Growth of Rayleigh instability in a Hall thruster channel having dust in exit region
Author:
Affiliation:
1. Plasma Waves and Particle Acceleration Laboratory, Department of Physics, Indian Institute of Technology Delhi, New Delhi 110 016, India
Funder
Indo-French Centre for the Promotion of Advanced Research
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5050688
Reference48 articles.
1. Plasma oscillations in Hall thrusters
2. Physics of closed drift thrusters
3. Effect of a magnetic field on the plasma plume from Hall thrusters
4. Measurement of Thrust in a Linear Hall Accelerator
5. Parametric studies of the Hall current plasma thruster
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