Next-Generation Electric Propulsion Thrusters

Author:

Patterson Michael

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. 1Welander, B. "Life and Operating Range Extension of the BPT-4000 Qualification Model Hall Thruster," AIAA Paper2006-5263, 42nd JointPropulsion Conference, July2006.

2. 4Patterson, M.J. "NEXT Studyof Thruster Extended Performance (NEXT STEP)," AIAAPaper No. 2006-4664, 42nd Joint Propulsion Conferenceand Exhibit, Sacramento, CA,July2006.

3. 5Dankanich,J.W.andPolsgrove,T."MissionBenefitsofGriddedIonandHallThrusterHybridPropulsionSystems,"AIAA Paper No.2006-5162, 42nd JointPropulsion Conferenceand Exhibit, Sacramento, CA,July2006.

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1. A theoretical thrust density limit for Hall thrusters;Journal of Electric Propulsion;2023-03-30

2. The Limitation Analysis of Two Dimensional Magnetic Field Configuration in Annular Ion Thruster;International Journal of Aerospace Engineering;2022-04-21

3. Confinement characteristic of primary electrons with the variation of channel width in the discharge chamber of annular ion thruster;Chinese Journal of Aeronautics;2021-05

4. Advancements in the Demonstration of High Thrust to Power Ion Thruster Technology;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

5. Current Density Measurements of an Annular-Geometry Ion Engine;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

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