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Improvement of ion thruster designTwo types of measurements were performed on ion thrustors equipped with SmCo magnets in either ring cusp or line cusp arrangements. Langmuir probes were used to measure plasma potential, electron density, and electron temperture in all regions inside the thruster. Loss fluxes to various surfaces were determined by measuring the currents to foils attached to or imbedded in the surface. Data were obtained for several sets of discharge voltages and currents. The loss currents were determined from current vs voltage characteristics observed on a transistor curve tracer oscilloscope. Both ion and electron currents were measured to all parts of the walls and to all parts of the cathode assembly using collecting plates. These measurement were also made for various parameter sets. In line cusp configuration the plasma density is essentially as predicted by existing calculations. In the ring cusp arrangement the interior of the plasma contains an inhomogeneous and relatively large magnetic field so the geometry is decidely two-dimensional and the models of Self (1967) and of Kino and Sham (1966) do not agree.
Document ID
19860017947
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carpenter, R. T.
(Iowa Univ. Iowa City, IA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:177223
NASA-CR-177223
Accession Number
86N27419
Funding Number(s)
CONTRACT_GRANT: NAG3-206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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