Stagnation-Point Density of Hypersonic Ions in a Repelling Plasma Sheath
Author:
Affiliation:
1. Science Applications International Corporation, San Diego, California 92121
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3948
Reference10 articles.
1. High-voltage interactions in plasma wakes: Simulation and flight measurements from the Charge Hazards and Wake Studies (CHAWS) experiment
2. Ion current collection in spacecraft wakes
3. Effect of object potentials on the wake of a flowing plasma
4. Anderson, J. D., Jr., Modern Compressible Flow, 2nd ed.McGraw-Hill, New York, 1982, pp.100-144.
5. High-voltage plasma interactions calculations using NASCAP/LEO
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