Small satellite electric propulsion options
Author:
Affiliation:
1. NYMA, Inc.; NASA, Lewis Research Center, Cleveland, OH
2. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-4137
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Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Feed and Pressurization Systems and Architectures for Green Chemical Micro-Propulsion;Space Technology Library;2024
2. System Design, Development and Ground Verification of a Separable De-Orbit Mechanism for the Orbital Manoeuvre of Micro-Satellite ALE-1;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2021
3. Propulsion options for very low Earth orbit microsatellites;Acta Astronautica;2017-04
4. Characterization of a very low power arcjet;35th Joint Propulsion Conference and Exhibit;1999-06-20
5. Pulsed plasma thruster technology directions;33rd Joint Propulsion Conference and Exhibit;1997-07-06
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