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High-Power Performance of a 100-kW Class Nested Hall ThrusterOperations of a three-channel 100-kW class nested Hall thruster at total power levels from 5 to 102 kW and discharge currents from 16 to 247 A were successful. The thruster was operated in all seven available channel combinations at discharge voltages of 300, 400, and 500 V and at current densities that were 0.60 and 0.95 of the nominal value. Additional test points were also collected at 1.20 the nominal current density. The thruster was throttled through a total of forty-six unique operating conditions. At each condition, thruster performance was measured using a high-power thrust stand designed to measure up to 8 N of thrust. From these thrust measurements, specific impulse and efficiency were calculated. All seven channel combinations showed similar performance at a given discharge voltage and current density. The largest thrust recorded was 5.42 N at 99 kW, 400 V discharge voltage. Total efficiency values 0.54 to 0.67, and total specific impulse ranged from 1800 seconds to 2650 seconds. Discharge current oscillations were also measured. Generally these oscillations increased on the inner and middle channels during multi-channel mode but stayed roughly a constant fraction of the channel discharge current for the outer channel in both single- and multi-channel operation. We also found that the thrust of the three channels firing together was not significantly higher than the sum of each channel _ring individually, a result that differs from what was found previously for nested Hall thrusters.
Document ID
20180004543
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Hall, Scott J.
(Michigan Univ. Ann Arbor, MI, United States)
Jorns, Benjamin A.
(Michigan Univ. Ann Arbor, MI, United States)
Gallimore, Alec D.
(Michigan Univ. Ann Arbor, MI, United States)
Kamhawi, Hani
(NASA Glenn Research Center Cleveland, OH, United States)
Haag, Thomas W.
(NASA Glenn Research Center Cleveland, OH, United States)
Mackey, Jonathan A.
(NASA Glenn Research Center Cleveland, OH, United States)
Gilland, James H.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Peterson, Peter Y.
(Vantage Partners, LLC Cleveland, OH, United States)
Baird, Matthew J.
(University of Western Michigan Kalamazoo, MI, United States)
Date Acquired
August 20, 2018
Publication Date
October 11, 2017
Subject Category
General
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN47556
Report Number: GRC-E-DAA-TN47556
Meeting Information
Meeting: International Electric Propulsion Conference (IEPC)
Location: Atlanta, GA
Country: United States
Start Date: October 8, 2017
End Date: October 12, 2017
Sponsors: Aerojet Rocketdyne, Inc.
Funding Number(s)
WBS: WBS 729200.06.03.05.01
CONTRACT_GRANT: NNX14AL67H
CONTRACT_GRANT: NNH16CP17C
CONTRACT_GRANT: NNX16AM96H
Distribution Limits
Public
Copyright
Public Use Permitted.
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