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EMI characteristics of a potential control systemWith the development and use of charged particle sources for controlling spacecraft potentials there is a need to better understand the effects of these systems on spacecraft operations. The emission of charged particles perturbs the spacecraft environment and signals are generated which may interfere with other vehicle functions. In particular, the generated signals are apt to interfere with detectors for observing waves that exist naturally in the space environment. Examples of this type of interference are presented from the SCATHA satellite during a period when the vehicle was highly charged. A plasma source on board the spacecraft succeeded in discharging the vehicle with each of four different operating modes. The VLF broadband receiver on SCATHA detected interference over the entire 0-5 kHz range of both the electric and magnetic field detectors during these charged particle emissions. This frequency range includes the 2 kHz electron gyrofrequency but is below the 9 kHz electron plasma frequency. The observations suggest that interference occurs through introduction of anomalous signals, and through suppression of background field measurements.
Document ID
19850014191
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Donatelli, D. E.
(Boston Coll. Chestnut Hill, MA, United States)
Cohen, H. A.
(AFGL Los Angeles, United States)
Burke, W. J.
(AFGL)
Koons, H. C.
(Aerospace Corp.)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Publication Information
Publication: NASA. Lewis Research Center Spacecraft Environ. Interactions Technol., 1983
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N22502
Funding Number(s)
CONTRACT_GRANT: F19628-81-K-0011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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