Soyuz-L Explained
Soyuz-L |
Function: | Carrier rocket |
Manufacturer: | OKB-1 |
Country-Origin: | Soviet Union |
Stages: | Two |
Capacities: | |
Family: | R-7 |
Status: | Retired |
Sites: | Baikonur Site 31/6 |
Launches: | 3[1] |
Success: | 3 |
First: | 24 November 1970 |
Last: | 12 August 1971 |
Payloads: | LK |
Stagedata: | Type: | booster | Number: | 4 | Si: | 314 sec | Burntime: | 119 seconds |
Type: | Stage | Stageno: | First | Si: | 315 sec | Burntime: | 291 seconds |
Type: | Stage | Stageno: | Second | Thrust: | 294kN | Si: | 330 sec | Burntime: | 246 seconds |
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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.[2] 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.
Notes and References
- Web site: Soyuz-L (11A511L) . Gunter's space page . Gunter . Krebs . 6 May 2016.
- Web site: Soyuz. Wade. Mark. Encyclopedia Astronautica. 2009-04-16. dead. https://web.archive.org/web/20100107163113/http://astronautix.com/lvs/soyuz.htm. 2010-01-07.