A Vacuum Arc Ion Thruster for Space Propulsion

Abstract

The Phase I project has demonstrated the feasibility of a 500 W vacuum arc ion thruster (VAIT) that is very different from present Xe ion thrusters that are in production for space missions. The VAIT does not require storage and feed of gases, reducing the parts count considerably. The VAIT produces a highly ionized plasma with minimal neutral build up in the grids, potentially making the grid lifetime longer and potentially allowing smaller grid spacing to be used. The VAIT has been shown (in related research over two decades) to produce plasmas (hence directed ion beams) of dozens of heavy ions such as Ba, La, Ce, Pr, Nd, Sm, Gd, Dy, Ho, Er, Tm, Yb, H(Ta, W, Ir, Pt, Au, Pb, Bi, Th and U. This wide range of possible ions provides great flexibility to the VAIT, allowing us to tailor different ion beams (with different thrust, specific impulse levels) to different missions. Ion streaming velocities of 5 x 104 rn/s were measured using Time-of-Flight (TOF) methods, which imply a thrust level of 0.13 N.

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Document Details

Document Type
Technical Report
Publication Date
Mar 31, 1998
Accession Number
ADA342818

Entities

People

  • Aleksei Vizir
  • Mahadevan Krishnan
  • Niansheng Qi
  • Rahul R. Prasad
  • Steve Gensler

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Current Density
  • Electric Arcs
  • Electric Propulsion
  • Energy Efficiency
  • Ion Beams
  • Ion Propulsion
  • Ion Thrusters
  • Ions
  • Materials
  • Materials Science
  • Measurement
  • Propulsion Systems
  • Repetition Rate
  • Space Propulsion
  • Specific Impulse
  • Thrust
  • Thrusters

Fields of Study

  • Physics

Readers

  • Analytical Mechanics
  • Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Space
  • Space - Hall-Effect Thruster