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Inert gas ion thrusterInert gas performance with three types of 12 cm diameter magnetoelectrostatic containment (MESC) ion thrusters was tested. The types tested included: (1) a hemispherical shaped discharge chamber with platinum cobalt magnets; (2) three different lengths of the hemispherical chambers with samarium cobalt magnets; and (3) three lengths of the conical shaped chambers with aluminum nickel cobalt magnets. The best argon performance was produced by a 8.0 cm long conical chamber with alnico magnets. The best xenon high mass utilization performance was obtained with the same 8.0 cm long conical thruster. The hemispherical thruster obtained 75 to 87% mass utilization at 185 to 205 eV/ion of singly charged ion equivalent beam.
Document ID
19820013378
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ramsey, W. D.
(Xerox Electro-Optical Systems Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
REPT-2372-5009
NAS 1.26:165521
NASA-CR-165521
Report Number: REPT-2372-5009
Report Number: NAS 1.26:165521
Report Number: NASA-CR-165521
Accession Number
82N21252
Funding Number(s)
CONTRACT_GRANT: NAS3-21345
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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