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A doubly charged ion model for ion thrustersA theoretical equilibrium model of doubly charged ion production and loss processes in electron bombardment ion thrusters is presented. The model is shown to predict double ion density levels accurately for 15 and 30 cm diameter thrusters operating with several different grid sets and at several different power levels. The model indicates the dominant mechanism of double ion production involves the singly charged ground state. This result is used to develop a much simpler model which, along with correlations of the average plasma properties, can be used to determine the double ion density in thrusters with acceptable accuracy.
Document ID
19770030148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Peters, R. R.
(Colorado State Univ. Fort Collins, CO, United States)
Wilbur, P. J.
(Colorado State University Fort Collins, Colo., United States)
Vahrenkamp, R. P.
(Hughes Research Laboratories Malibu, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
November 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-1010
Report Number: AIAA PAPER 76-1010
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Key Biscayne, FL
Start Date: November 14, 1976
End Date: November 17, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A13000
Funding Number(s)
CONTRACT_GRANT: NGR-06-002-112
CONTRACT_GRANT: NAS3-19703
Distribution Limits
Public
Copyright
Other

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