Neutron
Rocket Lab USA Vehicle
About
Medium-lift reusable launch vehicle (13,000 kg to LEO) powered by methane/LOX Archimedes engines. Carbon composite structure with captive Hungry Hippo fairing. In development.
Specifications
payload to leo kg 13000
stages 2
height m 43
diameter m 7
fairing diameter m 5
thrust kn 6606
propellant methane
reusable true
liftoff mass kg 480000
Tags
Technology
Orbit & Destination
Application
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