21 citations as recorded by crossref.

1. Electrostatic Tether Application for Scattering of Relativistic Particles in the Earth’s Radiation Belts A. Sanchez-Torres 10.1109/TPS.2015.2444473
2. Geomagnetic Field Tracker for Deorbiting a CubeSat Using Electric Thrusters J. Morales et al. 10.2514/1.G003908
3. Drag and propulsive forces in electric sails with negative polarity A. Sanchez-Torres 10.1016/j.asr.2015.12.013
4. Considerations for Eco-LeanSat Satellite Manufacturing and Recycling J. Buitrago-Leiva et al. 10.3390/su16124933
5. Artificial Collinear Lagrangian Point Maintenance With Electric Solar Wind Sail L. Niccolai et al. 10.1109/TAES.2020.2990805
6. Electric Sail Test Cube–Lunar Nanospacecraft, ESTCube-LuNa: Solar Wind Propulsion Demonstration Mission Concept A. Slavinskis et al. 10.3390/aerospace11030230
7. Small satellite attitude determination during plasma brake deorbiting experiment O. Khurshid et al. 10.1016/j.actaastro.2016.08.035
8. FORESAIL‐1 CubeSat Mission to Measure Radiation Belt Losses and Demonstrate Deorbiting M. Palmroth et al. 10.1029/2018JA026354
9. Analytical three-dimensional propulsion process of electric sail with fixed pitch angle R. Jin et al. 10.1016/j.ast.2023.108845
10. Aalto-1, multi-payload CubeSat: In-orbit results and lessons learned M. Mughal et al. 10.1016/j.actaastro.2020.11.044
11. Coulomb drag propulsion experiments of ESTCube-2 and FORESAIL-1 I. Iakubivskyi et al. 10.1016/j.actaastro.2019.11.030
12. Electric sail phasing maneuvers for constellation deployment L. Niccolai et al. 10.1016/j.actaastro.2019.12.003
13. A comprehensive review of Electric Solar Wind Sail concept and its applications M. Bassetto et al. 10.1016/j.paerosci.2021.100768
14. Electric Sail Mission Expeditor, ESME: Software Architecture and Initial ESTCube Lunar Cubesat E-Sail Experiment Design M. Palos et al. 10.3390/aerospace10080694
15. Rapid Evaluation of the Decay Time of a Plasma Brake-Based CubeSat M. Bassetto et al. 10.3390/aerospace9110636
16. Interplanetary Student Nanospacecraft: Development of the LEO Demonstrator ESTCube-2 J. Dalbins et al. 10.3390/aerospace10060503
17. Boltzmann electron PIC simulation of the E-sail effect P. Janhunen 10.5194/angeo-33-1507-2015
18. Gyroless Spin-Stabilization Controller and Deorbiting Algorithm for CubeSats J. Morales et al. 10.1007/s42405-020-00311-5
19. Plasma brake model for preliminary mission analysis L. Orsini et al. 10.1016/j.actaastro.2017.12.048
20. Trajectory Approximation of a Low-Performance E-Sail with Fixed Orientation A. Quarta & G. Mengali 10.3390/aerospace11070532
21. Trajectory Approximation of a Coulomb Drag-Based Deorbiting L. Niccolai et al. 10.3390/aerospace9110680