基于ISRU应用的电磁推进技术
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摘要
原位资源利用(ISRU)是实现空间电推进燃料补给、增加使用寿命、增大有效载荷能力和降低任务成本的推进技术方案。无电极电推力器由于不存在电极与推进剂兼容性约束,在应用ISRU技术方面具有优势。针对国内外四种先进无电极推力器发展现状进行调研,分析了无电极推力器在ISRU上的应用前景,重点介绍了场反构型(FRC)推力器在ISRU应用中的显著优点。
In Situ Resource Utilization(ISRU)technology scheme has great development potential for Space Electric Propulsion to supply propellant,increase lifetime,enhance effective load and reduce mission cost. Electrodeless propulsion has unique advantage in the application of ISRU technology owing to the absence of compatibility constraint between electrode and propellant. This paper investigated the current status of four advanced electrodeless thrusters at home and abroad,and analyzed the advantages of electrodeless thrusters in ISRU application. Field Reversed Configuration thruster was mainly introduced due to its distinct prospect in ISRU application.
In Situ Resource Utilization(ISRU)technology scheme has great development potential for Space Electric Propulsion to supply propellant,increase lifetime,enhance effective load and reduce mission cost. Electrodeless propulsion has unique advantage in the application of ISRU technology owing to the absence of compatibility constraint between electrode and propellant. This paper investigated the current status of four advanced electrodeless thrusters at home and abroad,and analyzed the advantages of electrodeless thrusters in ISRU application. Field Reversed Configuration thruster was mainly introduced due to its distinct prospect in ISRU application.
引文
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[2]Kirtley D,Slough J,Pfaff M,et al.Steady operation of an electromagnetic plasmoid thruster[C]//Joint Army Navy NASA AirForce Conference,2011.
[3]于达仁.空间电推进原理[M].哈尔滨:哈尔滨工业大学出版社,2014.
[4]Drake M G,Hoffman S J,Beaty D W.Human Exploration of Mars,Design Reference Architecture 5.0[C]//Aerospace Conference,IEEE,2010:1-24.
[5]方勇.2017年世界航天发展的重要趋势与进展[J].卫星应用,2018(2):8-14.
[6]Goebel D M,Katz I.Fundamentals of electric propulsion:ion and Hall thrusters[M].John Wiley&Sons,2008.
[7]Shinohara S,Nishida H,Tanikawa T,et al.Development of Electrodeless Plasma Thrusters With High-Density Helicon Plasma Sources[J].Transactions on Plasma Science,2014,42(5):1245-1254.
[8]Motomura T,Shinohara S,Tanikawa T,et al.Development of electrodeless electric propulsion systems using high-density helicon plasmas:The HEAT project[C]//General Assembly and Scientific Symposium,IEEE,2011:1-4.
[9]D??Az F R C.An overview of the VASIMR engine:High Power Space Propulsion with RF Plasma Generation and Heating[C]//American Institute of Physics,2001:3-15.
[10]Weber T E,Slough J T,Kirtley D.The electrodeless Lorentz force(ELF)thruster experimental facility[J].Review of Scientific Instruments,2012,83(11):113509.
[11]Toki K,Shinohara S,Tanikawa T,et al.Preliminary investigation of helicon plasma source for electric propulsion applications[C]//Proc 28thIEPC,2003:1-10.
[12]夏广庆,王冬雪,薛伟华,等.螺旋波等离子体推进研究进展[J].推进技术,2011,32(6):857-863.
[13]Shinohara S,Nishida H,Tanikawa T,et al.Characterization of developed high-density helicon plasma sources and Helicon Electrodeless Advanced Thruster(HEAT)project[C]//201319thIEEEPulsedPowerConference(PPC),2013:1-8.
[14]Nakamura T,Yokoi K,Nishida H,et al.Study on Helicon Plasma Lissajous Acceleration for Electrodeless Electric Propulsion[J].Transactions of the Japan Society for Aeronautical&SpaceencesSpaceTechnologyJapan,2013,10(10):17-23.
[15]EdgarA,BenjaminWL,TimothyW,etal.VASIMRVX-200:High Power Electric Propulsion for Space Transportation Beyond LEO[C]//AAIA SPACE 2009 Conference,2000.
[16]Lynn S,Ringwood J,Gamboa J I D V.State estimation for the VASIMR plasma engine[C]//Signals and Systems Conference,IET,2009:24-29.
[17]Slough J,Kirtley D,Weber T.Pulsed plasmoid propulsion:The ELF thruster[C]//31thInternational Electric Propulsion Conference,2009:20-24.
[18]Miller S,Rovey J.Pulse discharge network development for a heavy gas field reversed configuration plasma device[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition,2010.
[19]Kirtley D,Slough J,Pfaff M,et al.Steady operation of an electromagnetic plasmoid thruster[C]//Joint Army Navy NASAAir Force Conference,2011.
[20]孙新锋,温晓东,张天平,等.大功率射频场反构型等离子体电推进研究[J].火箭推进,2018,44(1):44-52.
[21]Meeks W,Pahl R,Rovey J.Investigation of Pre-ionization Characteristics in Heavy Gas Pulsed Inductive Plasmas via Numerical Modeling[C]//47thJoint Propulsion Conference&Exhibit,2011.
[22]Pancotti A P,Little J M,Neuhoff J S,et al.Electrodeless Lorentz Force(ELF)Thruster for ISRU and Sample Return Mission[C]//34thInternational Electric Propulsion Conference,2015.
[23]Kirtley D,Pancotti A,Slough J,et al.Steady Operation of an FRC Thruster on Martian Atmosphere and Liquid Water Propellants[C]//Joint Propulsion Conference&Exhibit.2012.
[24]Kirtley D,Pihl J,Pihl C.Development of a Steady Operating Pulsed Power System for FRC and Inductive Thrusters[C]//International Electric Propulsion Conference.2013.
[25]Kirtley D E,Slough J T.A Plasma Aerocapture and Entry System for Manned Missions and Planetary Deep Space Orbiters[C]//AIAA Atmospheric Flight Mechanics Conference.2013.