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Segmented ion thrusterApparatus and methods for large-area, high-power ion engines comprise dividing a single engine into a combination of smaller discharge chambers (or segments) configured to operate as a single large-area engine. This segmented ion thruster (SIT) approach enables the development of 100-kW class argon ion engines for operation at a specific impulse of 10,000 s. A combination of six 30-cm diameter ion chambers operating as a single engine can process over 100 kW. Such a segmented ion engine can be operated from a single power processor unit.
Document ID
19940016023
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Brophy, John R.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Date Acquired
August 16, 2013
Publication Date
December 14, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-934988
Patent Number: US-PATENT-5,269,131
Patent Number: NASA-CASE-NPO-18192-1-CU
Accession Number
94N20496
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,269,131|NASA-CASE-NPO-18192-1-CU
Patent Application
US-PATENT-APPL-SN-934988
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