PDF(7498 KB)
Simulation Researches on the Pulsed Plasma Thruster with Tongue-Shaped and Flared Electrodes
- CHENG Xiaoyan, LIU Xiangyang, HUANG Qitao, WU Zhiwen, XIE Kan, WANG Ningfei
Author information
+
School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,China
Show less
History
+
Received |
Revised |
14 Mar 2017 |
15 May 2017 |
Issue Date |
|
20 May 2022 |
|
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
This is a preview of subscription content, contact
us for subscripton.
References
[1] 杨福全,赵以德,李娟,等. 主带小行星采样返回任务中的离子电推进应用方案[J]. 深空探测学报,2015,2(2):168-173
Yang F Q,Zhao Y D,Li J,et al. Application scheme of ion electric propulsion system for main-belt asteroid sample and return mission[J]. Journal of Deep Space Exploration,2015,2(2):168-173
[2] 牛禄,王宏伟,杨威. 用于微小卫星推进装置的脉冲等离子体推力器[J]. 上海航天,2004,21(5):39-43
Niu L,Wang H W,Yang W. The pulsed plasma thruster for propeller in small and micro satellite[J]. Aerospace Shanghai,2004,21(5):39-43
[3] 杨磊,刘向阳,陈成权,等. 脉冲等离子体推力器宏观特性数值研究[J]. 推进技术,2011,32(6):776-780
Yang L,Liu X Y,Chen C Q,et al. Numerical analysis on macro-characteristics of pulsed plasma thruster[J]. Journal of Propulsion Technology,2011,32(6):776-780
[4] Vondra R J,Thomassen K I. Performance improvements in solid fuel microthrusters[J]. Journal of Spacecraft,1972,9(10):738-742
[5] 郑茂繁,耿海,梁凯,等. 用于小行星探测的离子推力器技术研究[J]. 深空探测学报,2015,2(3):236-240
Zheng M F,Geng H,Liang K,et al. Research on ion thruster technology for asteroid exploration[J]. Journal of Deep Space Exploration,2015,2(3):236-240
[6] 杨乐. 脉冲等离子体推力器工作过程理论和实验研究[D].长沙:国防科学技术大学,2007.
Yang L. Theoretical analysis and experiment investigation of pulsed plasma thruster [D].Changsha:National University of Defense Technology,2007.
[7] Solbes A,Thomassen K,Vondra R. Analysis of solid teflon pulsed plasma thruster[J]. Journal of Spacecraft & Rockets,2013,7(7):1402-1406
[8] Schonherr T,Komurasaki K,Kawashima R. Effect of capacitance on discharge behavior of pulsed plasma thruster[J]. Journal of IAPS,2010,18(1):23-28
[9] Kamhawi H,Arrington L,Pencil E,et al. Performance evaluation of a high energy pulsed plasma thruster[C]//AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. USA:AIAA,2005.
[10] Liu X,Zuo G,Herdrich G,et al. Numerical simulation of ADD SIMP-LEX pulsed plasma thruster based on a modified electromechanical model[C]//Space Propulsion. Rome:[s.n],2016.
[11] Sch?nherr T,Nawaz A,Herdrich G,et al. Influence of electrode shape on performance of pulsed magneto plasma dynamic thruster SIMP-LEX [J]. Journal of Propulsion & Power,2009,25(2):380-386
[12] Nawaz A,Albertoni R,Auweter-Kurtz M. Thrust efficiency optimization of the pulsed plasma thruster SIMP-LEX[J]. Acta Astronautica,2010,67(3):440-448
[13] Lau M,Grabe M,Herdrich G. Experimental characterization of a scalable pulsed magneto plasma dynamic propulsion system[C]//Space Propulsion. Germany:[s.n],2014.
[14] Krejci D,Scharlemann C. Analytic model for the assessment of the electrode configuration of a μPPT[C]//45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Colorado:AIAA,2009.
[15] 张华,吴建军,何振,等. 极板构型对脉冲等离子体推力器性能影响[J]. 国防科技大学学报,2014(4):5-9
Zhang H,Wu J J,He Z,et al. Effects of electrodes configuration on the performance of pulsed plasma thrusters[J]. Journal of National University of Defense Technology,2014(4):5-9