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12-kW Advanced Electric Propulsion System Hall Current Thruster Qualification and Production StatusInitial developments by the National Aeronautics and Space Administration (NASA) of a 12-kW-class Hall thruster began with maturation of the Hall Effect Rocket with Magnetic Shielding, which was then transitioned to industry via the Advanced Electric Propulsion System contract. This contract was awarded to Aerojet Rocketdyne (now part of L3Harris)in 2016 with the goal of developing and fully qualifying a 12 kW Hall thruster for NASA and commercial applications, with its first intended use on the Power and Propulsion Element as part of NASA’s Gateway lunar space station. This paper describes the status of the contract, including production and qualification efforts after the thruster design successfully passed Critical Design Review in 2022, as well as NASA-led independent testing in support of development and qualification. To-date, the first qualification thruster has successfully undergone pre-environmental characterization testing, qualification vibration and shock testing, with preparations for thermal vacuum testing underway at time of writing. Additional qualification testing of components such as the cathode, magnet coils, and thermal components are ongoing to demonstrate design robustness of these critical thruster elements. Flight hardware fabrication and testing is expected to be completed by 2025, at which point the hardware will be delivered to Maxar Technologies for integration and use on the Power and Propulsion Element spacecraft.
Document ID
20250003901
Acquisition Source
Glenn Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Rohit Shastry
(Glenn Research Center Cleveland, United States)
Hani Kamhawi
(Glenn Research Center Cleveland, United States)
Jason D Frieman
(Glenn Research Center Cleveland, United States)
George C Soulas
(Glenn Research Center Cleveland, United States)
Timothy G Gray
(Glenn Research Center Cleveland, United States)
Timothy R Verhey
(Glenn Research Center Cleveland, United States)
Clayton D Kachele
(Glenn Research Center Cleveland, United States)
George J Williams
(Glenn Research Center Cleveland, United States)
Nagual A Simmons
(HX5, LLC)
Robert B Lobbia
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Steven M Arestie
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Vernon H Chaplin
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Jack Fisher
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Gabriella Blackner
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Eleanor Forbes
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Jack Hondagneu
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Nicholas A Branch
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Jonathan M Zubair
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Hannah Watts
(Aerojet Rocketdyne, Inc. Redmond, WA, United States)
Date Acquired
April 18, 2025
Publication Date
May 5, 2025
Publication Information
Publication: Journal of Electric Propulsion
Publisher: Springer Nature
e-ISSN: 2731-4596
Subject Category
Spacecraft Propulsion and Power
Funding Number(s)
CONTRACT_GRANT: 80NM0018D0004
CONTRACT_GRANT: NNC16CA21C
WBS: 729200.01.03
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
electric propulsion
Hall thruster
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