Soyuz-L

In today's world, Soyuz-L has become a topic of great interest and relevance in various areas of society. From the scientific to the political sphere, Soyuz-L has captured the attention of researchers, academics, leaders and citizens in general, generating intense debate and analysis around its implications and repercussions. In this article, we will explore in detail the different facets and perspectives of Soyuz-L, examining its impact today and possible projections for the future. From its origin to its evolution, including its effects on the present, we will delve into a complete and exhaustive analysis of Soyuz-L, addressing its positive, negative and controversial aspects.

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Soyuz-L
Size
Function	Carrier rocket
Manufacturer	OKB-1
Country of origin	Soviet Union
Height	50 metres (160 ft)
Diameter	10.3 metres (34 ft)
Mass	300,000 kilograms (660,000 lb)
Stages	Two
Capacity
Payload to LEO
Mass	5,500 kilograms (12,100 lb)

Associated rockets
Family	R-7
Launch history
Status	Retired
Launch sites	Baikonur Site 31/6
Total launches	3
Success(es)	3
First flight	24 November 1970
Last flight	12 August 1971
Type of passengers/cargo	LK

Boosters
No. boosters	4
Powered by	1 RD-107-8D728
Maximum thrust	995 kilonewtons (224,000 lb_f)
Specific impulse	314 sec
Burn time	119 seconds
Propellant	RP-1/LOX
First stage
Powered by	1 RD-108-8D727
Maximum thrust	977 kilonewtons (220,000 lb_f)
Specific impulse	315 sec
Burn time	291 seconds
Propellant	RP-1/LOX
Second stage
Powered by	1 RD-0110
Maximum thrust	294 kilonewtons (66,000 lbf)
Specific impulse	330 sec
Burn time	246 seconds
Propellant	RP-1/LOX

[edit on Wikidata]

The Soyuz-L (Russian: Союз, meaning "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. The Soyuz-L was only launched three times between 1970 and 1971, all successful. The later Soyuz-U used a similar configuration to the Soyuz-L.

References

^ ^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 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 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 original C Vulcan Centaur Zenit 3SL 3SLB 3F Zhuque 2
In development	Antares 330 Ariane 6 Bloostar Cyclone-4M 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 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 VLS-1^† Zenit 2 2M 2FG 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)

R-7 rockets

Main articles

Rockets

Missiles

Launch systems

Sputnik Polyot Voskhod
Vostok	Luna Vostok-L Vostok-K Vostok-2 Vostok-2M
Molniya	Molniya Molniya-M
Soyuz	Soyuz/Vostok Soyuz Soyuz-L Soyuz-M Soyuz-U Soyuz-U2 Soyuz-FG
Soyuz-2	Soyuz 2.1a / STA Soyuz 2.1b / STB Soyuz 2-1v

Launch sites

Baikonur	Site 1/5 Site 31/6
Plesetsk	Site 41/1 Site 16/2 Site 43/3 Site 43/4
Kourou	Ensemble de Lancement Soyouz
Vostochny	Site 1A Site 1S

Launches

Soyuz-L

References

Wikious

Boobota

Sagapedia