Study of the design and efficiency of single stage EHD thrusters at the sub-atmospheric pressure of 1.3 kPa-Reference-Cited by-同舟云学术

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Study of the design and efficiency of single stage EHD thrusters at the sub-atmospheric pressure of 1.3 kPa

Published:2017-12 Issue:12 Volume:24 Page:123513
ISSN:1070-664X
Container-title:Physics of Plasmas
language:en
Short-container-title:Physics of Plasmas

Author:

Granados Victor H.¹^ORCID,Pinheiro Mario J.²^ORCID,Sá Paulo A.¹^ORCID

Affiliation:

1. Departamento de Engenharia Física, Faculdade de Engenharia da Universidade do Porto, Rua Doutor Roberto Frias s/n, 4200-465 Porto, Portugal

2. Departamento de Física, Instituto Superior Técnico—IST, Universidade de Lisboa Av. Rovisco Pais, 1049-001 Lisboa, Portugal

Publisher

AIP Publishing

Subject

Condensed Matter Physics

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5018424

Reference41 articles.

1. Electric propulsion for satellites and spacecraft: established technologies and novel approaches

2. On the performance of electrohydrodynamic propulsion

3. J. Wilson , H. D. Perkins , and W. K. Thompson , “ An investigation of ionic wind propulsion,” Technical Report No. NASA/TM-2009-215822 (2009).

4. Model of Ideal Electrohydrodynamic Thruster

5. Ionic wind generation by a wire-cylinder-plate corona discharge in air at atmospheric pressure

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2. Diversity of Physical Processes: Challenges and Opportunities for Space Electric Propulsion;Applied Sciences;2022-11-03

3. A novel method to predict current–voltage characteristics of positive corona discharges based on a perturbation technique. II. Global analysis and applications to electrohydrodynamic thrusters;AIP Advances;2022-10-01

4. Analysis of the Efficiency of the Electrohydrodynamic Propulsion Based on the Biefeld-Brown Effect for Manned and Unmanned Aircrafts;Applied Sciences;2022-03-15

5. Modeling of Electrohydrodynamic (EHD) Plasma Thrusters: Optimization of Physical and Geometrical Parameters;Applied Sciences;2022-02-04

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