Electrical Model and Electrical Temperature- Dependent Model for Electrospray Thrusters-Reference-Cited by-同舟云学术

Electrical Model and Electrical Temperature- Dependent Model for Electrospray Thrusters

Published:2023-10 Issue:10 Volume:38 Page:12988-12998
ISSN:0885-8993
Container-title:IEEE Transactions on Power Electronics
language:
Short-container-title:IEEE Trans. Power Electron.

Author:

Blázquez-Plaza Francisco José¹^ORCID,Barrado Andrés²^ORCID,Wijnen Mick³^ORCID,Villegas-Prados David⁴^ORCID

Affiliation:

1. Electrical Engineering, Universidad Carlos III de Madrid - Campus de Leganes, Leganes, Spain

2. Tecnologia Electronica, Universidad Carlos III De Madrid, Leganes, Spain

3. IENAI Space S.L., Leganes, Spain

4. Universidad Carlos III de Madrid - Campus de Leganes, Leganes, Spain

Funder

Comunidad de Madrid

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering

Link

http://xplorestaging.ieee.org/ielx7/63/10242187/10173640.pdf?arnumber=10173640

Reference32 articles.

1. A Novel Coupling Method of Power Supplies With High Power Density, Efficiency, and Fast Dynamic Response for Spacecraft Hollow Cathode Power Supply Applications

2. A Planar Array of Micro-Fabricated Electrospray Emitters for Thruster Applications

3. Electrochemical processes in electrospray ionization mass spectrometry

4. Space mobility optimization and concurrent engineering for modular micro-propulsion systems with 360 by IENAI SPACE;pasquale;Proc 73rd Int Astronautical Congr,0

Cited by 1 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. High-performance, miniaturized and configurable power and control unit for electrospray thrusters;CEAS Space Journal;2024-07-25