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A 5-kW xenon ion thruster lifetestThe results of the first life test of a high power ring-cusp ion thruster are presented. A 30-cm laboratory model thruster was operated steady-state at a nominal beam power of 5 kW on xenon propellant for approximately 900 hours. This test was conducted to identify life-timing erosion modifications, and to demonstrate operation using simplified power processing. The results from this test are described including the conclusions derived from extensive post-test analyses of the thruster. Modifications to the thruster and ground support equipment, which were incorporated to solve problems identified by the lifetest, are also described.
Document ID
19910009867
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patterson, Michael J.
(NASA Lewis Research Center Cleveland, OH., United States)
Verhey, Timothy R.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-103191
AIAA PAPER 90-2543
NAS 1.15:103191
E-5579
Report Number: NASA-TM-103191
Report Number: AIAA PAPER 90-2543
Report Number: NAS 1.15:103191
Report Number: E-5579
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Orlando, FL
Country: United States
Start Date: July 18, 1990
End Date: July 20, 1990
Sponsors: JSASS, DGLR, AIAA
Accession Number
91N19180
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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