Soyuz-L

Source: Wikipedia, the free encyclopedia.
Soyuz-L
Function
OKB-1
Country of originSoviet Union
Size
Height50 metres (160 ft)
Diameter10.3 metres (34 ft)
Mass300,000 kilograms (660,000 lb)
StagesTwo
Capacity
Payload to LEO
Mass5,500 kilograms (12,100 lb)
Associated rockets
Family
LOX

The Soyuz-L (

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.

References

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