A Plasma-to-Engineering Design Framework for Electrical, Thermal, and Mechanical Constraints in Hall-Effect Thrusters
Hall-Effect thrusters (HETs) have emerged as the primary electric propulsion system for compact spacecraft and satellites. Because of their high-temperature operation and pulsating thrust, specific engineering requirements must be met to maintain efficient and stable performance. Recent research by the University of Mi...
Sarvesh Raghupathy, Anirudh Koduganti, Rohan Kunala et al.
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