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NEXT Ion Engine 2000 Hour Wear Test ResultsThe results of the NEXT 2000 h wear test are presented. This test was conducted with a 40 cm engineering model ion engine, designated EM1, at a 3.52 A beam current and 1800 V beam power supply voltage. Performance tests, which were conducted over a throttling range of 1.1 to 6.9 kW throughout the wear test, demonstrated that EM1 satisfied all thruster performance requirements. The ion engine accumulated 2038 h of operation at a thruster input power of 6.9 kW, processing 43 kg of xenon. Overall ion engine performance, which includes thrust, thruster input power, specific impulse, and thrust efficiency, was steady with no indications of performance degradation. The ion engine was also inspected following the test. This paper presents these findings.
Document ID
20050060719
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH, United States)
Kamhawi, Hani
(NASA Glenn Research Center Cleveland, OH, United States)
Patterson, Michael J.
(NASA Glenn Research Center Cleveland, OH, United States)
Britton, Melissa A.
(QSS Group, Inc. Cleveland, OH, United States)
Frandina, Michael M.
(QSS Group, Inc. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2004-3791
NASA/TM-2004-213222
E-14729
Report Number: AIAA Paper 2004-3791
Report Number: NASA/TM-2004-213222
Report Number: E-14729
Meeting Information
Meeting: 40th Joint Propulsion Conference and Exhibit by the AIAA, ASME, SAE, and ASEE
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
WBS: WBS 22-800-50-01
Distribution Limits
Public
Copyright
Public Use Permitted.
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