Magnetic nozzle efficiency in a low power inductive plasma source
Author:
Funder
National Science Foundation Graduate Research Fellowship Program
Publisher
IOP Publishing
Subject
Condensed Matter Physics
Link
http://iopscience.iop.org/article/10.1088/1361-6595/ab2d7d/pdf
Reference61 articles.
1. Direct thrust measurement of a permanent magnet helicon double layer thruster
2. Performance improvement of a permanent magnet helicon plasma thruster
3. Plasma detachment in a propulsive magnetic nozzle via ion demagnetization
4. On plasma detachment in propulsive magnetic nozzles
5. Two-dimensional plasma expansion in a magnetic nozzle: Separation due to electron inertia
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