Electron
ActiveRocket Lab · 2-stage orbital rocket
Total Launches
91
Success Rate
95.6%
Payload to LEO
0.3 t
First Flight
2017
Reusable
No
Interactive Model
Specifications
Height18 m
Diameter1.2 m
Wet Mass13,000 kg
Payload to GTON/A
Payload to SSO0.2 t
ManufacturerRocket Lab
CountryNew Zealand
Engines Used
- Rutherford9x, Stage 1
- Rutherford Vacuum1x, Stage 2
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