Page 113 - 《真空与低温》2026年第2期
P. 113
232 真空与低温 第 32 卷 第 2 期
Conference,American Institute of Aeronautics and Astro- [371] CAVALL J N. Helicon plasma thrusters: Prototypes and
nautics,Nashville,Tennessee,9-12,January,2012. advances on modeling[C]//33rd International Electric Pro-
[362] PETERSON P Y,MASSEY D R. Performance and plume pulsion Conference, Washington, DC, USA, October,
characterization of a helicon hall thruster[C]//32nd Inter- 2013.
national Electric Propulsion Conference, Kurhaus, Wies- [372] PAVARIN D, FERRI F, MANENTE M, et al. Helicon
baden,Germany,September,2011. plasma hydrazine combined micro project overview and
[363] UCHIGASHIMA A,BABA T,ICHIHARA D,et al. De- development status[R]. SP2010-1842379, Space Propul-
velopment of helicon electrostatic thruster (HEST) [C]// sion,2010 .
34th International Electric Propulsion Conference, Kobe, [373] BATISHCHEV O, CAMBIER J. Experimental study of
Japan,July,2015. the mini-helicon thruster[R]. AFRL-RZ-ED-TR-2009-0020,
[364] ICHIHARA D, NAKAGAWA Y, IWAKAWA A, et al. Air Force Research Laboratory ,2009.
RF vs. acceleration power distribution in helicon electro- [374] BATISHCHEV O V. Minihelicon plasma thruster[J]. IEEE
static thruster[C]//35th International Electric Propulsion Transaction on Plasma Science,2009,37(8):1563−1571.
Conference,Atlanta,Georgia,October,2017. [375] TREZZOLANI F,MANENTE M,TOSON E,et al. Devel-
[365] BLACKHALL L. Helicon Magneto Plasma Dynamic opment and testing of a miniature helicon plasma thruster
(HMPD) thruster concept[C]//29th International Electric [C]//35th International Electric Propulsion Conference,At-
Propulsion Conference,Princeton,New Jersey,USA,Oc- lanta,Georgia,October,2017.
tober,2005. [376] RUIZ M,VELASCON A,GOMEZ V,et al. Results of the
[366] TAKAHAHSI K,KOMURO A ,ANDO A. Helicon mag- first Helicon Plasma Thruster (HPT) coupling test cam-
netoplasmadynamic plasma thruster for large thrust and paign within the HIPATIA project[C]//37th International
Electric Propulsion Conference, Boston, Massachusetts,
high specific impulse electric propulsion[C]//34th Interna-
tional Electric Propulsion Conference,Kobe,Japan,July, June,2022.
2015. [377] TAKAHASHI K. 5-kW class helicon plasma thruster per-
formance[C]//38th International Electric Propulsion Confe-
[367] FILLEUL F. Ion magnetization effects on plasma genera-
rence,Toulouse,France,June,2024.
tion in a magnetic nozzle RF device[C] //37th Internation-
al Electric Propulsion Conference,Boston,Massachusetts, [378] WINTER M ,KOCH H. Inertial electrostatic confinement
plasma devices-potential thruster technology for very accu-
June,2022.
rate attitude control systems[C]//35th International Electric
[368] MAGAROTTO M ,PAVARIN D. Numerical model of a
Propulsion Conference,Atlanta,Georgia,October,2017.
magnetically enhanced plasma thruster[C]//25th Interna-
tional Electric Propulsion Conference, Vienna, Austria, [379] WINTER M, KOCH H , GREEN R W. Direct inertial
electrostatic confinement propulsion at low power levels
September,2019.
[C]//25th International Electric Propulsion Conference,Vi-
[369] SOUHAIR N,PONTI F. Analysis of different numerical
enna,Austria,September,2019.
approaches for the simulation of a helicon plasma thrus-
[380] AUERBACH J, BILEN S G. Investigating beam diver-
ter[C]//37th International Electric Propulsion Conference,
gence and characteristics in a helical electrode inertial
Boston,Massachusetts,June,2022.
electrostatic confinement thruster[C]//38th International
[370] MA X,NISHIDA H. Numerical simulation of plasma flow
Electric Propulsion Conference, Toulouse, France, June,
field in RF plasma thruster with magnetic cusp[C]//37th
2024.
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:新型电推进(上)[J]. 真空与低温,2026,32(2):223−232.
ZHANG T P,CHEN J J,ZHANG X E. An overview of electric propulsion technology in space:new-type electric propul-
sion(ⅰ)[J]. Vacuum and Cryogenics,2026,32(2):223−232.

