Mission Capability Assessment of CubeSats Using a Miniature Ion Thruster
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of California, Los Angeles, Los Angeles, California 90095
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A32435
Reference29 articles.
1. Hollow Cathode and Low-Thrust Extraction Grid Analysis for a Miniature Ion Thruster
2. also AIAA Paper 2004-4115.
3. also AIAA Paper 2005-3887.
4. also AIAA 2006-4498.
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