Orbital launch vehicle
Neutron
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.
Flights flown03 scheduled
Payload to LEO15,000kg
Neutron is built by Rocket Lab of the United States. Company background, funding, contracts and news for this operator are tracked on Space Index.
Payload
| Low Earth orbit | 15,000kg |
|---|
Vehicle
| Stages | 2 |
|---|---|
| Length | 40m |
| Diameter | 7m |
| Launch mass | 480t |
| Liftoff thrust | 5,960kN |
| Reusable | Yes |
Pads used
Orbits delivered
Heliocentric N/A1Low Earth Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| TBD | Neutron | NZSA Venus Mission | Rocket Lab Launch Complex 3 (Launch Area 0 D) | Heliocentric N/A | Scheduled |
| TBD | Neutron | Maiden Flight | Rocket Lab Launch Complex 3 (Launch Area 0 D) | Unknown | Scheduled |
| TBD | Neutron | Kepler Communications Constellation | Rocket Lab Launch Complex 3 (Launch Area 0 D) | Low Earth Orbit | Scheduled |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia · Operator page