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Post-Test Inspection of NASA's Evolutionary Xenon Thruster Long-Duration Test Hardware: Discharge and Neutralizer CathodesThe NEXT Long-Duration Test is part of a comprehensive thruster service life assessment intended to demonstrate overall throughput capability, validate service life models, quantify wear rates as a function of time and operating condition, and identify any unknown life-limiting mechanisms. The test was voluntarily terminated in April 2014 after demonstrating 51,184 hours of high-voltage operation, 918 kg of propellant throughput, and 35.5 MN-s of total impulse. The post-test inspection of the thruster hardware began shortly afterwards with a combination of non-destructive and destructive analysis techniques, and is presently nearing completion. This presentation presents relevant results of the post-test inspection for both discharge and neutralizer cathodes.
Document ID
20170002725
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Shastry, Rohit
(NASA Glenn Research Center Cleveland, OH United States)
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
March 31, 2017
Publication Date
July 25, 2016
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN34105
Report Number: GRC-E-DAA-TN34105
Meeting Information
Meeting: 52nd AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
WBS: WBS 336763.01.05.02.04.05.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Lifetime
Electric Propulsion
Ion Thrusters
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