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Hollow cathode and keeper-region plasma measurementsThe successful performance of the NSTAR ion thruster in Deep Space 1 mission, coupled with the recently completed 30,032 hour life test of the flight spare thruster, has accelerated with the implementation of electric propulsion in NASA missions.
Document ID
20060043476
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Jameson, Kristina K.
Goebel, Dan M.
Watkins, Ron M.
Date Acquired
August 23, 2013
Publication Date
July 1, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2005-3667
Meeting Information
Meeting: 41st AIAA Joint Propulsion Conference
Location: Tuscon, AZ
Country: United States
Start Date: July 10, 2005
End Date: July 13, 2005
Distribution Limits
Public
Copyright
Other
Keywords
plasma density
ion thruster
electric propulsion

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