/
The Soyuz-2.1v represents a major departure from earlier Soyuz rockets. Unlike the Soyuz-2.1b upon which it is based, it does away with the four boosters used on all other R-7 vehicles. The first stage of the Soyuz-2.1v is a heavily modified derivative of the Soyuz-2 first stage, with a single-chamber NK-33 engine replacing the four-chamber RD-107 used on previous rockets along with structural modifications to the stage and lower tanking. Since the NK-33 is fixed, the RD-0110R engine is used to supply thrust vector control.
Missions
13
Success Rate
96.2%
Successes
12
Failures
0
Success Streak
11
Partial Failures
1
Active 2013 to 2025
Rocket
Height: 44.08m
Payload to Orbit
LEO: 2,850 kg
GTO: 0 kg
Liftoff Thrust
1,535 Kilonewtons
Fairing
Diameter: 3m
Height: 8.36m
Stages
3
Active 2018 to 2024
Rocket
Height: 44.08m
Payload to Orbit
LEO: 3,000 kg
GTO: 0 kg
Liftoff Thrust
1,535 Kilonewtons
Fairing
Diameter: 3m
Height: 8.36m
Stages
2