Theoretical Analysis of Performance Parameters in Oscillating Plasma Thrusters
Author:
Affiliation:
1. Princeton University, Princeton, New Jersey 08543
2. Princeton Plasma Physics Laboratory, Princeton, New Jersey 08543
Funder
Air Force Office of Scientific Research
U.S. Department of Energy, Office of Science, Office of Fusion Energy Sciences
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/am-pdf/10.2514/1.B37935
Reference20 articles.
1. Low frequency oscillations in a stationary plasma thruster
2. Low-frequency model of breathing oscillations in Hall discharges
3. Performance characterization of a low-power magnetically shielded Hall thruster with an internally-mounted hollow cathode
4. Maximum time-dependent space-charge limited diode currents
5. Hall thruster operation with externally driven breathing mode oscillations
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