Page 122 - 《真空与低温》2026年第1期
P. 122

张天平等:空间电推进技术概览—演化电推进(下)                                        119


                  tional  Electric  Propulsion  Conference, Washington, DC,  [328]   ZOLOTUKHIN D B,PRICE P C ,KEIDAR M. Towards
                  USA,October,2013.                                  independent thrust and specific impulse control in a three-
              [319]   QI J Y,ZHANG Z K,PAN R J,et al. Ignition characteris-  stage  µCAT-MPD  thruster[C]//38th  International  Electric
                  tics of a dual-anode vacuum arc thruster with magnetic no-  Propulsion Conference,Toulouse,France,June,2024.
                  zzle[C]//38th International Electric Propulsion Conference,  [329]   LAMPROU D,LAPPASA V J,SHIMIZU T. Hollow cath-
                  Toulouse,France,June,2024.                         ode thruster design and development for small satellites[C]//
              [320]   HAQUE S. Preliminary sizing of a micro-cathode arc thru-  32nd International Electric Propulsion Conference,Kurhaus,
                  ster subsystem for operations in cis-lunar space[C]//4th In-  Wiesbaden,Germany,September,2011.
                  ternational Workshop on Lunar Cubes,2014.     [330]   FROLLANI D,COLETTI M and GABRIEL S B. Thrust
              [321]   PIETZKA M,KAUFFELDT M K,SCHEIN J. Innovative   measurements on the T6 hollow cathode thruster using di-
                  vacuum arc thruster for cubesat constellations[C]//33rd In-  rect thrust balances[C]//33rd International Electric Propul-
                  ternational  Electric  Propulsion  Conference, Washington,  sion Conference,Washington,DC,USA,October,2013.
                  DC,USA,October,2013.                          [331]   NING Z X,LI C G ,YU D R. Development of a Hall effect
              [322]   MICHAUX E,MAZOUFFRE S,FRITZSCHE R. Spatial     hollow cathode thruster[C]//36th International Electric Pro-
                  and temporal evolution of ion and electron parameters in  pulsion Conference,Vienna,Austria,September,2019.
                  the plasma jet of a 30 W VAT[C]//37th International Elec-  [332]   LIU C G,NING Z X,ZHU X M. Design of magnetically
                  tric Propulsion Conference,Boston,Massachusetts,June,  enhanced hollow cathode micro-thruster:Concept and expe-
                  2022.                                              rimental research[J]. Acta Astronautica,2023,207:257−264.
                                                                [333]   AGEYEV V P ,OSTROVSKY V G. High-current station-
              [323]   AHEIEVA K,TOYODA K,CHO M,et al. Vacuum arc
                                                                     ary plasma accelerator of high power[C]//23rd International
                  thruster development and testing for micro and nanosatel-
                  lites[C]//34th International Electric Propulsion Conference,  Electric  Propulsion  Conference, Seattle, WA, USA, Sep-
                                                                     tember,1993.
                  Kobe,Japan,July,2015.
              [324]   田恺,吴益善,张兴民,等. LVAT-1 研制及在轨验证        [J].  [334]   CASSADY L D,KODYS A D,CHOUEIRI E Y. A thrust
                                                                     stand  for  high-power  steady-state  plasma  thrusters[C]//
                  真空与低温,2020,26(4):259−264.
                                                                     Modeling and Simulation Conference ,Monterey,Califor-
              [325]   ZHANG Y,WU J J. A novel laser ablation magnetoplas-
                                                                     nia,5-8 August ,2002.
                  madynamic thruster[C]//36th International Electric Propul-
                                                                [335]   KODYS A D,EMSELLEM G,CASSAY L D,et al. Lithi-
                  sion Conference,Vienna,Austria,September,2019.
                                                                     um mass flow control for high power Lorentz Force Accele-
              [326]   ZOLOTUKHIN D B,DANIELSAN K P,KEIDAR D M.
                                                                     rators[J]. AIP Conference proceedings,2001,552:908−915.
                  Micro-cathode  arc  thruster  improvement  by  the  second
                                                                [336]   ANGUS A. Critical review of the scientific and economic
                  MPD stage[C]//36th International Electric Propulsion Con-
                                                                     efficacy of lithium Lorentz Force Accelerators[J/OL]. arX-
                  ference,Vienna,Austria,September,2019.
                                                                     iv, 2020: 00705[2025-05-13].  https://arxiv.org/abs/2003.
              [327]   ZOLOTUKHIN  D  B.  A  two-stage  μCAT-MPD  thruster:
                                                                     00705.
                  toward  millinewton  thrust[C]//37th  International  Electric
                  Propulsion Conference,Boston,Massachusetts,June,2022.                (责任编辑:杨建斌)















              引文信息:张天平,陈娟娟,张雪儿. 空间电推进技术概览:演化电推进(下)[J]. 真空与低温,2026,32(1):108−119.
                      ZHANG T P,CHEN J J,ZHANG X E. An overview of electric propulsion technology in space:Evolutional electric propul-
                      sion(Ⅱ)[J]. Vacuum and Cryogenics,2026,32(1):108−119.
   117   118   119   120   121   122   123   124   125   126