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Ring-cusp ion thruster with shell anodeAn improved ion thruster for low specific impulse operation in the 1500 sec to 6000 sec range has a multicusp boundary field provided by high strength magnets on an iron anode shell which lengthens the paths of electrons from a hollow cathode assembly. A downstream anode pole piece in the form of an iron ring supports a ring of magnets to provide a more uniform beam profile. A cylindrical cathode magnet can be moved selectively in an axial direction along a feed tube to produce the desired magnetic field at the cathode tip.
Document ID
19850012946
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Sovey, J. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Rawlin, V. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Roman, R. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
August 21, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.71:LEW-13881-1
Patent Number: NASA-CASE-LEW-13881-1
Report Number: NAS 1.71:LEW-13881-1
Patent Application Number: US-PATENT-APPL-SN-473498
Patent Number: US-PATENT-4,466,242
Accession Number
85N21256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-13881-1|US-PATENT-4,466,242
Patent Application
US-PATENT-APPL-SN-473498
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