Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Soyuz-L

From Wikipedia, the free encyclopedia
Soviet expendable carrier rocket
This article is about the Soyuz-L rocket. For other Soyuz variants, seeSoyuz (rocket family).
Not to be confused withSoyuz 1.
icon
This articleneeds additional citations forverification. Please helpimprove this article byadding citations to reliable sources. Unsourced material may be challenged and removed.
Find sources: "Soyuz-L" – news ·newspapers ·books ·scholar ·JSTOR
(December 2009) (Learn how and when to remove this message)
Soyuz-L
FunctionCarrier rocket
ManufacturerOKB-1
Country of originSoviet Union
Size
Height50 metres (160 ft)
Diameter10.3 metres (34 ft)
Mass300,000 kilograms (660,000 lb)
StagesTwo
Capacity
Payload toLEO
Mass5,500 kilograms (12,100 lb)
Associated rockets
FamilyR-7
Launch history
StatusRetired
Launch sitesBaikonurSite 31/6
Total launches3[1]
Success(es)3
First flight24 November 1970
Last flight12 August 1971
Carries passengers or cargoLK
Boosters
No. boosters4
Powered by1RD-107-8D728
Maximum thrust995 kilonewtons (224,000 lbf)
Specific impulse314 sec
Burn time119 seconds
PropellantRP-1/LOX
First stage
Powered by1RD-108-8D727
Maximum thrust977 kilonewtons (220,000 lbf)
Specific impulse315 sec
Burn time291 seconds
PropellantRP-1/LOX
Second stage
Powered by1RD-0110
Maximum thrust294 kilonewtons (66,000 lbf)
Specific impulse330 sec
Burn time246 seconds
PropellantRP-1/LOX

TheSoyuz-L (Russian:Союз, meaning "union"),GRAU index11A511L was aSovietexpendablecarrier rocket designed byOKB-1 and manufactured byState Aviation Plant No. 1 inSamara, Russia. It was created to test theLK lunar lander inlow Earth orbit, as part of theSoviet lunar programme.

The Soyuz-L was a derivative of the originalSoyuz rocket featuring the reinforced first stage and boosters supporting theMolniya-M's third stage, so that it could carry a more massive payload. A largerpayload 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 laterSoyuz-U used a similar configuration to the Soyuz-L.

References

[edit]
  1. ^abKrebs, Gunter."Soyuz-L (11A511L)".Gunter's space page. Retrieved6 May 2016.
  2. ^Wade, Mark."Soyuz".Encyclopedia Astronautica. Archived fromthe original on 2010-01-07. Retrieved2009-04-16.
Active
In development
Retired
Cancelled (no launch attempts)
Current
In development
Retired
Classes
  • 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)
Missiles
Launch systems
Vostok
Molniya
Soyuz
Soyuz 2
Launch sites
Launches
Engines
See also


Stub icon

This rocketry article is astub. You can help Wikipedia byexpanding it.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Soyuz-L&oldid=1268409590"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp