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Design, fabrication and testing of porous tungsten vaporizers for mercury ion thrustersThe dispersions in the characteristics, performance and reliability of vaporizers for early model 30-cm thrusters were investigated. The purpose of the paper is to explore the findings and to discuss the approaches that were taken to reduce the observed dispersion and present the results of a program which validated those approaches. The information that is presented includes porous tungsten materials specifications, a discussion of assembly procedures, and a description of a test program which screens both material and fabrication processes. There are five appendices providing additional detail in the areas of vaporizer contamination, nitrogen flow testing, bubble testing, porosimeter testing, and mercury purity. Four neutralizers, seven cathodes and five main vaporizers were successfully fabricated, tested, and operated on thrusters. Performance data from those devices is presented and indicates extremely repeatable results from using the design and fabrication procedures.
Document ID
19830014047
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Zavesky, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Kroeger, E.
(NASA Lewis Research Center Cleveland, OH, United States)
Kami, S.
(Hughes Research Labs. Malibu, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:83063
E-1534
NASA-TM-83063
Report Number: NAS 1.15:83063
Report Number: E-1534
Report Number: NASA-TM-83063
Accession Number
83N22318
Funding Number(s)
PROJECT: RTOP 542-05-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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