DBSE
Hardware/Vehicles/Zenit-2

Zenit-2

Retired

Yuzhnoye Design Bureau · 2-stage orbital rocket · Part of the Zenit family

Total Launches
36
Success Rate
80.6%
Payload to LEO
13.5 t
First Flight
1985
Reusable
No

Interactive Model

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Specifications

Height57 m
Diameter3.9 m
Wet Mass459,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerYuzhnoye Design Bureau
CountryUkraine

Engines Used

Engine usage data lives in the Engine Dashboard.

Launch History

Reliability by Year

Related Entities

Zenit-3SLVehicle familyZenit-3SLBVehicle familyAntares 110Vehicle familyAntares 120Vehicle familyAntares 130Vehicle familyAntares 230+Vehicle familyAntares 230Vehicle familyYuzhnoye Design BureauManufacturerRD-171MEngine

Data Sources for This Record

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