Soyuz-U: Difference between revisions

Soyuz-U
	A Soyuz-U on the launchpad in 1975 for the Apollo-Soyuz mission
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
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)
Derivative work	Soyuz-U2; Soyuz-FG
Launch history
Status	Active
Launch sites	Baikonur Sites 1/5 & 31/6; Plesetsk Sites 16/2, 41/1, 43/3 & 43/4;
Total launches	785
Success(es)	764
Failure(s)	22
First flight	18 May 1973
Last flight	1 December 2016 (Progress MS-04)
Type of passengers/cargo	Soyuz spacecraft; Progress spacecraft
Boosters – Blok-B,V,G,D
No. boosters	4
Height	19.6 m (64 ft)
Diameter	2.68 m (8.8 ft)
Empty mass	Soyuz: 3,800 kg (8,400 lb); Soyuz/ST: 3,820 kg (8,420 lb)
Gross mass	43,400 kg (95,700 lb)
Powered by	RD-117
Maximum thrust	Sea Level: 838.5 kN (188,500 lbf); Vacuum: 1,021.3 kN (229,600 lbf)
Specific impulse	Sea Level: 262 s (2.57 km/s); Vacuum: 319 s (3.13 km/s)
Burn time	118 seconds
Propellant	LOX/RG-1
First stage – Blok-A
Height	27.10 m (88.9 ft)
Diameter	2.95 m (9.7 ft)
Empty mass	Soyuz: 6,550 kg (14,440 lb); Soyuz/ST: 6,450 kg (14,220 lb)
Gross mass	Soyuz: 99,500 kg (219,400 lb); Soyuz/ST: 99,400 kg (219,100 lb)
Powered by	RD-118
Maximum thrust	Sea Level: 792.5 kN (178,200 lbf); Vacuum: 990.2 kN (222,600 lbf)
Specific impulse	Sea Level: 255 s (2.50 km/s); Vacuum: 319 s (3.13 km/s)
Burn time	290 seconds
Propellant	LOX/RG-1
Second stage – Blok-I
Height	6.70 m (22.0 ft)
Diameter	2.66 m (8.7 ft)
Empty mass	Soyuz: 2,410 kg (5,310 lb); Soyuz/ST: 2,470 kg (5,450 lb)
Gross mass	Soyuz: 25,200 kg (55,600 lb); Soyuz/ST: 25,300 kg (55,800 lb)
Powered by	RD-0110
Maximum thrust	297.9 kilonewtons (67,000 lbf)
Specific impulse	325 seconds
Burn time	270 seconds
Propellant	LOX/RG-1
Upper stage (optional) – Fregat
Height	1.5 m (4.9 ft)
Diameter	3.35 m (11.0 ft)
Empty mass	930 kg (2,050 lb)
Propellant mass	5,250 kg (11,570 lb)
Powered by	S5.92
Maximum thrust	19.85 kilonewtons (4,460 lbf)
Specific impulse	333.2 seconds
Burn time	1100 seconds
Propellant	N2O4/UDMH
Upper stage (optional) – Ikar
Height	2.56 metres (8 ft 5 in)
Diameter	2.72 metres (8 ft 11 in)
Empty mass	820 kilograms (1,810 lb)
Gross mass	3,164 kilograms (6,975 lb)
Powered by	17D61
Maximum thrust	2.94 kilonewtons (660 lbf)
Specific impulse	307 seconds
Propellant	N2O4/UDMH
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Template:Launching/Progress

The Soyuz-U launch vehicle is an improved version of the original Soyuz rocket. 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 (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.^[6] As of 2016^[update] the rocket is still in service, although production has stopped since April 2015 as part of the transition process to Soyuz-2.^[10] The last flight is expected to take place on February 1, 2017, carrying Progress MS-05 to the International Space Station.

Soyuz-U has been in use continuously for 43 years, the longest lifetime of an orbital rocket worldwide. Production of R-7 derived launch vehicles peaked in the late 1970s-early 1980s at 55–60 a year. Soyuz-U holds the world record of highest launch rate in a year in 1979 with 47 flights. Over its operational lifetime, the Soyuz-U variant flew a total of 785 missions, another world record. Soyuz-U has also been one of the most reliabie launchers, with a success rate of 97.2%.

Development

The earlier Soyuz 11A511 was the first attempt at creating a standardized R-7 core in place of the numerous variations that had been used up to 1966. Starting that year, the 11A511 Blok I and strap-on boosters were added to the Voskhod (11A57), Vostok-2 (8A92), and Molniya-M (8K78M) vehicles as well as minor R-7 variants flown once or twice for specialized payloads.

The uprated 11A511U core was introduced to the R-7 family in 1973, yielding the carrier rocket variant named Soyuz-U, although adoption across the board was not complete until 1977 when the existing stock of 11A511-derived boosters was used up.

Versions

Two versions of Soyuz-U were fitted with an additional upper stage:

Soyuz-U/Ikar with the Ikar third 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. The performance of the Ikar upper stage is lower than that of the Fregat upper stage, but it is more precise in maneuvering and it can operate autonomously longer. This version was launched 6 times in 1999, carrying four GlobalStar satellites on each mission.^[3]
Soyuz-U/Fregat with the Fregat third stage, developed and produced by Lavochkin Association in Khimki. This version only flew 4 times in 2000;^[4] the Fregat upper stage was subsequently flown regularly atop Soyuz-FG and Soyuz-2 boosters.

An older variant of Soyuz-U, the Soyuz-U2 launcher, first flown in 1982, had the same hardware as the basic Soyuz-U. Instead of standard RP-1, it used a high energy, synthetic version, Syntin, as the first stage fuel. This variant, mainly used to transport crew and cargo to the Mir space station, last flew in 1995, after production of Syntin ended due to cost reasons.

Soyuz-U was the basic platform for the development of the Soyuz-FG variant, which used an all-new first stage and took over crew transport to the ISS in 2002. Since 2013, both Soyuz-U and Soyuz-FG are gradually being replaced by the modernized Soyuz-2 launch vehicle.

Human spaceflight

The first use of a Soyuz-U to launch a crewed 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.^[6]

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 crewed mission to utilize the Soyuz-U was Soyuz TM-34, a Soyuz ferry flight to the International Space Station.

A spectacular accident occurred on 26 September 1983, when the launcher for the Soyuz T-10a mission was destroyed by fire on the launch pad. The crew was saved by activation of the launch escape system a few seconds before the explosion.

Recent missions

Since the early 2000s, Soyuz-U vehicles have been used by the Russian Federal Space Agency primarily to launch Progress-M robotic cargo spacecraft on resupply missions to the International Space Station (ISS).

Although the Soyuz-U is generally very reliable, occasional failures have happened, such as the October 2002 launch of a Foton satellite which crashed near the pad at Plesetsk after the Blok D strap-on booster suffered an engine malfunction. One person on the ground was killed.

A recent Soyuz-U mission failed to launch Progress M-12M to the ISS on 24 August 2011, when the upper stage experienced a problem and broke up over Siberia. It was the first time a Progress spacecraft had failed to reach orbit. Another cargo ship, Progress MS-04, was lost on December 1, 2016 shortly after launch, likely due to a problem with the third stage of the Soyuz-U.

In April 2015 Soyuz-U was declared obsolete; its production has been stopped, and the rocket was scheduled for retirement after launching the remaining vehicles with Progress cargo ships.^[10] The last flight is scheduled for February 2017 with Progress MS-05.

References

^ http://www.astronautix.com/lvs/soyuzu.htm Astronautix.com
^ ^a ^b Krebs, Gunter. "Soyuz-U (11A511U)". Gunter's Space Page. Retrieved 20 December 2016.
^ ^a ^b Krebs, Gunter. "Soyuz-U Ikar (11A511U)". Gunter's space page. Retrieved 7 May 2016.
^ ^a ^b Krebs, Gunter. "Soyuz-U Fregat (11A511U)". Gunter's space page. Retrieved 7 May 2016.
^ ^a ^b In 1983, flight Soyuz T-10a took fire on the launch pad before the end of the countdown, so it is not counted in the list of launches; this is why adding successes and failures yields 786 launches instead of 785.
^ ^a ^b ^c Mark Wade (26 March 2001). "Soyuz 11A511U". Friends and Partners.
^ ^a ^b ^c "Soyuz-U User's Manual" (PDF). Starsem. Retrieved 11 March 2016.
^ "Конструкция разгонного блока "Фрегат"". NPO Lavochkin (in Russian). Retrieved 10 March 2016.
^ "IKAR Upper Stage". TsSKB-Progress. Retrieved 21 December 2015.
^ ^a ^b Nowakowski, Tomasz (30 June 2015). "All eyes on Progress: Russian spacecraft to deliver supplies to ISS". Spaceflight Insider. Retrieved 6 May 2016.

External links

[1] ttp://www.astronautix.com/lvs/soyuzu.htm Astronautix.com

[gunter-soyuz-u-2] Krebs, Gunter. "Soyuz-U (11A511U)". Gunter's Space Page. Retrieved 20 December 2016.

[gunter-ikar-3] Krebs, Gunter. "Soyuz-U Ikar (11A511U)". Gunter's space page. Retrieved 7 May 2016.

[gunter-fregat-4] Krebs, Gunter. "Soyuz-U Fregat (11A511U)". Gunter's space page. Retrieved 7 May 2016.

[explain-launch-counts-5] In 1983, flight Soyuz T-10a took fire on the launch pad before the end of the countdown, so it is not counted in the list of launches; this is why adding successes and failures yields 786 launches instead of 785.

[mwade-6] Mark Wade (26 March 2001). "Soyuz 11A511U". Friends and Partners.

[starsem-7] "Soyuz-U User's Manual" (PDF). Starsem. Retrieved 11 March 2016.

[lavochkin-fregat-8] "Конструкция разгонного блока "Фрегат"". NPO Lavochkin (in Russian). Retrieved 10 March 2016.

[9] "IKAR Upper Stage". TsSKB-Progress. Retrieved 21 December 2015.

[obsolete-10] Nowakowski, Tomasz (30 June 2015). "All eyes on Progress: Russian spacecraft to deliver supplies to ISS". Spaceflight Insider. Retrieved 6 May 2016.

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 The '''Soyuz-U''' [[launch vehicle]] is an improved version of the original [[Soyuz (rocket)|Soyuz rocket]]. Soyuz-U is part of the [[R-7 (rocket family)|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]] (now a united company, [[TsSKB-Progress]]). The first Soyuz-U flight took place on 18 May 1973, carrying as its payload [[Cosmos (satellite)|Kosmos 559]], a [[Zenit (satellite)|Zenit]] military surveillance satellite.<ref name=mwade /> {{Asof|2016}} the rocket is still in service, although production has stopped since April 2015 as part of the transition process to [[Soyuz-2 (rocket)|Soyuz-2]].<ref name=obsolete /> The last flight is expected to take place on February 1, 2017, carrying [[Progress MS-05]] to the [[International Space Station]].
-Soyuz-U has been in use continuously for 43 years, the longest lifetime of an orbital rocket worldwide. Production of R-7 derived launch vehicles peaked in the late 1970s-early 1980s at 55–60 a year. Soyuz-U holds the world record of highest launch rate in a year in 1979 with 47 flights. Over its operational lifetime, the Soyuz-U variant flew a total of 785 missions, another world record. Soyuz-U has also been one of the most reliabie launchers, with a success rate of {{percent|764|786|1}}.
+Soyuz-U has been in use continuously for 43 years, the longest lifetime of an orbital rocket worldwide. Production of R-7 derived launch vehicles peaked in the late 1970s-early 1980s at 55–60 a year. Soyuz-U holds the world record of highest launch rate in a year [[1979 in spaceflight#Launches|in 1979 with 47 flights]]. Over its operational lifetime, the Soyuz-U variant flew a total of 785 missions, another world record. Soyuz-U has also been one of the most reliabie launchers, with a success rate of {{percent|764|786|1}}.
 == Development ==

v t e Soviet and Russian launch vehicles
Active	Angara 1.2 A5 Soyuz-2 2.1a 2.1b 2-1v UR Proton-M
In development	Amur Irtysh Yenisei
Retired	Dnepr Energia Kosmos 1 2I 3 3M N1 R-7 Luna Molniya M L Polyot Soyuz original L M U U2 FG Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna Start-1 Tsyklon original 2 3 UR UR-500 Proton-K Rokot Strela Zenit 2 2M 3SL 3SLB 3F
Cancelled (no launch attempts)	Tsyklon-4 Proton Light Medium

v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased RS1^† Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 12 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)