Progress Rocket Space Center

Soyuz 2.1a Fregat-M

Fregat-M

Soyuz 2.1a Fregat-M
Active

Overview

/01

The 2.1a version includes conversion from analog to digital flight control system and uprated engines on the booster and the first stage with improved injection systems. The new digital flight control and telemetry systems allow the rocket to launch from a fixed rather than angled launch platform and adjust its heading in flight. A digital control system also enables the launch of larger commercial satellites with wider and longer payload fairings such as the ST-type fairing. These fairings introduce too much aerodynamic instability for the old analog system to handle.

Manufacturer

Progress Rocket Space Center

Variant

Fregat-M

Alias

N/A

Maiden Flight

October 19, 2010

Technical Specifications

/02
46.3 m

Length

2.95 m

Diameter

0 t

Launch Mass

4149 kN

Liftoff Thrust

7020 kg

LEO Capacity

GTO Capacity

Launch Record

/03
19

Total Launches

18

Successful

1

Failed

94.7%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

← Back to Launchers