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Ion thruster charge-exchange plasma flowThe electron bombardment ion thruster has been under development for a number of years and during this time, studies of the plasmas produced by the thrusters and their interactions with spacecraft have been evaluated, based on available data. Due to diagnostic techniques used and facility effects, there is uncertainty as to the reliability of data from these early studies. This paper presents data on the flow of the charge-exchange plasma produced just downstream of the thruster's ion optics. The 'end-effect' of a cylindrical Langmuir probe is used to determine ion density and directed ion velocity. Results are compared with data obtained from a retarding potential analyzer-Faraday cup.
Document ID
19820036267
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carruth, M. R., Jr.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Gabriel, S. B.
(California Institute of Technology, Jet Propulsion Laboratory, Electrical Power and Propulsion Section, Pasadena CA, United States)
Kitamura, S.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena, CA; National Aerospace Laboratory Tokyo, Japan)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 82-0403
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A19802
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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