The RAE/Culham T4 10cm Electron-Bombardment Mercury Ion Thruster.

Abstract

The RAE/Culham T4 thruster is described with particular reference to its suitability for N-S station-keeping on planned European communication satellites and for many other possible missions. Details are given of the design, construction, testing and performance, including the characteristics and life-test experience of components such as vaporisers, isolators and grids. The accuracy of the physically-based scaling laws used in the design is demonstrated. Special reference is made to the excellent thermal stability and performance of the grid system, to efforts made to minimise grid erosion, and to the flexibility offered by a large throttling range.

Document Details

Document Type
Technical Report
Publication Date
Feb 04, 1974
Accession Number
ADA004927

Entities

People

  • C. M. Philip
  • D. G. Fearn
  • H. H. H. Watson
  • P. J. Harbour
  • R. Hastlings

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Accuracy
  • Artificial Satellites
  • Communication Satellites
  • Construction
  • Electric Propulsion
  • Electrons
  • Engineering
  • Ion Thrusters
  • Joule Thomson Effect
  • Life Tests
  • Mechanical Engineering
  • Propulsion Systems
  • Scaling Laws
  • Thermal Stability
  • Thrusters

Fields of Study

  • Physics

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Pulsed Power and Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites