Webthrusters.11,12,13 Knowledge gained from applying magnetic shielding circuit design approach in these two Hall thrusters is leveraged in the design and construction of the 12.5-kW Hall thruster. This paper provides an overview of the 12.5-kW Technology Development Unit (TDU) Hall thruster development activity and the planned thruster test campaign. Web10 Mar 2024 · Magnetic shielding (MS) of a Hall effect thruster (HET) chamber has been proven an effective technique to limit both wall erosion, due to high-energy ion …
The KM-10 Hall-Effect Thruster: Development Status and …
Web18 Feb 2024 · S. E. Cusson, R. Hofer, R. Lobbia, B. Jorns, and A. Gallimore, “ Performance of the H9 magnetically shielded Hall thrusters,” in Proceedings of the 35th International … WebThe results from the acceptance and performance tests of three laboratory-model, 9kW, magnetically-shielded Hall thrusters are presented. These thrusters, built through a joint development program led by the Jet Propulsion Laboratory in collaboration with the University of Michigan and the Air Force Research Laboratory, are intended to serve as … george washington mba
Performance at High Current Densities of a Magnetically-Shielded Hall …
Web25 Jul 2016 · The Hall Effect Rocket with Magnetic Shielding (HERMeS) is a 12.5 kW magnetically shielded Hall thruster presently under development for deep-space missions. A development model HERMeS thruster,… Expand 6 Correction: Ion Velocity in the Discharge Channel and Near-Field of the HERMeS Hall Thruster Wensheng Huang, H. Kamhawi, D. … Web9 Jul 2024 · The Hall Effect Rocket with Magnetic Shielding (HERMeS) is a 12.5 kW magnetically shielded Hall thruster presently under development for deep-space missions. A development model HERMeS thruster, TDU-2, with borosilicate channel walls, has successfully undergone proto-qualification testing including random vibration and thermal … Web20 Jul 2024 · This study systematically investigated the influence of the position and inclination angle of an externally mounted hollow cathode in 1.35 kW magnetically shielded Hall thrusters to establish the relationship between thruster performance, plume state, and cathode placement. george washington medical school match list