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Environmental Testing of the NEXT PM1 Ion EngineThe NEXT propulsion system is an advanced ion propulsion system presently under development that is oriented towards robotic exploration of the solar system using solar electric power. The Prototype Model engine PM1 was subjected to qualification-level environmental testing to demonstrate compatibility with environments representative of anticipated mission requirements. Random vibration testing, conducted with the thruster mated to the breadboard gimbal, was executed at 10.0 Grms for 2 minutes in each of three axes. Thermal-vacuum testing included a deep cold soak of the engine to temperatures of -168 C and thermal cycling from -120 to 203 C. Although the testing was largely successful, several issues were identified including the fragmentation of potting cement on the discharge and neutralizer cathode heater terminations during vibration which led to abbreviated thermal testing, and generation of particulate contamination from manufacturing processes and engine materials. Thruster performance was nominal throughout the test program, with minor variations in some engine operating parameters likely caused by facility effects. In general, the NEXT PM1 engine and the breadboard gimbal were found to be well-designed against environmental requirements based on the results reported herein. After resolution of the findings from this test program the hardware environmental qualification program can proceed with confidence.
Document ID
20080012738
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Synder, John S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Anderson, John R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
VanNoord, Jonathan L.
(NASA Glenn Research Center Cleveland, OH, United States)
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-16186
AIAA Paper 2007-5275
NASA/TM-2008-215014
Report Number: E-16186
Report Number: AIAA Paper 2007-5275
Report Number: NASA/TM-2008-215014
Meeting Information
Meeting: 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Cincinnati, OH
Country: United States
Start Date: July 8, 2007
End Date: July 11, 2007
Sponsors: American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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