Padside

Electron

Rocket Lab · Active

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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.

Specifications

Thrust
162 kN
Height
18 m
Diameter
1.2 m
Launch mass
13 t
Stages
3
Launch cost
$6M
LEO capacity
300 kg
GTO capacity
GEO capacity
SSO capacity
225 kg

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
91
Launches with a definitive outcome
Success rate
95.6%
87 of 91
Current success streak
50
Landings
7
9 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Boosters that flew this rocket

Boosters by flights

  1. 201 flights1/1 landings
  2. 221 flights1/1 landings
  3. 241 flights
  4. 251 flights
  5. 261 flights0/1 landings
  6. 271 flights
  7. 281 flights
  8. 291 flights
  9. 301 flights
  10. 161 flights1/1 landings

Serial-tracked stages only — predominantly SpaceX.

Launches

Next: Electron | StriX Launch 11July 31, 2026