Soyuz-2

Soyuz‑2 (2.1a / 2.1b)
A Soyuz‑2.1b rocket launches carrying a GLONASS-K2 satellite to orbit
FunctionMedium-lift launch vehicle
ManufacturerRKTs Progress
Country of originRussia
Cost per launchUS$35 million (2018, 2.1b without fourth stage)[1][2]
Size
Height46.3 m (152 ft)[3]
Diameter10.3 m (33 ft 10 in)
Mass312,000 kg (688,000 lb)
Stages3 or 4
Capacity
Payload to LEO
Altitude240 km (150 mi)
Orbital inclination
  • 51.6° from Baikonur and Vostochny
  • 72° from Plesetsk
Mass
  • From Baikonur:
  • A: 7,430 kg (16,380 lb)
  • B: 8,670 kg (19,110 lb)
  • From Plesetsk:
  • A: 6,800 kg (15,000 lb)
  • B: 7,730 kg (17,040 lb)
  • From Vostochny:
  • A: 7,460 kg (16,450 lb)
  • B: 8,600 kg (19,000 lb)
Payload to Polar orbit
Altitude240 km (150 mi)
Orbital inclination98°
Mass
  • From Baikonur:
  • A: 5,830 kg (12,850 lb)
  • B: 7,030 kg (15,500 lb)
  • From Plesetsk:
  • A: 6,130 kg (13,510 lb)
  • B: 7,270 kg (16,030 lb)
  • From Vostochny:
  • A: 6,070 kg (13,380 lb)
  • B: 7,260 kg (16,010 lb)
Payload to TLI[a]
MassB: 2,350 kg (5,180 lb)[2]
Associated rockets
FamilyR-7 (Soyuz)
Based onSoyuz-FG
Derivative workSoyuz-ST
Soyuz-2.1v
Launch history
StatusActive
Launch sites
Total launches160 (A: 78, B: 82)
Success(es)155 (A: 75, B: 80)
Failure4 (A: 2, B: 2)
Partial failure1 (A: 1, B: 0)
First flight
  • A: 8 November 2004
  • B: 27 December 2006
Last flight
  • A: 25 December 2025 (most recent)
  • B: 5 February 2026 (most recent)
Carries passengers or cargo
Boosters (First stage) – Block B, V, G & D[b]
No. boosters4
Height19.6 m (64 ft 4 in)
Diameter2.68 m (8 ft 10 in)
Empty mass3,784 kg (8,342 lb)
Gross mass44,413 kg (97,914 lb)
Propellant mass
  • LOX: 27,900 kg (61,500 lb)
  • RP-1: 11,260 kg (24,820 lb)
Powered by1 × RD-107A
Maximum thrustSL: 838.5 kN (188,500 lbf)
vac: 1,021.3 kN (229,600 lbf)
Specific impulseSL: 262 s (2.57 km/s)
vac: 319 s (3.13 km/s)[4]
Burn time118 seconds
PropellantLOX / RP-1
Second stage (core) – Block A
Height27.1 m (88 ft 11 in)
Diameter2.95 m (9 ft 8 in)
Empty mass6,545 kg (14,429 lb)
Gross mass99,765 kg (219,944 lb)
Propellant mass
  • LOX: 63,800 kg (140,700 lb)
  • RP-1: 26,300 kg (58,000 lb)
Powered by1 × RD-108A
Maximum thrustSL: 792.5 kN (178,200 lbf)
vac: 990.2 kN (222,600 lbf)
Specific impulseSL: 255 s (2.50 km/s)
vac: 319 s (3.13 km/s)[4]
Burn time286 seconds
PropellantLOX / RP-1
Third stage – Block I[c]
Height6.7 m (22 ft 0 in)
Diameter2.66 m (8 ft 9 in)
Empty mass2,355 kg (5,192 lb)
Gross mass27,755 kg (61,189 lb)
Propellant mass
  • LOX: 17,800 kg (39,200 lb)
  • RP-1: 7,600 kg (16,800 lb)
Powered byA: 1 × RD-0110
B: 1 × RD-0124
Maximum thrustA: 298.03 kN (67,000 lbf)
B: 294.3 kN (66,200 lbf)[5]
Specific impulseA: 325 s (3.19 km/s)
B: 359 s (3.52 km/s)[6]
Burn timeA: 250 seconds
B: 270 seconds
PropellantLOX / RP-1
Fourth stage (optional) – Fregat / Fregat-M[7]
HeightFregat: 1.875 m (6 ft 1.8 in)
Fregat-M: 1.945 m (6 ft 4.6 in)
DiameterFregat: 3.44 m (11 ft 3 in)
Fregat-M: 3.8 m (12 ft 6 in)
Empty massFregat: 945 kg (2,083 lb)
Fregat-M: 1,035 kg (2,282 lb)
Gross massFregat: 6,235 kg (13,746 lb)
Fregat-M: 7,640 kg (16,840 lb)
Propellant massFregat: 5,307 kg (11,700 lb)
Fregat-M: 6,650 kg (14,660 lb)
Powered by1 × S5.92
Maximum thrust13.93–19.85 kN (3,130–4,460 lbf)
Specific impulse320–333.2 s (3.14–3.27 km/s)
Burn timeUp to 1,100 seconds (up to 7 starts)
PropellantN2O4 / UDMH
Fourth stage (optional) – Volga[8]
Height1.025 m (3 ft 4.4 in)
Diameter3.2 m (10 ft 6 in)
Empty mass840 kg (1,850 lb)
Propellant mass300–900 kg (660–1,980 lb)
Powered by1 × 17D64[9]
Maximum thrust2.94 kN (660 lbf)
Specific impulse307 s (3.01 km/s)
PropellantN2O4 / UDMH

Soyuz‑2 (Russian: Союз‑2, lit.'Union‑2', GRAU index: 14A14) is a Russian expendable medium-lift launch vehicle and the seventh major iteration of the Soyuz rocket family. Compared to its predecessors, Soyuz-2 features significant upgrades, including improved engines and a digital flight control system that enables launches from fixed platforms and supports larger payload fairings.

Developed by the Progress Rocket Space Centre (RKTs Progress) in Samara, Soyuz-2 is used to place payloads into low Earth orbit in standard configuration but can also support missions to higher orbits using an additional upper stage, most commonly the Fregat, though the smaller Volga is available as a less expensive option. Since its introduction in 2004, Soyuz-2 has gradually replaced earlier Soyuz variants and is launched from the facilities of its R-7 derived predecessors: Site 31/6 at the Baikonur Cosmodrome in Kazakhstan and Sites 43/3 and 43/4 at the Plesetsk Cosmodrome in northwestern Russia, and, since 2016, Site 1S at the Vostochny Cosmodrome in eastern Russia.

The Soyuz‑2 family includes several variants. The base model, Soyuz‑2.1a, debuted on 8 November 2004, followed by the Soyuz‑2.1b, with a 15 percent more powerful third stage, on 27 December 2006. A derivative version, Soyuz‑ST, was introduced in 2011 with modifications for operation at the Guiana Space Centre, the European Space Agency's launch site in French Guiana. Launches from this site were suspended in 2022 following the Russian invasion of Ukraine.

History

The Soyuz-2 project was initiated in the early 1990s by RKTs Progress with support from the Government of Russia as the "Rus" program. Following the Dissolution of the Soviet Union, it aimed to consolidate production within Russia and replace foreign-supplied systems while modernizing the aging Soyuz-U and Molniya-M launch vehicles. These earlier rockets relied on 1960s-era analog guidance systems developed by the Ukrainian Polisvit Special Design Bureau.[10]

Soyuz-2 introduced a fully digital flight control system and upgraded engines. Development of the digital system began in 1993 at NPO Avtomatiki in Yekaterinburg, incorporating triple redundancy and dual gyroscopes to improve reliability. The modernization program also included updated RD-107A and RD-108A engines for the boosters and core stage, as well as the development of the new RD-0124 third-stage engine employing oxygen-rich staged combustion. Together, these upgrades were intended to increase payload capacity by approximately 1,200 kilograms (2,600 lb).[11]

Financial constraints in the late 1990s led to a phased implementation. The upgraded RD-107A and RD-108A engines first flew on the transitional Soyuz-FG, while the majority of structural and avionics changes were incorporated into Soyuz-2.1a. The new RD-0124 engine was later introduced with Soyuz-2.1b.[11]

Soyuz-2.1a conducted its maiden suborbital flight from Plesetsk Cosmodrome on 8 November 2004 and entered operational service in October 2006 with the launch of MetOp-A for the European Space Agency and EUMETSAT. Soyuz-2.1b followed in December 2006. Between 2010 and 2019, the Soyuz-2 family gradually replaced Molniya-M, Soyuz-U, and Soyuz-FG.[12][13]

Variants

Soyuz-2.1a

Soyuz‑2.1a introduced the digital flight control system, replacing the analog unit used on previous Soyuz rockets.[2] The system enabled in-flight trajectory adjustments and supported larger payload fairings, permitting the launch of heavier commercial satellites.[14]

The vehicle uses upgraded RD-107A and RD-108A engines, featuring over 1,000 single-component injectors replacing earlier dual-component designs, improving combustion efficiency and increasing specific impulse by approximately 5-second (0.049 km/s).[15][2]

The third stage retained the RD-0110 engine but adopted enlarged propellant tanks and a revised structure shared with Soyuz-2.1b. Combined with the lighter avionics, these changes increased payload capacity by about 300 kilograms (660 lb).[3][16]

The first Soyuz‑2.1a launch took place on 8 November 2004 from Plesetsk Cosmodrome Site 43 with a boilerplate payload simulating a Zenit-8 reconnaissance satellite.[2]

Soyuz-2.1b

Soyuz 2.1b retains the upgrades of the 2.1a and introduces a new third stage powered by the RD-0124 engine. Using oxygen-rich staged combustion, the engine increases specific impulse from 326 to 359 seconds (3.20 to 3.52 km/s). Although maximum thrust was slightly reduced from 298 to 294 kilonewtons (67,000 to 66,000 lbf), extended burn time with the same propellant load improved overall performance.

The enhanced third stage significantly increased payload capability. From the Baikonur Cosmodrome, payload capacity to low Earth orbit rose from approximately 7,430 kilograms (16,380 lb) for the 2.1a to 8,670 kilograms (19,110 lb) for the 2.1b.[17][18]

The first Soyuz‑2.1b launch occurred on 26 July 2008 from Plesetsk Cosmodrome Site 43 with a classified military payload.[19]

Vostochny modifications

The Soyuz-2 family received specific modifications for operation from the Vostochny Cosmodrome, aimed at improving reliability, compatibility with ground infrastructure, and safety:[20][21]

  • Enhanced Durability: The rocket was modified to remain fueled on the launch pad for up to 100 hours and withstand transport over distances of up to 10,000 kilometres (6,200 mi) from the manufacturing site in Samara to the Russian Far East.
  • Adaptation for Vertical Integration: Structural and piping modifications enable vertical payload integration and safely vent excess propellant outside the Mobile Service Tower, minimizing oxygen vapor buildup inside the gantry.
  • Upgraded Computer: Offers six times the performance, reduced weight, and simplified wiring through multiplexing and shared data buses.[22][23][24]
  • Improved Batteries: New nickel-cadmium batteries eliminate the need for a dedicated charging station.

On 1 October 2015, it was revealed that parts of the assembly complex at Vostochny had been incorrectly designed for a different rocket variant, with some structures too small to accommodate Soyuz-2. This issue cast doubt on the planned inaugural launch in December 2015.[25] The first launch successfully took place on 28 April 2016.[26]

Notable missions

Suborbital test flight

On 8 November 2004, at 18:30 UTC, the first Soyuz‑2 rocket, in the Soyuz‑2.1a configuration, was launched from the Plesetsk Cosmodrome in Russia. The rocket followed a suborbital trajectory, with the third stage and Boilerplate landing in the Pacific Ocean.

Maiden launch

The first attempt at launching a Soyuz‑2 to orbit with the MetOp-A satellite occurred on 17 July 2006. It was scrubbed two hours before the launch by an automatic sequence after the onboard computer failed to check the launch azimuth. Fuelling of the rocket was underway at the time, and all launch complex equipment and onboard preliminary checks had proceeded without incident. The rocket was left fuelled on the launch pad for the next attempt on 18 July 2006. Launch was eventually conducted on 19 October 2006.

First crewed mission

The first crewed launch of Soyuz‑2 took place on 9 April 2020, carrying Soyuz MS-16 to the ISS.

Naphthyl fuel

Following successful ground testing, a naphthyl (Russian: нафтил) fueled Soyuz‑2.1b launch took place on 22 October 2022 at Vostochny. Naphthyl is an environmentally safe hydrocarbon fuel with fewer aromatic compounds than kerosene, which also slightly improves engine performance. There are only minor differences in thermal properties, viscosity, and surface tension, so this did not require significant engine changes.[27]

Launch statistics

Since 2006, Soyuz‑2 rockets have accumulated a total of 160 launches, 155 of which were successful, yielding a 97% success rate.

For Soyuz flights for ESA/Ariannespace from French Guiana see Soyuz-ST.

Launch outcomes

2
4
6
8
10
12
14
16
18
20
2006
2010
2015
2020
2025
  •   Failure
  •   Partial failure
  •   Success
  •   Planned

Launch sites

5
10
15
20
2006
2010
2015
2020
2025
  •   Baikonur
  •   Plesetsk
  •   Vostochny

List of launches

Planned launches

Launch date (UTC) Configuration Spaceport Result Payload Function Remark
19 March 2026 Soyuz‑2.1b / Fregat‑M Plesetsk, Site 43 Planned 16 x Rassvet-3 Internet Constellation
22 March 2026[161] Soyuz‑2.1a Baikonur, Site 31/6 Scheduled Progress MS-33 ISS logistics
2026[162] Soyuz‑2.1a / Fregat Vostochny, Site 1S Planned Meteor-M No.2-5 Weather
2026[163] Soyuz‑2.1b Vostochny, Site 1S Planned Resurs-PM No.1 Earth observation
2026[164][165] Soyuz‑2.1a / Fregat Vostochny, Site 1S Planned Kondor-FKA-M No.1 Reconnaissance
2026[162] Soyuz‑2.1a / Fregat Vostochny, Site 1S Planned Meteor-M No.2-6 Weather
2026[163] Soyuz‑2.1b Vostochny, Site 1S Planned Resurs-PM No.2 Earth observation
2026 Soyuz‑2.1b / Fregat‑M Plesetsk, Site 43 Planned GLONASS-K No. 19L Navigation
2026[166] Soyuz‑2.1a / Fregat‑M Plesetsk, Site 43 Planned Meridian-M No. 21L Communications
February 2026[161] Soyuz‑2.1a Baikonur, Site 31/6 Scheduled Progress MS-34 ISS logistics
March 2026[167] Soyuz‑2.1a Baikonur, Site 31 Planned Soyuz MS-29 ISS crew transport
May 2026[161] Soyuz‑2.1a Baikonur, Site 31/6 Scheduled Progress MS-35 ISS logistics
August 2026[161] Soyuz‑2.1a Baikonur, Site 31/6 Scheduled Progress MS-36 ISS logistics
September 2026[167] Soyuz‑2.1a Baikonur, Site 31 Planned Soyuz MS-30 ISS crew transport
October 2026[161] Soyuz‑2.1a Baikonur, Site 31/6 Scheduled Progress MS-37 ISS logistics
2027[168] Soyuz‑2.1b / Fregat Vostochny, Site 1S Planned Luna 26 Lunar orbiter
Soyuz‑2.1b / Fregat Plesetsk, Site 43 Planned GLONASS-K 19–23 Navigation

See also

Notes

  1. ^ with Fregat from Baikonur
  2. ^ This is a transliteration of the second through fifth letters of the Cyrillic alphabet (Б, В, Г, Д). A sense-for-sense translation would correspond to the second through fifth letters of the Latin alphabet, 'Block B, C, D & E'.
  3. ^ This is a transliteration of the tenth letter of the Cyrillic alphabet (И), which also carries the numerical value 10 in Cyrillic numerals. A sense-for-sense translation would use a Roman numeral, 'Block X'.

References

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