Soyuz-L
This article needs additional citations for verification. (December 2009) |
Function | OKB-1 |
---|---|
Country of origin | Soviet Union |
Size | |
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 | 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
- ^ 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.