Neutron

In-active Re-Usable

Rocket Lab (RL)

None

Description

Neutron is an upcoming medium-lift two-stage launch vehicle under development by Rocket Lab. Neutron features a reusable first stage fueled by LOX and Methane.

Specifications
  • Stages
    2
  • Length
    40.0 m
  • Diameter
    7.0 m
  • Fairing Diameter
    5.0 m
  • Launch Mass
    480.0 T
  • Thrust
    5960.0 kN
Family
  • Name
    Neutron
  • Family
  • Variant
  • Alias
  • Full Name
    Neutron
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    15000.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Rocket Lab

Commercial
CEO: Peter Beck
RL 2006

Rocket Lab is an American aerospace manufacturer with a wholly owned New Zealand subsidiary. The company develops lightweight, cost-effective commercial rocket launch services. The Electron Program was founded on the premise that small payloads such as CubeSats require dedicated small launch vehicles and flexibility not currently offered by traditional rocket systems. Its rocket, the Electron, is a light-weight rocket and is now operating commercially. The company is also producing a variety of spacecrafts and spacecrafts components.

Upcoming Spaceflights


Neutron | Maiden Flight

Rocket Lab | United States of America
Wallops Flight Facility, Virginia, USA
TBD December, 2025
Status: To Be Determined
Mission:

Maiden flight of the Neutron launch vehicle.

Unknown
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Neutron | NZSA Venus Mission

Rocket Lab | United States of America
Wallops Flight Facility, Virginia, USA
TBD December, 2026
Status: To Be Determined
Mission:

NZSA Venus Mission is a small direct Venus entry probe with a single 1 kg low-mass, low-cost autofluorescing nephelometer riding on a satellite bus based on the Photon Upper stage of the Electron rocket. The probe mission will spend approximately 5 minutes in the Venus cloud layers, 48-60 km above the surface, collecting in situ measurements to search for organic molecules in cloud particles and constrain particle composition.

Heliocentric N/A
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