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Retired

Soyuz STA

Soyuz STA Fregat

🏭 Progress Rocket Space Center🌐 Russian📖 Wikipedia
Soyuz STA

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

📏Height
46.3 m
⭕Diameter
2.95 m
⚖️Launch Mass
312 kg
🛰️LEO Capacity
7,020 kg
🌍GTO Capacity
2,810 kg
🗓️Maiden Flight
Dec 17, 2011
🚀Total Launches
8
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
Progress Rocket Space Center
🌐Country
Russian
📋Status
Retired

📷 Photo Gallery

Soyuz STA Fregat photo 1

🛰️ Launch History