Soyuz-U

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  1. In 1983, during flight Soyuz T-10a, a rocket erupted in fire on the launch pad before the end of the countdown. The launch escape system pulled the crew to safety six seconds before the rocket exploded. It is not counted in the list of launches or in-flight failures.
  2. This is a transliteration of the second through fifth letters of the Cyrillic alphabet (Б, В, Г, Д). The English translation is Block B, C, D & E.

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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.

References

  1. 1 2 "Soyuz-U". Archived from the original on 11 December 2016. Retrieved 19 March 2022. Astronautix.com
  2. 1 2 3 "Soyuz 11A511U / Ikar". Astronautix.com. Retrieved 10 December 2024.
  3. 1 2 3 4 5 "Soyuz-U User's Manual" (PDF). Starsem. Retrieved 11 March 2016.
  4. 1 2 Krebs, Gunter. "Soyuz-U (11A511U)". Gunter's Space Page. Retrieved 22 February 2017.
  5. 1 2 Krebs, Gunter. "Soyuz-U Fregat (11A511U)". Gunter's space page. Retrieved 7 May 2016.
  6. 1 2 Krebs, Gunter. "Soyuz-U Ikar (11A511U)". Gunter's space page. Retrieved 7 May 2016.
  7. 1 2 3 Mark Wade (26 March 2001). "Soyuz 11A511U". Friends and Partners. Archived from the original on 4 March 2016. Retrieved 7 January 2009.
  8. Конструкция разгонного блока "Фрегат". NPO Lavochkin (in Russian). Archived from the original on 26 December 2015. Retrieved 10 March 2016.
  9. "IKAR Upper Stage". TsSKB-Progress. Retrieved 21 December 2015.
  10. @elonmusk (20 October 2022). "Congrats to @SpaceX team on 48th launch this year! Falcon 9 now holds record for most launches of a single vehicle type in a year" (Tweet) via Twitter.
  11. "Soyuz-FG on penultimate flight delivers three new crewmembers for ISS". NASASpaceFlight.com. 20 July 2019. Retrieved 21 October 2022.
  12. Soyuz at the Guiana Space Centre User’s Manual Issue 1 (PDF). Arianespace. June 2006. p. 1-4. Archived from the original (PDF) on 27 September 2007. Retrieved 26 November 2024.
  13. "ЖРД РД-107 и РД-108 и их модификации" [RD-107 and RD-108 and their modifications] (in Russian). Retrieved 19 February 2024.
  14. Nowakowski, Tomasz (30 June 2015). "All eyes on Progress: Russian spacecraft to deliver supplies to ISS". Spaceflight Insider. Archived from the original on 21 April 2016. Retrieved 6 May 2016.
  15. Chris Gebhardt (21 February 2017). "Longest-serving rocket in history bids farewell with Progress MS-05 launch". NasaSpaceFlight.com.
  16. Zak, Anatoly (1 June 2011). "Soyuz-2 to replace its predecessors". RussianSpaceWeb.com.
  17. "Alexander Kirilin: "We are working on three rocket"". Volzkhskaya Kommuna. 1 June 2011. Archived from the original on 19 March 2012. Retrieved 13 July 2011.
Soyuz-U
Soyuz 18 booster.jpg
A Soyuz-U on the launchpad for the Soyuz 18 mission in 1975
Function Medium-lift launch vehicle
Manufacturer TsSKB-Progress
Country of origin Soviet Union  · Russia
Size
Height
  • Soyuz-U: 50.7 m (166 ft 4 in) [1]
  • Soyuz-U/Ikar: 47.4 m (155 ft 6 in) [2]
  • Soyuz-U/Fregat: 42.5 m (139 ft 5 in) [3]
Diameter10.3 m (33 ft 10 in)
Mass
  • Soyuz-U: 313,000 kg (690,000 lb) [1]
  • Soyuz-U/Ikar: 305,000 kg (672,000 lb) [2]
  • Soyuz-U/Fregat: 308,000 kg (679,000 lb) [3]
Stages3 or 4
Capacity
Payload to LEO
Mass
Associated rockets
Family R-7 (Soyuz)
Based on
Derivative work Soyuz-U2  · Soyuz-FG
Launch history
StatusRetired
Launch sites
Total launches
  • 786:
  •   U: 776 [4]
  •   U/Fregat: 4 [5]
  •   U/Ikar: 6 [6]
Success(es)765
Failure(s)21 [4]
Notable outcome(s) Soyuz T-10a [a]
First flight18 May 1973 [7]
Last flight22 February 2017 (Progress MS-05)
Type of passengers/cargo
Boosters (First stage) – Block B, V, G & D [b] [3]
No. boosters4
Height19.6 m (64 ft 4 in)
Diameter2.68 m (8 ft 10 in)
Empty mass3,800 kg (8,400 lb)
Gross mass43,400 kg (95,700 lb)
Powered by1 × RD-117
Maximum thrustSL: 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 time118 seconds
Propellant LOX/RG-1