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Simulation of an ion thruster control systemThe results of an initial effort to model the control loops of a 30-cm diameter electron bombardment thruster and a transistorized power processor predicting its operation were described. Data from which the model is made is presented as well as comparisons between the computer outputs and test data from the JPL Solar Electric Propulsion systems laboratory.
Document ID
19760014190
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kudo, I. (Electrotech. Lab. Tokyo, United States)
Pless, L. C. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pawlik, E. V. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
February 15, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
JPL-TM-33-755
NASA-CR-146580
Report Number: JPL-TM-33-755
Report Number: NASA-CR-146580
Accession Number
76N21278
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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