Finite Element Analysis of Particle Ionization within Carbon Nanotube Ion Micro Thruster

Abstract

As electric propulsion becomes more of a viable option for satellite station keeping, MEMS electrodes are being more thoroughly investigated for their operational capacity. Computer modelling simulations of the particle physics involved during the initial ionization events of plasma generation have proven reliable in determining the effectiveness of carbon nanotube-covered nozzles. Two different simulations, comparing angled-wall etched nozzles with and without CNT deposition, demonstrated improvement of ion beam current when the walls are lined with carbon nanotubes. These models agree well with experimental results in the initial ionization event regime. Further investigation of complete plasma physics simulation and ionization parameter characterization are required to refine the simulation before it is a complete, viable system for thruster design optimization.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 2017
Accession Number
AD1053238

Entities

People

  • Jamison R. Fiebrandt

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Advanced Electronics
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Assembly
  • Boundary Layer
  • Carbon Nanotubes
  • Charged Particles
  • Electric Fields
  • Electric Propulsion
  • Electron Emission
  • Electrons
  • Emission
  • Finite Element Analysis
  • Fluid Dynamics
  • Fluid Flow
  • Fullerenes
  • Geometry
  • Ion Beams
  • Ion Thrusters
  • Ionization
  • Ions
  • Measurement
  • Microelectromechanical Systems
  • Particle Physics
  • Physics
  • Quantum Tunneling
  • Simulations
  • Thrusters

Fields of Study

  • Physics

Readers

  • Aerospace Propulsion Engineering.
  • Computational Fluid Dynamics (CFD)
  • Plasma Physics.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster