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Soyuz STA/Fregat | Pléiades-HR 1A, FASat-Charlie (SSOT), 4 x ELISA

Soyuz STA

Family: Soyuz
Configuration: Fregat

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. This stage continues to use the RD-0110 engine. The 2.1a/ST version is sometimes called Soyuz ST-A.

Specifications
  • Stages
    3
  • Length
    46.3 m
  • Diameter
    2.95 m
  • Fairing Diameter
  • Launch Mass
    312 T
  • Thrust
Family
  • Name
    Soyuz STA
  • Family
    Soyuz
  • Variant
    Fregat
  • Alias
  • Full Name
    Soyuz STA Fregat
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    7020 kg
  • Geostationary Transfer Orbit
    2810 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity
    4230 kg

Progress Rocket Space Center

Circle Image
Dmitry Baranov Founded: 1996 Successes: 44 Failures: 1 Pending: 0

Agency Type: Commercial

Progress Rocket Space Centre, formerly known as TsSKB-Progress, is a space science and aerospace research company which is known for manufacturing launch vehicles and satellites. Most notably, Progress Rocket Space Centre is the manufacturer of Soyuz launch vehicles.

INFO WIKI

Kourou, French Guiana

Soyuz Launch Complex


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