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Soyuz-L (11A511L)
Size
Function	Medium-lift launch vehicle
Manufacturer	OKB-1
Country of origin	Soviet Union
Height	50 m (160 ft)
Diameter	10.3 m (34 ft)
Mass	300,000 kg (660,000 lb)
Stages	3
Capacity
Payload to LEO
Mass	5,500 kg (12,100 lb)

Associated rockets
Family	R-7
Launch history
Status	Retired
Launch sites	Baikonur, Site 31/6
Total launches	3^[1]
Success(es)	3
First flight	24 November 1970
Last flight	12 August 1971
Carries passengers or cargo	LK
Boosters (First stage) – Block B, V, G & D^[a]
No. boosters	4
Powered by	1 × RD-107-8D728
Maximum thrust	995 kN (224,000 lb_f)
Total thrust	3,980 kN (890,000 lb_f)
Specific impulse	314 s (3.08 km/s)
Burn time	119 seconds
Propellant	LOX / RP-1
Second stage (core) – Block A
Powered by	1 × RD-108-8D727
Maximum thrust	977 kN (220,000 lb_f)
Specific impulse	315 s (3.09 km/s)
Burn time	291 seconds
Propellant	LOX / RP-1
Third stage
Powered by	1 × RD-0110
Maximum thrust	294 kN (66,000 lb_f)
Specific impulse	330 s (3.2 km/s)
Burn time	246 seconds
Propellant	LOX / RP-1
[edit on Wikidata]

The Soyuz-L (Russian: Союз, lit. 'union', GRAU index: 11A511L) was a Soviet expendable carrier rocket designed by OKB-1 and manufactured by State Aviation Plant No. 1 in Samara, Russia. It was created to test the LK lunar lander in low Earth orbit, as part of the Soviet lunar programme.

The Soyuz-L was a derivative of the original Soyuz rocket featuring the reinforced first stage and boosters supporting the Molniya-M's third stage, so that it could carry a more massive payload. A larger payload fairing was also fitted, to accommodate the LK spacecraft.^[2] The Soyuz-L was only launched three times between 1970 and 1971, all successful.^[1] The later Soyuz-U used a similar configuration to the Soyuz-L.

Notes

[edit]

^ 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'.

References

[edit]

^ ^a ^b Krebs, Gunter. "Soyuz-L (11A511L)". Gunter's space page. Retrieved 6 May 2016.
^ Wade, Mark. "Soyuz". Encyclopedia Astronautica. Archived from the original on 2010-01-07. Retrieved 2009-04-16.

v t e Soviet and Russian launch vehicles
Active	Angara 1.2 A5 Soyuz-2 2.1a 2.1b 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 M U U2 FG 2.1v 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 2^† Chollima-1 Electron Eris^† Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H3 HANBIT-NANO^† Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 2 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 6C 7 7A 8 11 11H 12 12A LVM3 Minotaur I IV V C New Glenn Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB Spectrum^† SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2E 3
In development	Antares 330 Bloostar Blue Whale 1 Cyclone-4M Deca Eclipse Epsilon S Gravity-2 Hyperbola-2 Irtysh Kinetica 2H 3 KSLV-III Kuaizhou 21 31 Long March 9 10 Miura 5 Neutron New Line 1 NGLV Nova OS-M 2 4 Pallas-1 Red Dwarf RFA One SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero 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-IIA 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 M U U2 2-1v Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† 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^† 2
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)

R-7 rockets

Missiles

👁 Image

Launch systems

Sputnik Polyot Voskhod
Vostok	Luna Vostok-L Vostok-K Vostok-2 Vostok-2M
Molniya	Molniya Molniya-M
Soyuz	Soyuz/Vostok Soyuz Soyuz-M Soyuz-U U2 Soyuz-FG
Soyuz 2	Soyuz 2.1a / 2.1b ST-A / ST-B Soyuz 2.1v

Launch sites

Launches

Engines

URL: https://en.wikipedia.org/wiki/Soyuz-L

⇱ Soyuz-L - Wikipedia

Notes

References