Optimization of the Energy Distribution in Ablative Pulsed Plasma Thrusters
Author:
Affiliation:
1. Shanghai Aerospace Control Technology Institute, 201109 Shanghai, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056272
Reference27 articles.
1. “You can get there from here”: Advanced low cost propulsion concepts for small satellites beyond LEO
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3. Pulsed Plasma Thruster
4. Plasma acceleration processes in an ablative pulsed plasma thruster
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