Thrust movement of an ion engine system
Author:
Affiliation:
1. Electrotechnical Laboratory, Sakura-mura, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.8613
Reference7 articles.
1. Direct thrust measurement on 5-cm diameter mercury Kaufman ion thruster with a torsion type thrust balance
2. Measurement of double charged ions in the beam of a 30-cm mercury bombardment thruster
3. Ion beam divergence characteristics of two-grid accelerator systems
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