2005年 第7卷 第4期
稳态等离子体发动机磁场设计的发展及其展望
1.哈尔滨工业大学能源科学与工程学院，哈尔滨 黑龙江 150001
2.Ring（MIREA），Prospect Vernardskogo，78，Moskow，117454，Russia
下一篇 上一篇
摘要
论述了稳态等离子体发动机对于我国空间发展战略的重要意义和作用，指出磁场设计是提高稳态等离子体发动机性能的关键技术之一；分析了稳态等离子体发动机通道内磁场设计的发展过程，在此基础上提出了用于稳态等离子发动机磁场设计的体系化构想，并且指出了其中存在的一些关键问题和拟采取的解决措施以及磁场体系化设计对稳态等离子体发动机带来的预期效益和影响；最后展望了稳态等离子体发动机磁场设计体系的进一步发展和应用。
图片
图1
图2
图3
图4
图5
图6
图7
参考文献
[ 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 链接1
[ 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 链接1
[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
京公网安备 11010502051620号
