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Electromagnetic interference assessment of an ion drive electric propulsion systemAn electric propulsion thrust system has the capability of providing a high specific impulse for long duration scientific missions in space. The EMI from the elements of an ion engine was characterized. The compatibility of ion drive electric propulsion systems with typical interplanetary spacecraft engineering was predicted.
Document ID
19810008616
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Whittlesey, A. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 15, 1981
Publication Information
Publication: Exptl. and Anal. Evaluation of Ion Thruster(Spacecraft Interactions
Subject Category
Spacecraft Propulsion And Power
Accession Number
81N17136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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