Rokot
RetiredKhrunichev · 3-stage orbital rocket · Part of the UR-100N family
Total Launches
32
Success Rate
90.6%
Payload to LEO
1.9 t
First Flight
1994
Reusable
No
Specifications
Height29 m
Diameter2.5 m
Wet Mass107,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerKhrunichev
CountryRussia
Engines Used
No engine records tracked for this vehicle yet.
Engine usage data lives in the Engine Dashboard.
Launch History
Reliability by Year
Related Entities
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata