HEIGHT
VEHICLE PROFILE
Electron
Rocket Lab’s small orbital launch vehicle for dedicated satellite missions.
SPECIFICATIONS
DIAMETER / WIDTH
1.2 m / 3.9 ft
MASS CONTEXT
13,000 kg / 28,660 lb wet mass, per current Rocket Lab Electron reference.
PAYLOAD
300 kg / 661 lb payload to low Earth orbit, per current Rocket Lab Electron reference.
PROPULSION
First stage: nine sea-level Rutherford engines; second stage: one vacuum Rutherford engine; LOX/kerosene propellants; optional Kick Stage for precise deployment.
Dimensions and capabilities depend on configuration.
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