DocumentCode
778676
Title
Plasma Electron Detector Using an Open Electron Multiplier
Author
Lind, D.L. ; McIlwraith, N.
Author_Institution
NASA-Goddard Space Flight Center, Greenbelt, Maryland
Volume
13
Issue
1
fYear
1966
Firstpage
511
Lastpage
514
Abstract
The Triaxial Electron Spectrometer, scheduled for flight on the OGO-E spacecraft, measures flux and energy distributions of electrons reaching the detector with from zero to 10 kilovolts energy. Electrons are analyzed in a curved-plate, electrostatic analyzer, and detected with a windowless continuous-dynode electron multiplier. The multiplier is operated in a constant-output, variablegain, current mode as the null detector in a feedback circuit. Five decades of dynamic range for flux measurements are obtained with a logarithmically compressed analog telemetry signal. Tests of the gain stability of two different channel multipliers have been made for periods of up to 850 hours. These tests indicate that the gain loss can be limited to a factor of two or three during the one year lifetime of the spacecraft.
Keywords
Circuit testing; Detectors; Electron multipliers; Electrostatic analysis; Electrostatic measurements; Energy measurement; Feedback circuits; Plasma measurements; Space vehicles; Spectroscopy;
fLanguage
English
Journal_Title
Nuclear Science, IEEE Transactions on
Publisher
ieee
ISSN
0018-9499
Type
jour
DOI
10.1109/TNS.1966.4324010
Filename
4324010
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