An atmosphere-breathing propulsion system using inductively coupled plasma source-Reference-Cited by-同舟云学术

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An atmosphere-breathing propulsion system using inductively coupled plasma source

Published:2023-05 Issue:5 Volume:36 Page:223-238
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHENG Peng,WU Jianjun,ZHANG Yu,CHE Bixuan,ZHAO Yuanzheng

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference37 articles.

1. An evaluation of CubeSat orbital decay;Oltrogge,2011

2. A comprehensive review of atmosphere-breathing electric propulsion systems;Zheng;Int J Aerosp Eng,2020

3. Air intake performance of air breathing ion engines;Fujita;Proc Jpn Soc Aeronautical Space Sci,2004

4. Design of air intake for air breathing ion engine;Hisamoto,2012

5. Development statue of atomic oxygen simulator for air breathing ion engine;Hisamoto,2011

Cited by 4 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. Optical detection method of discharge mode transition of inductively coupled plasma in an atmosphere-breathing electric propulsion system;Chinese Journal of Aeronautics;2024-08

2. Full lifetime demonstration of a Micro-Cathode-Arc thruster evolution characteristics;Chinese Journal of Aeronautics;2024-06

3. Investigation on plasma ionization process of a micro-cathode arc thruster;Acta Astronautica;2024-03

4. Elliptical Orbit Design Based on Air-Breathing Electric Propulsion Technology in Very-Low Earth Orbit Space;Aerospace;2023-10-20

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