (Soyuz-U/Ikar and Soyuz-U/Fregat)
Stages 2 (Soyuz-U) or 3 (Soyuz-U/Ikar and Soyuz-U/Fregat)
Capacity
Payload to LEO 6,900 kg from Baikonur and 6,700 kg from Plesetsk
Associated rockets
Family R-7 (Soyuz)
Derivatives Soyuz-U2
Soyuz-FG
Launch history
Status Active
Launch sites LC-1 & LC-31, Baikonur
LC-16 & LC-43, Plesetsk
Total launches 745
Successes 724
Failures 21
Maiden flight 18 May 1973[2]
Notable payloads Soyuz spacecraft
Progress spacecraft

The Soyuz-U launch vehicle (LV) is an improved version of the original Soyuz LV. Soyuz-U is part of the R-7 family of rockets based on the R-7 Semyorka missile. Members of this rocket family were designed by the TsSKB design bureau and constructed at the Progress Factory in Samara, Russia. (These two are now a united company, TsSKB-Progress). The first Soyuz-U flight took place on 18 May 1973, carrying as its payload Kosmos 559, a Zenit military surveillance satellite.[2]

The Soyuz-U vehicle replaced earlier Soyuz launch vehicle variants and the Voskhod rocket, all of which were closely related vehicles derived from the Soviet R-7 ICBM. The Soyuz-U is a unified, single vehicle capable of launching manned and unmanned payloads.

Soyuz-U is still in use today, making several launches a year.

Contents

[edit] Versions

There are two versions of Soyuz-U in current use, Soyuz-U/Ikar and Soyuz-U/Fregat.

Soyuz-U/Ikar uses Ikar as its 3rd stage, produced by the Progress State Research and Production Rocket Space Center, TsSKB-Progress. Ikar is used to deliver various payloads with masses of 750 kg to 3920 kg to heights 250 km to 1400 km. Ikar's performance is lower than that of Fregat, but it is more precise in maneuvering and it can operate autonomously longer.

Soyuz-U/Fregat uses Fregat as its 3rd stage, developed and produced by Lavochkin Association in Khimki.

An older variant of Soyuz-U, the Soyuz-U2 launcher, had the same hardware as the basic Soyuz-U. Instead of normal kerosene it used a high energy, synthetic kerosene, Syntin, as the first stage fuel. This variant last flew in 1996, after production of Syntin ended.

Soyuz-U was the basic platform for the development of the Soyuz-FG launch vehicle, which uses an all-new first stage.

In the future both Soyuz-U and Soyuz-FG will be replaced by the Soyuz-2 launch vehicle.

[edit] Launches of human spaceflight missions

The first use of a Soyuz-U to launch a human spaceflight mission took place 2 December 1974, when the Soyuz 16 crew was launched in preparation for the Apollo-Soyuz Test Project (ASTP). Soyuz 19, which as part of the ASTP docked with the last Apollo spacecraft ever flown, was also launched by a Soyuz-U rocket.[2]

On 6 July 1976 a Soyuz-U launched Soyuz 21, which took a crew of two to the Salyut 5 space station. Many subsequent space station crews were launched on Soyuz-U launchers. The final human spaceflight mission to utilize the Soyuz-U was Soyuz TM-34, a Soyuz ferry flight to the International Space Station.

[edit] Recent missions

Lately Soyuz-U vehicles have been used by the Russian Federal Space Agency mostly with Progress-M robotic cargo spacecraft to resupply the International Space Station (ISS).

The most recent Soyuz-U mission failed to launch Progress M-12M to the ISS on 24 August 2011.

Its most recent non-Progress launch was on 16 April 2010, when a Soyuz-U was used to carry the Kosmos 2462 spacecraft to orbit. As of August 2011, a total of 745 Soyuz-U launch vehicles were launched[3], with 21 launch failures and 724 successes (2.8% failure rate).[citation needed][4]

[edit] References

[edit] External links

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