Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms
In-space electric propulsion technologies have advanced significantly in the last decade, while there has been increasing interest in economical propulsion systems with growing demand for commercial and scientific applications using small spacecraft platforms. Electrostatic propulsion, in particular...
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| Published in | Progress in aerospace sciences Vol. 126; p. 100742 |
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| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
Oxford
Elsevier Ltd
01.10.2021
Elsevier BV |
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| Online Access | Get full text |
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| Abstract | In-space electric propulsion technologies have advanced significantly in the last decade, while there has been increasing interest in economical propulsion systems with growing demand for commercial and scientific applications using small spacecraft platforms. Electrostatic propulsion, in particular, offers advantages over other propulsion systems in various aspects, including long operational lifetime, high specific impulse, and light weight. However, electric propulsion systems are subject to drawbacks such as system complexity and wall erosion, which represent obstacles toward miniaturization to be utilized for small spacecraft. New ideas are continuously explored to overcome such challenges and improve the performance. This article presents a comprehensive review of electrostatic propulsion systems, with particular focus on Gridded Ion Engine (GIE), Hall Effect Thruster (HET), and Cusped Field Thruster (CFT) systems, with respect to their operational principles, applications, and characteristics. State-of-the-art technologies and novel concepts are discussed including research efforts for miniaturization, along with the latest available data of their performance and features. While GIE and HET are mature and well understood, the power consumption of miniaturized thrusters is relatively high, leaving room for improvement toward practical application. CFT, on the other hand, features appreciable performance even in miniaturized form, offering promise to serve for small spacecraft platforms. |
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| AbstractList | In-space electric propulsion technologies have advanced significantly in the last decade, while there has been increasing interest in economical propulsion systems with growing demand for commercial and scientific applications using small spacecraft platforms. Electrostatic propulsion, in particular, offers advantages over other propulsion systems in various aspects, including long operational lifetime, high specific impulse, and light weight. However, electric propulsion systems are subject to drawbacks such as system complexity and wall erosion, which represent obstacles toward miniaturization to be utilized for small spacecraft. New ideas are continuously explored to overcome such challenges and improve the performance. This article presents a comprehensive review of electrostatic propulsion systems, with particular focus on Gridded Ion Engine (GIE), Hall Effect Thruster (HET), and Cusped Field Thruster (CFT) systems, with respect to their operational principles, applications, and characteristics. State-of-the-art technologies and novel concepts are discussed including research efforts for miniaturization, along with the latest available data of their performance and features. While GIE and HET are mature and well understood, the power consumption of miniaturized thrusters is relatively high, leaving room for improvement toward practical application. CFT, on the other hand, features appreciable performance even in miniaturized form, offering promise to serve for small spacecraft platforms. |
| ArticleNumber | 100742 |
| Author | Yeo, Suk Hyun Kahnfeld, Daniel Ogawa, Hideaki Schneider, Ralf |
| Author_xml | – sequence: 1 givenname: Suk Hyun orcidid: 0000-0002-8788-5491 surname: Yeo fullname: Yeo, Suk Hyun email: suk.hyun.yeo@student.rmit.edu.au organization: RMIT University, Melbourne, Victoria 3001, Australia – sequence: 2 givenname: Hideaki orcidid: 0000-0002-7584-0077 surname: Ogawa fullname: Ogawa, Hideaki email: hideaki.ogawa@aero.kyushu-u.ac.jp organization: Kyushu University, Fukuoka 819-0395, Japan – sequence: 3 givenname: Daniel orcidid: 0000-0002-5900-4423 surname: Kahnfeld fullname: Kahnfeld, Daniel email: kahnfeldd@uni-greifswald.de organization: University of Greifswald, Greifswald 17498, Germany – sequence: 4 givenname: Ralf orcidid: 0000-0002-4492-8869 surname: Schneider fullname: Schneider, Ralf email: schneider@uni-greifswald.de organization: University of Greifswald, Greifswald 17498, Germany |
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| SubjectTerms | Commercial spacecraft Cusped Field Thruster Electric propulsion Electrostatic propulsion Gridded Ion Engine Hall effect Hall Effect Thruster Ion engines Miniaturization Performance enhancement Platforms Power consumption Propulsion systems Spacecraft propulsion Specific impulse Thrusters Weight reduction |
| Title | Miniaturization perspectives of electrostatic propulsion for small spacecraft platforms |
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