1

As we can see, in the first stage of Rocketlab's Electron the nozzles have small nozzle exit area.

Side view of Electron Rocket first stage's nine Rutherford engines Rear three-quarter view of Electron rocket second stage's single Rutherford engine

Source (all)

But for second stage why are they using nozzle skirt/ extension with huge exit area?

Comparison of Rocket Labs' Rutherford sea-level and vacuum optimised engines

Amar
  • 2,246
  • 1
  • 12
  • 35

0 Answers0