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Electric Propulsion Technology Development for the Jupiter Icy Moons Orbiter ProjectDuring 2004, the Jupiter Icy Moons Orbiter project, a part of NASA's Project Prometheus, continued efforts to develop electric propulsion technologies. These technologies addressed the challenges of propelling a spacecraft to several moons of Jupiter. Specific challenges include high power, high specific impulse, long lived ion thrusters, high power/high voltage power processors, accurate feed systems, and large propellant storage systems. Critical component work included high voltage insulators and isolators as well as ensuring that the thruster materials and components could operate in the substantial Jupiter radiation environment. A review of these developments along with future plans is discussed.
Document ID
20050041919
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Date Acquired
September 7, 2013
Publication Date
December 1, 2004
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-14737
NASA/TM-2004-213290
Paper AIAA 2004-3449
Report Number: E-14737
Report Number: NASA/TM-2004-213290
Report Number: Paper AIAA 2004-3449
Meeting Information
Meeting: 40th Joint Propulsion Conference and Exhibit
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2001
End Date: July 14, 2001
Sponsors: American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Society for Electrical Engineers
Funding Number(s)
WBS: WBS 22-982-10-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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