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Soyuz 2.1a Fregat-M

Progress Rocket Space Center · Russland

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.

Hersteller
Progress Rocket Space Center
Erstflug
19. Oktober 2010
Starts
20
Erfolgreich
19
Fehlgeschlagen
1
Erfolgsquote
95%
Geplant
1
Höhe
46,3 m
Durchmesser
2,95 m
Startmasse
312 t
Nutzlast in den niedrigen Erdorbit
7.020 kg
Wiederverwendbar
nein

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