1. Hofer, R., Kamhawi, H., Herman, D., et al., Development approach and status of the 12.5 kW HERMeS Hall thruster for the solar electric propulsion technology demonstration mission, 30th International Symposium on Space Technology and Science 34th International Electric Propulsion Conference and 6th Nano-satellite Symposium, Kobe, Hyogo, Japan, 2015, paper IEPC-2015-186.
2. Williams, G.J., Jr., Gilland, J.H., Peterson, P.Y., et al., Wear testing of the HERMeS thruster, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, Salt Lake City, USA, 2016, paper AIAA 2016–2025.
3. Hofer, R.R., Cusson, S.E., Lobbia, R.B., and Gallimore, A.D., The H9 magnetically shielded Hall thruster, 35th International Electric Propulsion Conference, Atlanta, GA, USA, 2017, paper IEPC-2017-232.
4. Shashkov, A.S. and Lovtsov, A.S., Laboratory tests of 10.5 kW Hall thruster and 42 kW cluster, 71st International Astronautical Congress (IAC), The CyberSpace Edition, October 12–14, 2020.
5. Ostrivsky, V.G., Smolentsev, A.A., and Sokolov, B.A., The experience of the creation of electric propulsion thrusters with high power in “S.P. Korolev Rocket and Space Corporation Energia,” Electron. J. Proc. Moscow Aviation Inst., 2002, no. 60.