Volume 26, Issue 2 No AccessElectrostatic Plasma Brake for Deorbiting a SatellitePekka JanhunenPekka Janhunen Finnish Meteorological Institute, FIN-00101, Helsinki, FinlandSearch for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/1.47537SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byElectrodynamic tether and brake sails combination deorbit design1 Jan 2025 | Acta Astronautica, Vol. 226A review of electrodynamic tether missions: Historical trend, dimensionless parameters, and opportunities opening space markets1 Dec 2024 | Acta Astronautica, Vol. 225Trajectory Approximation of a Low-Performance E-Sail with Fixed Orientation28 June 2024 | Aerospace, Vol. 11, No. 7Magnetic Attitude Control Scheme for Drag Sail Deorbiting with Limited SensorsShuo Mu, Nan Zhang and Hexi Baoyin23 March 2024 | Journal of Guidance, Control, and Dynamics, Vol. 47, No. 6Electric Sail Test Cube–Lunar Nanospacecraft, ESTCube-LuNa: Solar Wind Propulsion Demonstration Mission Concept14 March 2024 | Aerospace, Vol. 11, No. 3Analytical three-dimensional propulsion process of electric sail with fixed pitch angle1 Feb 2024 | Aerospace Science and Technology, Vol. 145Optimal deep-space heliocentric transfers with an electric sail and an electric thruster1 Jan 2024 | Advances in Space Research, Vol. 73, No. 1Robust Flight Tether for In-Orbit Demonstrations of Coulomb Drag Propulsion9 January 2024 | Aerospace, Vol. 11, No. 1Performance Estimate of a Spin-Stabilized Drag Sail for Spacecraft Deorbiting10 January 2024 | Applied Sciences, Vol. 14, No. 2Charged aerodynamics: Ionospheric plasma drag on objects in low-Earth orbit1 Nov 2023 | Acta Astronautica, Vol. 212Thrust model and guidance scheme for single-tether E-sail with constant attitude1 Nov 2023 | Aerospace Science and Technology, Vol. 142Review of methods and means for space debris removal from low-earth orbits19 October 2023 | Technical mechanics, Vol. 2023, No. 3Interplanetary Student Nanospacecraft: Development of the LEO Demonstrator ESTCube-226 May 2023 | Aerospace, Vol. 10, No. 6Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation TechniqueLorenzo Niccolai , Alessandro A. 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