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Hardware/Vehicles/Soyuz-2-1A

Soyuz-2-1A

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

Total Launches
59
Success Rate
98.3%
Payload to LEO
7.6 t
First Flight
2004
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 SSO4.9 t
ManufacturerTsSKB-Progress
CountryRussia

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

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