Ion Thruster Operation with Carbon Nanotube Field Emission Cathode
Author:
Affiliation:
1. Kyushu University, Fukuoka 816-8580, Japan
2. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
3. Tokyo Metropolitan College of Industrial Technology, Tokyo 116-8523, Japan
4. Japan Aerospace Exploration Agency, Kanagawa 252-5210, Japan
Funder
Institute of Space and Astronautical Science
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B37214
Reference25 articles.
1. Ion Propulsion Development Projects in U.S.: Space Electric Rocket Test I to Deep Space 1
2. WallaceN. C.FehringerM. “The ESA GOCE Mission and the T5 Ion Propulsion Assembly,” IEPC Paper 2009–269, Sept. 2009.
3. Powered Flight of Electron Cyclotron Resonance Ion Engines on Hayabusa Explorer
4. Development and Testing of the Hayabusa2 Ion Engine System
5. FeuerbornS. A.NearyD.A.PerkinsJ.M. “Finding a Way: Boeing’s ‘All Electric Propulsion Satellite’,” AIAA Paper 2013-4126, July 2013.
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