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Spacecraft mass spectrometer ion source employing field emission cathodesAn ion source that utilizes a pair of thin-film field emission cathodes to provide current for electric impact ionization is studied. The field emission cathodes are composed of microscopically small needle tips and an extraction electrode; the cathodes generate a 200-eV, 0.1-mA electron beam. The multistep process for the manufacturing of the field emission cathodes is examined. The operation of the ion source, which ionizes atoms and molecules that enter the mass spectrometer with a ram velocity of about 80 km/sec, is described.
Document ID
19860052662
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Curtis, C. C.
(Arizona Univ. Tucson, AZ, United States)
Hsieh, K. C.
(Arizona, University Tucson, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: Review of Scientific Instruments
Volume: 57
ISSN: 0034-6748
Subject Category
Spacecraft Instrumentation
Accession Number
86A37400
Funding Number(s)
CONTRACT_GRANT: NASW-3627
Distribution Limits
Public
Copyright
Other

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