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A Segmented Ion-Propulsion EngineNew design approach for high-power (100-kW class or greater) ion engines conceptually divides single engine into combination of smaller discharge chambers integrated to operate as single large engine. Analogous to multicylinder automobile engine, benefits include reduction in required accelerator system span-to-gap ratio for large-area engines, reduction in required hollow-cathode emission current, mitigation of plasma-uniformity problem, increased tolerance to accelerator system faults, and reduction in vacuum-system pumping speed.
Document ID
19920000378
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Brophy, John R.
(Caltech)
Date Acquired
August 15, 2013
Publication Date
June 1, 1992
Publication Information
Publication: NASA Tech Briefs
Volume: 16
Issue: 6
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
NPO-18192
Accession Number
92B10378
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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