NEUTRON
REUSABLE 2-STAGE LAUNCH VEHICLE
INACTIVE
Technical Overview
Length
height
40
m
Diameter
radio_button_unchecked
7
m
Launch Mass
scale
480
t
Payload to LEO
rocket
15,000
kg
Engine Details
Archimedes
Archimedes is Rocket Lab’s reusable methalox engine developed for Neutron.
Propellant
LOX / LNG
Thrust
733 kN
Cycle
Oxygen-rich staged combustion
Flight History
*Current Launch Library totals
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Total Launches
0
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Tracked launch count
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Successful Launches
0
verified
Completed launches
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Failed Launches
0
schedule
2 pending