In-Flight Plume Control and Thrust Tuning in Magnetic Nozzle Using Tapered-Coils System Under the Effect of Density Gradient
Author:
Affiliation:
1. Department of Manufacturing Processes and Automation Engineering, Netaji Subhas University of Technology, New Delhi, India
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Condensed Matter Physics,Nuclear and High Energy Physics
Link
http://xplorestaging.ieee.org/ielx7/27/10132334/10092894.pdf?arnumber=10092894
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5. Time-resolved investigation of the asymmetric plasma plume in a pulsed plasma thruster
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