DBSE
Hardware/Vehicles/Zenit-3SL

Zenit-3SL

Retired

Yuzhnoye Design Bureau · 3-stage orbital rocket · Part of the Zenit family

Total Launches
36
Success Rate
91.7%
Payload to LEO
—
First Flight
1999
Reusable
No

Interactive Model

Open full size →

Specifications

Height59.6 m
Diameter3.9 m
Wet Mass471,000 kg
Payload to GTO5 t
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-2Vehicle 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