CONDENSATION COLLOIDAL ION SOURCE.

Abstract

The report describes the experimental and analytical efforts on the evaluation of the controlled-growth, condensation colloidal ion source concept as a means of producing propellant particles for use in an electrostatic ion engine. An improved concept is presented which depends on convection rather than radiation for cooling the particles and assumes the presence of electrons in the nozzle. These factors relieve space charge restrictions but necessitate removal of electrons downstream from the throat and increase the requirements for collisions. Design considerations to provide the necessary conditions are discussed and were incorporated in the construction of a controlled-growth colloidal ion engine which performed well in thrust tests. Theoretical analyses show that sodium or lithium could give the performance required of a colloidal ion engine if neutral nucleation is insignificant. Detailed experimental studies of nozzles and ionizers are described which indicate that the skimmer nozzle and a free arc ionizer can best fulfill the requirements of the colloidal ion source. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 12, 1964
Accession Number
AD0602115

Entities

People

  • A. Lucille Cox
  • S. Graybill
  • S. Harrison

Tags

DTIC Thesaurus Topics

  • Charged Particles
  • Collisions
  • Condensation
  • Construction
  • Convection
  • Corpuscular Radiation
  • Electromagnetic Radiation
  • Electrons
  • Elementary Fermions
  • Elementary Particles
  • Engines
  • Ion Engines
  • Ion Sources
  • Ions
  • Particles
  • Radiation
  • Space Charge

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Plasma Physics.
  • Systems Analysis and Design

Technology Areas

  • Microelectronics
  • Space
  • Space - Hall-Effect Thruster