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- W2056541611 abstract "Space electrodynamic tethers offer the opportunity for in-space “propellantless” propulsion ar0und.planet.s with a magnetic field and ionosphere. This propulsion is accomplished by converting the .m.agnetic force on the tether current into propulsive <or drag thrust to either increase or decrease the orbital energy of the spacecraft system. To validate electrodynamic-tether thrusting, we must be able to demonstrate sustainable currents and effective methods of collecting and emitting electron current under varying ionospheric conditions. To date; significant tether current flow (-1 A) to/from the tether’s end collectors in the Earth’s ionosphere has been demonstrated as part of NASA’s TSS-IR mission in 1996;though the maximum possible current was not tested. Here, we review system-level issues associated with effective electrodynamic-tether operation, which include ionospheric and motional-EMF variability as well as details of the tether “end? contacts under varying ionospheric cpnditions. We also survey potential future near-Earth applications of electrodynamic tethers as currently conceived. Applications ranging from orbit transfer of payloads, orbit maintenance, and end-of-mission deorbiting will be described. The NASA ProSEDS mission, an important first step to understanding electrodynamic-tether capabilities, is discussed.." @default.
- W2056541611 created "2016-06-24" @default.
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- W2056541611 date "1999-06-20" @default.
- W2056541611 modified "2023-09-27" @default.
- W2056541611 title "Space electrodynamic tether propulsion technology - System considerations and future plans" @default.
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- W2056541611 doi "https://doi.org/10.2514/6.1999-2841" @default.
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