25 citations as recorded by crossref.

1. Electric Sail Mission Expeditor, ESME: Software Architecture and Initial ESTCube Lunar Cubesat E-Sail Experiment Design M. Palos et al. 10.3390/aerospace10080694
2. Optimal switching strategy for radially accelerated trajectories A. Quarta & G. Mengali 10.1007/s10569-009-9233-2
3. Simulation study of the plasma-brake effect P. Janhunen 10.5194/angeo-32-1207-2014
4. Optimal Guidance for Heliocentric Orbit Cranking with E-Sail-Propelled Spacecraft A. Quarta 10.3390/aerospace11060490
5. Propulsive Force in Electric Solar Sails for Missions in the Heliosphere A. Sanchez-Torres 10.1109/TPS.2019.2897082
6. Electric sail, photonic sail and deorbiting applications of the freely guided photonic blade P. Janhunen 10.1016/j.actaastro.2013.07.041
7. Electric sail missions to potentially hazardous asteroids A. Quarta & G. Mengali 10.1016/j.actaastro.2009.11.021
8. Drag and propulsive forces in electric sails with negative polarity A. Sanchez-Torres 10.1016/j.asr.2015.12.013
9. Flight Dynamics and Control Strategy of Electric Solar Wind Sails G. Li et al. 10.2514/1.G004608
10. Electric sail phasing maneuvers for constellation deployment L. Niccolai et al. 10.1016/j.actaastro.2019.12.003
11. Optimal interplanetary rendezvous combining electric sail and high thrust propulsion system A. Quarta et al. 10.1016/j.actaastro.2010.01.024
12. Electrostatic Plasma Brake for Deorbiting a Satellite P. Janhunen 10.2514/1.47537
13. Analytical Tool for Thrust Vector Description of a Web-Shaped E-Sail M. Bassetto et al. 10.1109/TAES.2024.3409272
14. An orbital-attitude coupled control framework for a full-scale flexible electric solar wind sail spacecraft in orbital transformation missions S. Zeng et al. 10.1016/j.ast.2024.109655
15. Coupled Attitude-Orbit Dynamics and Control for an Electric Sail in a Heliocentric Transfer Mission M. Huo et al. 10.1371/journal.pone.0125901
16. Invited Article: Electric solar wind sail: Toward test missions P. Janhunen et al. 10.1063/1.3514548
17. Space sails for achieving major space exploration goals: Historical review and future outlook M. Berthet et al. 10.1016/j.paerosci.2024.101047
18. Plasma brake model for preliminary mission analysis L. Orsini et al. 10.1016/j.actaastro.2017.12.048
19. Coupled attitude-vibration analysis of an E-sail using absolute nodal coordinate formulation C. Zhao et al. 10.1007/s42064-020-0081-x
20. Trajectory Approximation of a Coulomb Drag-Based Deorbiting L. Niccolai et al. 10.3390/aerospace9110680
21. Electric Sail Mission Analysis for Outer Solar System Exploration A. Quarta & G. Mengali 10.2514/1.47006
22. Rapid Evaluation of the Decay Time of a Plasma Brake-Based CubeSat M. Bassetto et al. 10.3390/aerospace9110636
23. Boltzmann electron PIC simulation of the E-sail effect P. Janhunen 10.5194/angeo-33-1507-2015
24. Robust Flight Tether for In-Orbit Demonstrations of Coulomb Drag Propulsion P. Toivanen et al. 10.3390/aerospace11010062
25. A comprehensive review of Electric Solar Wind Sail concept and its applications M. Bassetto et al. 10.1016/j.paerosci.2021.100768