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The Soyuz-L, 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 program. 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.
Missions
3
Success Rate
100.0%
Successes
3
Failures
0
Success Streak
3
Partial Failures
0
Active 1970 to 1971
Rocket
Height: 48m
Payload to Orbit
LEO: 5,500 kg
GTO: 0 kg
Liftoff Thrust
4,054 Kilonewtons
Fairing
Diameter: 5m
Height: 7.8m
Stages
3
Strap-ons
4