Approach to the parametric design of ion thrusters
Author:
Affiliation:
1. Colorado State University, Fort Collins, Colorado 80523
2. Hughes Research Laboratories, Malibu, California 90265
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23258
Reference20 articles.
1. Critical Elements of Electron-Bombardment Propulsion for Large Space Systems
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2. On the space-charge effects in the beam extraction process of ion thrusters: the roles of compensating electrons and changing beam radius;Plasma Sources Science and Technology;2023-04-01
3. Investigation of the ion-optical system of an ion thruster with a microwave plasma generator with a power of up to 10 W;Acta Astronautica;2021-12
4. Dynamic characteristics of beam perveance under thermal deformation for a three-grid ion thruster;Journal of Vacuum Science & Technology B;2019-01
5. A Study of Ion Thruster Optics through Particle Simulations and Evaluation of the Near Plume Plasma Properties;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-28
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