Function | Medium-lift launch vehicle |
---|---|
Manufacturer | TsSKB-Progress |
Country of origin | Soviet Union · Russia |
Size | |
Height | |
Diameter | 10.3 m (33 ft 10 in) |
Mass | |
Stages | 3 or 4 |
Capacity | |
Payload to LEO | |
Mass | |
Associated rockets | |
Family | R-7 (Soyuz) |
Based on | |
Derivative work | Soyuz-U2 · Soyuz-FG |
Launch history | |
Status | Retired |
Launch sites | |
Total launches | |
Success(es) | 765 |
Failure(s) | 21 [4] |
Notable outcome(s) | Soyuz T-10a [a] |
First flight | 18 May 1973 [7] |
Last flight | 22 February 2017 (Progress MS-05) |
Type of passengers/cargo | |
Boosters (First stage) – Block B, V, G & D [b] [3] | |
No. boosters | 4 |
Height | 19.6 m (64 ft 4 in) |
Diameter | 2.68 m (8 ft 10 in) |
Empty mass | 3,800 kg (8,400 lb) |
Gross mass | 43,400 kg (95,700 lb) |
Powered by | 1 × RD-117 |
Maximum thrust | SL: 838.5 kN (188,500 lbf) vac: 1,021.3 kN (229,600 lbf) |
Specific impulse | SL: 262 s (2.57 km/s) vac: 319 s (3.13 km/s) |
Burn time | 118 seconds |
Propellant | LOX/RG-1 |
Second stage (core) –Block A [3] | |
Height | 27.10 m (88 ft 11 in) |
Diameter | 2.95 m (9 ft 8 in) |
Empty mass | 6,550 kg (14,440 lb) |
Gross mass | 99,500 kg (219,400 lb) |
Powered by | 1 ×RD-118 |
Maximum thrust | SL:792.5 kN (178,200 lbf) vac:990.2 kN (222,600 lbf) |
Specific impulse | SL:255 s (2.50 km/s) vac:319 s (3.13 km/s) |
Burn time | 290 seconds |
Propellant | LOX/RG-1 |
Third stage –Block I [3] | |
Height | 6.70 m (22 ft 0 in) |
Diameter | 2.66 m (8 ft 9 in) |
Empty mass | 2,410 kg (5,310 lb) |
Gross mass | 25,200 kg (55,600 lb) |
Powered by | 1 ×RD-0110 |
Maximum thrust | 297.9 kN (67,000 lbf) |
Specific impulse | 325 s (3.19 km/s) |
Burn time | 270 seconds |
Propellant | LOX/RG-1 |
Fourth stage (optional) –Fregat [8] | |
Height | 1.5 m (4 ft 11 in) |
Diameter | 3.35 m (11.0 ft) |
Empty mass | 930 kg (2,050 lb) |
Propellant mass | 5,250 kg (11,570 lb) |
Powered by | 1 ×S5.92 |
Maximum thrust | 19.85 kN (4,460 lbf) |
Specific impulse | 333.2 s (3.268 km/s) |
Burn time | Up to 1,100 seconds (up to 7 starts) |
Propellant | N2O4 / UDMH |
Fourth stage (optional) –Ikar [9] [2] | |
Height | 2.56 m (8 ft 5 in) |
Diameter | 2.72 m (8 ft 11 in) |
Empty mass | 820 kg (1,810 lb) |
Gross mass | 3,164 kg (6,975 lb) |
Propellant mass | 2,310 kg (5,090 lb) |
Powered by | 1 ×S5.144 |
Maximum thrust | 2.943 kN (662 lbf) |
Specific impulse | 326 s (3.20 km/s) |
Burn time | Up to 600 seconds (up to 50 starts) |
Propellant | N2O4 / UDMH |
Soyuz-U (GRAU index:11A511U) was a Soviet and later Russian expendable medium-lift launch vehicle designed by the TsSKB design bureau and constructed at the Progress factory in Samara,Russia. The U designation stands for unified,as the launch vehicle was the replacement for both the Voskhod rocket and the original Soyuz rocket. The Soyuz-U is part of the R-7 rocket family,which evolved from the R-7 Semyorka,an intercontinental ballistic missile.
The first Soyuz-U flight took place on 18 May 1973,carrying as its payload Kosmos 559,a Zenit military surveillance satellite. [7] The final flight of a Soyuz-U rocket took place on 22 February 2017,carrying Progress MS-05 to the International Space Station.
Soyuz-U was in use continuously for almost 44 years. Production of R-7 derived launch vehicles peaked in the late 1970s-early 1980s at 55–60 a year. Soyuz-U held the world record of highest launch rate in a year in 1979 with 47 flights until this was beaten by SpaceX's Falcon 9 in 2022. [10] [11] Over its operational lifetime,the Soyuz-U variant flew a total of 786 missions,another world record. Soyuz-U has also been one of the most reliable launchers,with a success rate of 97.3%.
The original Soyuz rocket,introduced in 1966,represented the first attempt to standardize the R-7 design. It was largely identical to the Molniya booster but omitted the fourth stage. Two variants of the original Soyuz were produced,with at least three additional variants planned but ultimately canceled.
By the mid-1970s,the Soviet Union was operating a wide range of R-7 variants,including the Molniya,Voskhod,and various Vostok models. To address this fragmentation,the Soyuz-U was introduced as a unified platform. The "U" stood for "unified," as it replaced both the Voskhod and original Soyuz rockets. This model featured an upgraded core with enhanced RD-117/118 engines to mitigate issues like in-flight vibration and combustion instability. [12] [13]
Complete adoption of the Soyuz-U was not achieved until 1977,when the remaining stock of the original Soyuz boosters was depleted. However,despite the move toward standardization,some variants persisted. The Vostok-2M and Molniya-M continued to serve specialized roles,launching satellites into higher orbits until 1991 and 2010,respectively.
Two versions of Soyuz-U were fitted with an additional upper stage:
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.
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. [7]
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 use 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.
From 2000 until its retirement in 2017,Soyuz-U vehicles were 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 was generally reliable,occasional failures occurred,most of them on launches of Zenit and Yantar reconnaissance satellites. As with all Soviet/Russian launch vehicles,the 11A511U featured the AVD malfunction detection system which would terminate engine thrust in-flight if it detected a deviation from the booster's normal performance levels and on Soyuz launches also activate the launch escape system. The flight termination command could not be sent until 20 seconds into launch so the booster wouldn't fall onto or around the launch complex and the AVD could not generate a flight termination command until eight seconds to ensure the booster had entered stable mainstage operation. On June 18,1987,a launch of a Resurs satellite from Plesetsk ended disastrously when the Blok D strap-on LOX turbopump disintegrated at T+6 seconds due to ingested debris. The booster crashed near the pad,badly damaging it and putting it out of use for 18 months. During investigation into the mishap,it was concluded that the launch would not have been survivable had it been manned because the failure occurred before the AVD system could have activated,and thus the launch escape system would not have worked on a manned launch.
It was also concluded that eight seconds was excessive and the booster would reach mainstage operation by about T+1.6 seconds;the AVD system had been designed in the late 1950s when only a few R-7 prototypes had flown and there was little flight data to go by. The AVD was redesigned to be able to issue a flight termination command at 1.6 seconds,which of course would still be blocked until T+20 seconds.
On July 27,1988,the first R-7 vehicle with the redesigned AVD system launched from Plesetsk with another Resurs satellite. The AVD issued an erroneous shutdown command at T+1.6 seconds. The booster lifted and flew until T+20 seconds when the shutdown command was unblocked and terminated engine thrust,causing it to fall near LC-43/4 and severely damage it. An investigation into the mishap found that the new AVD system had a faulty circuit layout.
The October 2002 launch of a Foton satellite crashed near the pad at Plesetsk after the Blok D strap-on booster suffered an engine malfunction. One person on the ground was killed. The Blok D experienced an abnormally slow thrust rise at ignition followed by a decay in performance starting at T+4 seconds. The AVD system sensed the drop in Blok D performance and issued the flight termination command at T+5 seconds but it was blocked until T+20 seconds. The Blok D shut down completely and broke off the stack at T+8 seconds. The booster continued to climb but started deviating from its flight path due to the unbalanced thrust. The flight termination command was unblocked at T+20 seconds and the core and remaining strap-ons shut down. The booster impacted the ground at T+41 seconds as a crowd of 300 spectators watched. Six Russian military servicemen were injured and one later died of his injuries. A building used to produce compressed air and nitrogen was also badly damaged. Investigation into the mishap found that the Blok D's hydrogen peroxide pump had stopped working due to ingested debris.
A 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 1 December 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 was stopped and the rocket was scheduled for retirement after launching the remaining vehicles with Progress cargo ships. [14] The final flight was Progress MS-05,which launched from the Baikonur Cosmodrome on 22 February 2017,05:58:33 UTC. [15]
The modernized Soyuz 2 was introduced in 2004,adding several key enhancements,including improved engines along with digital flight control and telemetry systems,enabling launches from fixed platforms and the use of large payload fairings. The analogue flight control systems of the Soyuz-U and FG limited the ability of the launch vehicle to adjust its trajectory in-flight,requiring that the rocket be "aimed" before takeoff by a complex rotating launchpad. Long and wide payload fairings also introduced too much aerodynamic instability for the old analog system to handle,limiting the vehicle's potential to launch increasingly larger commercial satellites.
After several years of development,flight tests and concurrent use,the Soyuz 2 replaced the Soyuz-U in 2017 the Soyuz-FG in 2019,and launched its first crewed mission in 2020. [16] [17]
Proton is an expendable launch system used for both commercial and Russian government space launches. The first Proton rocket was launched in 1965. Modern versions of the launch system are still in use as of 2023, making it one of the most successful heavy boosters in the history of spaceflight. The components of all Protons are manufactured in the Khrunichev State Research and Production Space Center factory in Moscow and Chemical Automatics Design Bureau in Voronezh, then transported to the Baikonur Cosmodrome, where they are assembled at Site 91 to form the launch vehicle. Following payload integration, the rocket is then brought to the launch pad horizontally by rail, and raised into vertical position for launch.
Soyuz is a family of Soviet and later Russian expendable medium-lift launch vehicles initially developed by the OKB-1 design bureau and manufactured by the Progress Rocket Space Centre factory in Samara, Russia. It holds the record for the most launches in the history of spaceflight. Soyuz rockets are part of the R-7 rocket family, which evolved from the R-7 Semyorka, the world's first intercontinental ballistic missile.
Zenit was a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union. Zenit was originally built in the 1980s for two purposes: as a liquid rocket booster for the Energia rocket and, equipped with a second stage, as a stand-alone middle-weight launcher with a payload greater than the 7 tonnes of the Soyuz but smaller than the 20 tonnes payload of the Proton. The last rocket family developed in the USSR, the Zenit was intended as an eventual replacement for the dated Soyuz and Proton families, and it would employ propellants which were safer and less toxic than the Proton's nitrogen tetroxide/UDMH mix. Zenit was planned to take over crewed spaceship launches from Soyuz, but these plans were abandoned after the dissolution of the Soviet Union in 1991.
Soyuz‑2 is a modernized expendable medium-lift launch vehicle and the seventh major version of the Soyuz rocket family. It includes key enhancements over its predecessors, including improved engines along with digital flight control and telemetry systems, enabling launches from fixed platforms and the use of large payload fairings.
The Soyuz-FG launch vehicle was an improved version of the Soyuz-U from the R-7 family of rockets, designed and constructed by RKTs Progress in Samara, Russia. The rocket's guidance, navigation, and control system was developed and manufactured by the Polisvit Special Design Bureau in Kharkiv, Ukraine.
The RD-107 and its sibling, the RD-108, are a type of rocket engine used on the R-7 rocket family. RD-107 engines are used in each booster and the RD-108 is used in the central core. The engines have four main combustion chambers and either two (RD-107) or four (RD-108) vernier chambers.
The Molniya-M was a Soviet and Russian launch vehicle derived from the R-7 Semyorka Intercontinental ballistic missile (ICBM).
The Luna 8K72 vehicles were carrier rockets used by the Soviet Union for nine space probe launch attempts in the Luna programme between 23 September 1958 and 16 April 1960. Like many other Soviet launchers of that era, the Luna 8K72 vehicles were derived from the R-7 Semyorka design, part of the R-7, which was also the basis for the Vostok and modern Soyuz rocket.
The Soyuz was a Soviet expendable carrier rocket designed in the 1960s by OKB-1 and manufactured by State Aviation Plant No. 1 in Kuybyshev, Soviet Union. It was commissioned to launch Soyuz spacecraft as part of the Soviet human spaceflight program, first with eight uncrewed test flights, followed by the first 19 crewed launches. The original Soyuz also propelled four test flights of the improved Soyuz 7K-T capsule between 1972 and 1974. It flew 30 successful missions over ten years and suffered two failures.
Soyuz TMA-22 was a crewed spaceflight to the International Space Station (ISS). TMA-22 was the 111th flight of a Soyuz spacecraft, and transported three members of the Expedition 29 crew to the ISS. The spacecraft docked to the ISS on 16 November 2011, and remained docked to serve as an emergency escape vehicle until its undocking on 27 April 2012. Soyuz TMA-22 successfully landed in Kazakhstan on 27 April 2012 11:45 GMT.
Progress M-12M, identified by NASA as Progress 44P, was an uncrewed Progress spacecraft that was lost in a launch failure on 24 August 2011, at the start of a mission to resupply the International Space Station. It was the twelfth modernised Progress-M spacecraft to be launched. Manufactured by RKK Energia, the spacecraft was to have been operated by the Russian Federal Space Agency.
Meridian 5, also known as Meridian No.15L, was a communications satellite launched by the Russian Federal Space Agency which was lost in a launch failure in December 2011. The fifth Meridian spacecraft to be launched, Meridian 5 was to have been deployed into a Molniya orbit with an apogee of 39,000 kilometres (24,000 mi), a perigee of 900 kilometres (560 mi) and 65 degrees of orbital inclination; from which it would have provided communications for the Russian military. It would have been operated by the newly formed Russian Aerospace Defence Forces.
The Ikar was a Russian rocket upper stage introduced by TsSKB Progress in 1999 for use with its Soyuz-U rocket. It was derived from the propulsion module which had been used successfully on more than 30 Yantar reconnaissance satellites, leveraging existing equipment and subsystems to minimize new development. Modifications were limited to updates in command and control systems and adjustments to mechanical and electrical interfaces with payloads.
The Soyuz-ST-A and ST-B were modified versions of the Soyuz-2 rocket, designed to launch from the Guiana Space Centre (CSG) in French Guiana. Developed as part of a European Space Agency (ESA) programme to add a medium-lift launch vehicle to complement the light-lift Vega and heavy-lift Ariane 5 rockets.
Progress MS-01, identified by NASA as Progress 62P was a Progress spaceflight operated by Roscosmos to resupply the International Space Station (ISS) in 2015. It was launched on 21 December 2015, to deliver cargo to the ISS. Progress MS-01 is the first vehicle in the Progress-MS series.
Volga is a Russian rocket upper stage designed for use with the Soyuz-2.1a and Soyuz-2.1v rockets. It was derived from the propulsion module of the Yantar satellite, and is closely related to the retired Ikar upper stage. It serves as a lighter and more cost-effective alternative to the Fregat upper stage, used on most Soyuz-2 missions. RKTs Progress began development of the Volga in 2008 and the design was finalized in 2010.
Progress MS-04, identified by NASA as Progress 65P, was a Progress mission launched by Roscosmos in an unsuccessful attempt to resupply the International Space Station (ISS).
Soyuz flight VS22 was a rocket launch conducted by multinational launch service provider Arianespace. It was the sixteenth launch of a Soyuz-ST-B launch vehicle, and the 22nd launch of a Soyuz-2 series launch vehicle from the Ensemble de Lancement Soyouz at the Guiana Space Centre. After two scheduling delays and a 33-minute logistical delay, the rocket lifted off on 4 April 2019, and successfully delivered to medium Earth orbit the final four satellites in the O3b broadband satellite constellation, which services Latin America, Africa, and Oceania. After four previous Soyuz flights delivered the constellation's first sixteen satellites, the launch increased the constellation's throughput by 26 per cent. The flight marked the second occasion in which two Soyuz-2 launch vehicles were launched on the same day, occurring hours after the launch of Progress MS-11 from the Baikonur Cosmodrome.
This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out Comparison of Orbital Launch Systems.