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Study on the modes transformation and emission characteristics of Ionic Liquid Electrospray Thrusters

  • Published:2024-02 Issue: Volume:215 Page:415-425
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Yang ChengORCID,Luo Jiawei,Wu Xiangbei,Shen Yan

Funder

Ministry of Science and Technology of the People's Republic of China

Science, Technology and Innovation Commission of Shenzhen Municipality

National Key Research and Development Program of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. Recent progress and perspectives of space electric propulsion systems based on smart nanomaterials;Levchenko;Nat. Commun.,2018

2. Space micropropulsion systems for Cubesats and small satellites: from proximate targets to furthermost frontiers;Levchenko;Appl. Phys. Rev.,2018

3. CubeSat constellation management using ionic liquid electrospray propulsion;Gomez Jenkins;Acta Astronaut.,2018

4. Development and laboratory testing of a CubeSat-compatible staged ionic-liquid electrospray propulsion system;Pettersson,2021

5. Review of micro propulsion technology for space gravitational waves detection;Liu;Acta Astronaut.,2022
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