NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Characterizing Electrical Arc Behavior in Ion EnginesTest results using an engineering model Advanced NEXT thruster are presented to identify different arc types utilizing ground test hardware. Three distinct arc types were observed: grid-to-grid arcs, high voltage-to-chassis arcs, and a combination of both. The frequency of high voltage-to-chassis arcs ranged from 4-30%, depending on operating conditions and hardware configuration. Higher beam currents were typically associated with more frequent high voltage-to-chassis arcs. During these arcs, the measured chassis current levels ranged from 20-70 A, however a significant portion of the output beam current returned to the beam supply via the neutralizer cathode plasma, which may be a ground test facility effect. The paper also discusses conducted susceptibility tests that can be performed at the spacecraft level to address the transients associated with arcing events.
Document ID
20240014086
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Robert E Thomas
(Glenn Research Center Cleveland, United States)
Rittu S Raju
(HX5, LLC)
James J Bontempo
(ZIN Technologies (United States) Cleveland, United States)
Date Acquired
November 6, 2024
Subject Category
Spacecraft Design, Testing and Performance
Spacecraft Propulsion and Power
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: SpaceDoc SAA3-1711
WBS: 966826.02.03.1724.24
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
electric propulsion
gridded ion engines
spacecraft interactions
No Preview Available