Time-synchronized laser-induced fluorescence in the near-field of a 600 Watt Hall thruster
Author:
Affiliation:
1. Mechanical Engineering Department, Stanford University, Stanford, California 94305, USA
2. Edwards Air Force Base, California 93524, USA
Funder
Air Force Office of Scientific Research
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/am-pdf/10.1063/5.0058416
Reference35 articles.
1. The Hall effect and rocket flight
2. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters
3. Low frequency oscillations in a stationary plasma thruster
4. Low-frequency model of breathing oscillations in Hall discharges
5. J. M. Fife, M. Martinez-Sanchez, and J. Szabo, “A numerical study of low-frequency discharge oscillations in Hall thrusters,” in Proceedings of the 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Seattle, WA (AIAA, 1997).
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