›› 2013, Vol. 33 ›› Issue (6): 67-73.doi: 10.3780/j.issn.1000-758X.2013.06.009

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LEOSpacecraftMagnetismPropulsionandItsCapabilityEstimation

 XIAO  Xin-Xin, LI  Wen-Hao, ZHANG  Heng, LIU  Kai-Lei   

  1. (InstituteofMechanics,ChineseAcademyofSciences,Beijing100190)
  • Received:2013-07-03 Revised:2013-09-16 Published:2013-12-25 Online:2013-12-25

Abstract: Accordingtothecharacteristicsofthemagneticfielddistributionintheearthspace,thepropulsiontechnologywithoutpropellantconsumptionwasproposedtomaintainorchangetheLEOspacecraftaltitude.Themagneticthrustdynamicswasmodeledbasedonthefundamentalmagnetics,themagnetismpropulsionprinciplewithcontinuousthrustbutnopropellantconsumptionwasclarified,andthetrackingcontrolstrategyofgeomagneticlineofforcefordecouplingthemagneticmomentwasproposed.Theflightenvelopeofmagnetismpropulsionandtypicalcalculationsfortheorbitaltitudemaintenanceorchangeswascarriedout.Theresultsshowthatthemagneticmomentofthespacecraftcanbeusedtomaintainorchangethespacecraftaltitudefrom600kmto1000kminlowearthorbit(LEO)whenitisupto106Am2.Furthermore,thetechnicalfeasibilityofobtaininghighmagneticmomentisbrieflyanalyzed.

Key words: Magnetismpropulsion, Nopropellantconsumptionpropulsion, Orbitalaltitudemaintenance, Orbitalaltitudeincrease, Spacepropulsion, Spacecraft