Neutron
In DevelopmentRocket Lab · 2-stage orbital rocket
Total Launches
0
Success Rate
—
Payload to LEO
—
First Flight
—
Reusable
Yes
Specifications
Height42.8 m
Diameter7 m
Wet Mass480,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerRocket Lab
CountryNew Zealand
Engines Used
- Archimedes9x, Stage 1
- Archimedes1x, Stage 2
Engine usage data lives in the Engine Dashboard.
Launch History
No launches attributed to this vehicle in the database yet.
Reliability by Year
Reliability data not available yet.
Related Entities
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata