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High Power Demonstration of a 100 kW Nested Hall Thruster SystemThe XR-100 team successfully completed high power system testing of a Nested Hall Thruster system made up of the X3 Nested Hall Thruster, a modular Power Processing Unit, and a 5 valve Mass Flow Controller as the culmination of work performed under a NASA NextSTEP program. The test campaign attained several key firsts, including highest directly measured thrust of an electric propulsion (EP) string, highest demonstrated current of an EP string, and highest power operation of an EP string at thermal equilibrium published to date. Most importantly, the XR-100 system testing demonstrated that a 100 kW-class Nested Hall Thruster system has comparable performance and behavior to current state-of-the-art mid power Hall Thrusters, validating that the heritage technology can be scaled up to 100+ kW
Document ID
20190030503
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Shark, Sarah
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Hall, Scott J.
(Vantage Partners, LLC Brook Park, OH, United States)
Jorns, Benjamin
(Michigan Univ. (HQ) Ann Arbor, MI, United States)
Hofer, Richard R.
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Goebel, Dan M.
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Date Acquired
September 6, 2019
Publication Date
August 19, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN71845
Meeting Information
Meeting: AIAA Propulsion and Energy Forum and Exposition 2019
Location: Indianapolis, IN
Country: United States
Start Date: August 19, 2019
End Date: August 22, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
CONTRACT_GRANT: NNH16CP17C
WBS: 469947.04.99.22.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
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