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Dynamic characteristics of a 30-centimeter mercury ion thrusterThe present work reports on measurements of the fluctuations in the beam current, discharge current, neutralizer keeper current, and discharge voltage of a 30-cm ion thruster made with 60Hz laboratory-type power supplies. The intensities of the fluctuations (ratio of the root-mean-square magnitude to time-average quantity) were found to depend significantly on the beam and magnetic baffle currents. The shape of the frequency spectra of the discharge plasma fluctuations was related to the beam and magnetic baffle currents. The predominant peaks of the beam and discharge current spectra occurred at frequencies less than 30 kilohertz. This discharge chamber resonance could be attributable to ion-acoustic wave phenomena. Cross-correlations of the discharge and beam currents indicated that the dependence on the magnetic baffle current was strong. The measurements revealed that the discharge current fluctuations directly contribute to the beam current fluctuations and that the power supply characteristics can modify these fluctuations.
Document ID
19750040881
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Serafini, J. S.
Mantenieks, M. A.
Rawlin, V. K.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 75-345
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Electric Propulsion Conference
Location: New Orleans, LA
Start Date: March 19, 1975
End Date: March 21, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A24953
Distribution Limits
Public
Copyright
Other

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