LauncherOne
RetiredVirgin Orbit · 2-stage orbital rocket
Total Launches
6
Success Rate
66.7%
Payload to LEO
0.3 t
First Flight
2020
Reusable
No
Specifications
Height21.3 m
Diameter1.57 m
Wet Mass30,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerVirgin Orbit
CountryUnited States
Engines Used
- NewtonThree1x, Stage 1
- NewtonFour1x, 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