Chinese Space Science and Technology ›› 2013, Vol. 33 ›› Issue (6): 67-73.doi: 10.3780/j.issn.1000-758X.2013.06.009
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XIAO Xin-Xin, LI Wen-Hao, ZHANG Heng, LIU Kai-Lei
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Abstract: Accordingtothecharacteristicsofthemagneticfielddistributionintheearthspace,thepropulsiontechnologywithoutpropellantconsumptionwasproposedtomaintainorchangetheLEOspacecraftaltitude.Themagneticthrustdynamicswasmodeledbasedonthefundamentalmagnetics,themagnetismpropulsionprinciplewithcontinuousthrustbutnopropellantconsumptionwasclarified,andthetrackingcontrolstrategyofgeomagneticlineofforcefordecouplingthemagneticmomentwasproposed.Theflightenvelopeofmagnetismpropulsionandtypicalcalculationsfortheorbitaltitudemaintenanceorchangeswascarriedout.Theresultsshowthatthemagneticmomentofthespacecraftcanbeusedtomaintainorchangethespacecraftaltitudefrom600kmto1000kminlowearthorbit(LEO)whenitisupto106Am2.Furthermore,thetechnicalfeasibilityofobtaininghighmagneticmomentisbrieflyanalyzed.
Key words: Magnetismpropulsion, Nopropellantconsumptionpropulsion, Orbitalaltitudemaintenance, Orbitalaltitudeincrease, Spacepropulsion, Spacecraft
XIAO Xin-Xin, LI Wen-Hao, ZHANG Heng, LIU Kai-Lei. LEOSpacecraftMagnetismPropulsionandItsCapabilityEstimation[J]. Chinese Space Science and Technology, 2013, 33(6): 67-73.
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URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2013.06.009
https://journal26.magtechjournal.com/kjkxjs/EN/Y2013/V33/I6/67