Patent · US Active

Neutralizer for an ion thruster of a spacecraft

US12168976B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 2, 2021
Grant dateDec 17, 2024
Priority date
Expiry dateMar 18, 2041

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF03H1/005
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A Neutralizer for an ion thruster of a spacecraft comprises a cathode for emission of electrons, a support with an opening inside which the cathode is supported in a radially spaced manner, and an electrically conductive shielding which surrounds said opening and is electrically insulated from the support, wherein a ring is mounted between the shielding and the cathode and is electrically insulated from the shielding and radially spaced from the cathode.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.