Strategic Study of CAE >> 2005, Volume 7, Issue 4
Research Status and Development of the Magnetic Field Design for Stationary Plasma Thruster
1. Harbin Institute of Technology , School of Energy Science and Technology , Harbin 150001 , China
2. Ring (MIREA) , Prospect Vernardskogo , 78 , Moskow 117454 , Russia
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Abstract
The Stationary Plasma Thruster (SPT) will play a very important role for China's future space developing plan. And the magnetic field is the key to improve the performance of SPT. The evolvement of the magnetic field character applied to the two generations SPT has been reviewed. Then a set of engineering method used in the magnetic field design for SPT is set up in the paper. Besides, some possible problems existing in the method and the corresponding ways to resolve them are respectively put forward. And the expectant results are also anticipated when the set of method is applied to the magnetic field design for SPT. At last, more advanced development and application of the magnetic field design method is imaged.
Keywords
space electric propulsion ; stationary plasma thruster ; magnetic field design ; development trend
References
[ 1 ] ZhurinVV , KaufmanHR , RobinsonRS .Physicsofcloseddriftthrusters[J].PlasmaSourcesSciTechnol, 1999, 8 (1) :R1~R20
[ 2 ] MorozovAI, EsipchukYV , TilininGN , TrofimovAV , SharovYA , ShshepkinGY .Plasmaacceleratorwithclosedelectrondriftandextendedaccelerationzone[J].SovietPhysicsTechnicalPhysics, 1972, 17 (1) :38~45
[ 3 ] MorizovAI, EsipchukYV , KapulkinAM , NevroskiiVA , SmirnovVA .Effectofthemagneticfieldonaclosed electronic driftaccelerator[J].SovietPhysicsTechnicalPhysics, 1972, 17 (3) :612~619
[ 4 ] MorozovAI .TheConceptualdevelopmentofstationary plasmathrusters[J].PlasmaPhysicsReports, 2003, 29 (3) :235~250 link1
[ 5 ] BoberN , MaslennikovN , DayM , PopovG , RylovY .DevelopmentandapplicationofelectricpropulsionthrustersinRussia[A ].23rdInternationalElectricPropulsionConference[C ].SeattleWA :ElectricRocketPropusionSociety, 1993.IEPC 93001
[ 6 ] PetersonPY , GallimoreAD , HaasJM .Experimentalinvestigationofhallthrusterinternalmagneticfieldtopography[R].AIAA 200138901~15
[ 7 ] HaasJM , HoferRR , GallimoreAD .HallThrusterdischargechamber plasmacharacterizationusingahigh speedaxialreciprocatingelectrostaticprobe[R].AIAA 9924261~14
[ 8 ] HoferRR , HaasJM .Optimizationofhallthrustermagneticfieldtopography[A ].27thIEEEInternationalConferenceonPlasmaScience[C].NewOrleansLA :InstituteforElecteicalandEletronicEngineers, 2000
[ 9 ] GarriguesL , HagelaarGJM , BareillesJ , BonifaceC , BoeufJP .ModelstudyoftheinfluenceofthemagneticfieldconfigurationontheperformanceandlifetimeofaHallthruster[J].PhysicsofPlasmas, 2003, 10 (12) :4886~4892
[10] HagelaarGJM , BareillesJ, GarriguesL , BoeufJP .Two dimensionalmodelofastationaryplasmathruster[J].JournalofAppliedPhysics, 2002, 91 (9) :5592~5598
[11] MorozovAI , BugrovaAI , DesyatskovAV .ATON thrusterplasmaAccelerator[J].PlasmaPhysicsReports, 1997, 23 (7) :587~597
[12] BugrovaAI , LipatovA .S , KharchevnikovVK , ChurbanovDV , MorozovAI .SPT ATONTestsatKurchatovInstituteStands[A ].24thInternationalElectricPropulsionConference[C].MoscowRussia:ElectricRocketPropusionSociety, 1995.IEPC 95067
[13] 王仲奇, 郑 严.叶轮机械弯扭叶片的研究现状及发展趋势[J].中国工程科学, 2000, 2 (6) :40~48 link1
[14] 菅井秀郎, 等离子体电子工程学[M ].北京:科学出版社, 2002.56~58
[15] MorozovAI , SvelyevVV .Fundamentalsofstationaryplasmathrustertheory[M ].In:KadomtsevB , Shafranov, eds.ReviewsofPlasmaPhysics.NewYork:ConsultantsBureau, 2001, 21:244
[16] BugrovaAI .Electrondistributionfunctioninthechannelofanelectron ringplasmaaccelerator[J].ZhTekhFiz, 1987, 57:1852~1854
[17] BugrovaAI , DesyatskovAV , MorozovAI.ElectrondistributionfunctioninaHallaccelerator[J].1992, Sov.J.PlasmaPhys, 18 (8) :501~507
[18] DarnonF , GarriguesL , BoeufJP , BouchouleA , LyszykM .SpontaneousoscillationsinaHallthruster[J].IEEETrans.PlasmaScience, 1999, 27 (1) :98
[19] ChaseRL , MehtaUB , BogdanoffDW , etal.CommentsonanMHDenergybypassenginepoweredspaceliner[R].AIAA 994975