Modeling of Initial Detonation-mode Acceleration in Pulsed Plasma and Magnetoplasmadynamic Thrusters
Author:
Affiliation:
1. NASA Marshall Space Flight Center
2. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4728
Reference8 articles.
1. Performance of a Hydromagnetic Plasma Gun
2. Measured performance of a multimegawatt MPD thruster
3. Acceleration Modes and Transitions in Pulsed Plasma Accelerators
4. Plasma deflagration and the properties of a coaxial plasma deflagration gun
5. 5J.K. Ziemer, "Performance scaling of gas-fed pulsed plasma thrusters," Ph.D. Dissertation 3016-T, Mechanical and Aerospace Engineering,Princeton Univ., Princeton,NJ (2001).
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