DBSE
Hardware/Vehicles/Soyuz-ST-A

Soyuz-ST-A

Retired

TsSKB-Progress · 3-stage orbital rocket · Part of the R-7 family

Total Launches
0
Success Rate
—
Payload to LEO
7.6 t
First Flight
2011
Reusable
No

Interactive Model

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Specifications

Height50.7 m
Diameter2.95 m
Wet Mass313,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerTsSKB-Progress
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

No launches attributed to this vehicle in the database yet.

Reliability by Year

Reliability data not available yet.

Related Entities

Soyuz-UVehicle familySoyuz-FGVehicle familySoyuz-2-1AVehicle familySoyuz-2-1B FregatVehicle familySoyuz-2-1A FregatVehicle familySoyuz-2-1BVehicle familySoyuz-ST-BVehicle familyRD-107AEngine

Data Sources for This Record

Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata