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Puncture discharges in surface dielectrics as contaminant sources in spacecraft environments

Author
Hazelton, R. C.
Published
JAN 1, 1978.
Physical Description
1 electronic document
Additional Creators
Yadlowsky, E. J. and Churchill, R. J.
Online Version

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Unclassified, Unlimited, Publicly available.
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Summary
Spacecraft in geosynchronous orbits are known to become charged to large negative potentials during the local midnight region of the satellite orbit. Such discharges have been studied by the electron beam irradiation of dielectric samples in a vacuum environment. In addition to static measurements and photographic examination of the puncture discharges in Teflon samples, the transient characteristics of the electrical discharges are determined from oscillographs of voltage and current and by charged particle measurements employing a biased Faraday cup and a retarding potential analyzer. Using these latter techniques, studies of angular and energy distributions of charged particles have indicated an initial burst of high energy electrons (5 x 10 to the 13th power per discharge at energies greater than 300 eV) followed by a less intense burst of lower energy negative particles. Positive ions are emitted from the discharge site in an initial high velocity burst followed by a lower velocity burst tentatively identified as carbon.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19780016516.
Accession ID: 78N24459.
NASA-CR-157105.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15728846