Energiya/Buran
RetiredNPO Energiya · 1-stage orbital rocket · Part of the Energiya family
Total Launches
1
Success Rate
100%
Payload to LEO
88 t
First Flight
1988
Reusable
Yes
Interactive Model
Specifications
Height58.7 m
Diameter7.75 m
Wet Mass2,524,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerNPO Energiya
CountryRussia
Engines Used
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