Rockets

Launch Vehicle

Electron

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Specifications

Status
active
Height
18 m
Diameter
1.2 m
Mass
13,000 kg
Stages
3
Thrust
162 kN
Payload to LEO
300 kg
First flight
2017-05-25
Total launches
91
Success / Fail
87 / 4

Electron is a two-stage orbital expendable launch vehicle (with an optional third stage) developed by the American aerospace company Rocket Lab. Electron is a small-lift launch vehicle designed to launch small satellites and cubesats to sun-synchronous orbit and low earth orbit. The Electron is the first orbital class rocket to use electric-pump-fed engines, powered by the 9 Rutherford engines on the first stage. It is also used as a suborbital testbed (called HASTE) for hypersonics research.

Propulsion

First stage

9×Rutherford25 kN
RP-1 / LOX · electric-pump
Rocket LabIsp 311s (vac)since 2017

Second stage

Rutherford Vacuum26 kN
RP-1 / LOX · electric-pump
Rocket LabIsp 343s (vac)since 2017

Payloads it launched

60 loaded

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