1 edition of Extended test of a xenon hollow cathode for a space plasma contactor found in the catalog.

Extended test of a xenon hollow cathode for a space plasma contactor

from Mainz and Bamberg to Westminster and St. Albans : One hundreed incunabula and manuscripts important for the development of printing, with 2 color plates, 35 half tones, and 45 line cuts

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Published by Administrator in National Aeronautics and Space Administration

    Places:
  • United States
    • Subjects:
    • National Aeronautics and Space Administration


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      • Distributed to depository libraries in microfiche.Shipping list no.: 95-0267-M.Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.

        StatementNational Aeronautics and Space Administration
        PublishersNational Aeronautics and Space Administration
        Classifications
        LC Classifications1994
        The Physical Object
        Paginationxvi, 54 p. :
        Number of Pages42
        ID Numbers
        ISBN 10nodata
        Series
        1
        2NASA contractor report -- NASA CR-195402.
        3NASA contractor report -- 195402.

        nodata File Size: 4MB.


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Extended test of a xenon hollow cathode for a space plasma contactor by National Aeronautics and Space Administration Download PDF EPUB FB2


National Aeronautics and Space Administration. 26:189227 Aboriginal, Torres Strait Islander and other First Nations people are advised that this catalogue contains names, recordings and images of deceased people and other content that may be culturally sensitive. National Aeronautics and Space Administration. Implementation of a hollow cathode plasma contactor for charge control on the Space Station has required validation of long-life hollow cathodes.

[PDF] Multiple Hollow Cathode Wear Testing for the Space Station Plasma Contactor

These objectives were achieved by wear testing four cathodes…. : National Technical Information Service, distributor, 1992] 1 v. A test series of hollow cathodes and hollow cathode plasma contactors was initiated as part of the plasma contactor development program. Continuing life test of a xenon hollow cathode for a space plasma contactor Implementation of a hollow cathode plasma contactor for charge control on the Space Station has required validation of long-life hollow cathodes.

: National Aeronautics and Space Administration], 1992. Extended-testing of Xenon ion thruster hollow cathodes. Catalogue Persistent Identifier APA Citation Sarver-Verhey, Timothy R. A test series of hollow cathodes and hollow cathode plasma contactors was initiated as part of the plasma contactor development program. The discharge has experienced 10 shutdowns during the test, all of which were due to test facility failures or expellant replenishment.

National Aeronautics and Space Administration. An on-going wear-test of a hollow cathode has demonstrated cathode operation in excess of 4700 hours with small changes in operating parameters. In all cases, the cathode was re-ignited at approximately 42 volts and resumed typical operation. The discharge experienced 4 shutdowns during the test, all of which…. This test represents the longest demonstrated stable operation of a high current greater than 1 A xenon hollow cathode reported to date.

An on-going wear-test of a hollow cathode has demonstrated cathode operation in excess of 4700 hours with small changes in operating parameters. Sarver-Verhey National Aeronautics and Space Administration ; National Technical Information Service, distributor [Washington, DC] : [Springfield, Va Wikipedia Citation Please see for further citation fields that may be required.

Sarver-Verhey Book Bib ID 4054250 Format Microform, BookAuthor Description [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va.

Continuing life test of a xenon hollow cathode for a space plasma contactor

A wear test of four hollow cathodes was conducted to resolve issues associated with the Space Station plasma contactor. This test represents the longest demonstrated stable operation of a high current greater than 1A xenon hollow cathode reported to date. In all cases, the cathode was reignited at approximately 42 volts and resumed typical operation.