Performance and High-Speed Characterization of a 100-kW Nested Hall Thruster
Author:
Affiliation:
1. Western Michigan University, Kalamazoo, MI 49008
2. Ohio Aerospace Institute, Brookpark, OH 44142
Funder
National Aeronautics and Space Administration
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38080
Reference29 articles.
1. HallS. J. “Characterization of a 100-kW Class Nested-Channel Hall Thruster,” Ph.D. Dissertation, Dept. of Aerospace Engineering, Univ. of Michigan, Ann Arbor, MI, 2018.
2. Mass and Cost Model for Selecting Thruster Size in Electric Propulsion Systems
3. Hall Thruster Cathode Flow Impact on Coupling Voltage and Cathode Life
4. ManzellaD. “Scaling Hall Thrusters to High Power,” Ph.D. Dissertation, Dept. of Mechanical Engineering, Stanford Univ., Stanford, CA, 2005.
5. Performance Test Results of the NASA-457M v2 Hall Thruster
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