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Field evaporation ion source with possible application to electrostatic propulsionField evaporation of solid metal electrodes has been proposed as an ion source for an electrostatic propulsion device. The chief advantage over existing ion sources is the prospect of 100 percent fuel utilization efficiency. This advantage arises as a result of the elimination of the need for a gaseous precursor state for propellant ionization. The attainment of required high surface field strengths is achieved through field-induced extrusion of the electrode geometry at elevated temperatures. Contributions of both surface and bulk transport mechanisms are taken into account.
Document ID
19720005141
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Weizer, V. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-6593
E-6540
Report Number: NASA-TN-D-6593
Report Number: E-6540
Accession Number
72N12790
Funding Number(s)
PROJECT: RTOP 114-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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