[1] Baird, Matthew. Designing an accessible hall effect thruster. 2016.
[2] A. Azimipanah, Kh. Alavi, B. Shokri. Plasma electrical hall effect thruster. in The 8th Annual Conference of Iranian Aerospace Society, Tehran, 2009.
[3] Myers, R. Solar electric propulsion: Introduction, applications and status, 2013.
[4] Hall, Scott. Characterization of a 100-kw class nestedchannel hall thruster. 2018.
[5] A.D.Galimore,A.F.Thurnau. Thephysicsofhall-effected thrusters, 2004.
[6] Boeuf, Jean-Pierre. Tutorial: Physics and modeling of hall thrusters. JournalofAppliedPhysics,121(1):011101,2017.
[7] McGrail, Scott and Parker, Sam. Preliminary design of a laboratory cylindrical hall-effect thruster. 2012.
[8] Kieckhafer, Alex and King, Lyon B. Energetics of propellant options for high-power hall thrusters. Journal of propulsion and power, 23(1):21–26, 2007.
[9] Jankovsky, Robert, Tverdokhlebov, Sergey, and Manzella, David. Highpowerhallthrusters. in35th Joint Propulsion Conference and Exhibit, p. 2949, 1999.
[10] Warner, Noah Zachary. Theoretical and experimental investigation of Hall thruster miniaturization. Ph.D. thesis, Massachusetts Institute of Technology, 2007.
[11] Khatry, Jivan, Aydogan, Fatih, Ilyas, Muhammad, and Houts, Michael. Designofapassivesafetysystemforanuclear thermal rocket. Annals of Nuclear Energy, 111:536– 553, 2018.
[12] Goebel, Dan M and Katz, Ira. Fundamentals of electric propulsion: ion and Hall thrusters, vol. 1. John Wiley & Sons, 2008.