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Photonic spin control for solar wind electric sail
Institution:1. School of Aerospace Engineering, Tsinghua University, 100084 Beijing, People''s Republic of China;2. Department of Civil and Industrial Engineering, University of Pisa, I-56122 Pisa, Italy;1. College of Engineering, University of South Alabama, 150 Jaguar Dr. Mobile, 36688, AL, USA;2. NASA Marshall Space Flight Center, Huntsville, AL, USA;1. Department of Earth and Space Science and Engineering, York University, 4700 Keele Street, Toronto, Ontario, M3J 1P3, Canada;2. Department of Mechanical Engineering, York University, 4700 Keele Street, Toronto, Ontario, M3J 1P3, Canada;3. Department of Mechanical and Industrial Engineering, University of Toronto, 5 King''s College Road, Toronto, Ontario, M5S 3G8, Canada
Abstract:The electric solar wind sail (E-sail) is a novel, efficient propellantless propulsion concept which utilises the natural solar wind for spacecraft propulsion with the help of long centrifugally stretched charged tethers. The E-sail requires auxiliary propulsion applied to the tips of the main tethers for creating the initial angular momentum and possibly for modifying the spinrate later during flight to counteract the orbital Coriolis effect and possibly for mission specific reasons. We introduce the possibility of implementing the required auxiliary propulsion by small photonic blades (small radiation pressure solar sails). The blades would be stretched centrifugally. We look into two concepts, one with and one without auxiliary tethers. The use of small photonic sails has the benefit of providing sufficient spin modification capability for any E-sail mission while keeping the technology fully propellantless. We conclude that small photonic sails appear to be a feasible and attractive solution to E-sail spinrate control.
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