参考文献
[1]POLZINK A. Comprehensive review of planar pulsed inductive plasma thruster research and technology[J]. Journal of Propulsion and Power, 2011, 27(3): 513531.
[2]DAILEYC L, LOVBERG R H. The PIT MkV pulsed inductive thruster[D]. NASACR191155, 1993.
[3]FRISBEER H. Evaluation of highpower solar electric propulsion using advanced ion, hall, MPD, and PIT thrusters for Lunar and Mars cargo missions[C]//The 42nd IAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Sacramento. California: AIAA, 20064465.
[4]DAILEYC L. Thrust MEASUREMENT for a pulsed inductive thrusters[D]. AD702498, 1970.
[5]LOVBERGR H, DAILEY C L. Current sheet development in a pulsed inductive thruster[C]//The 25th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Monterey, CA: AIAA, 1989.
[6]RUSSELLD, POYLIO J H, GOLDSTEIN W, et al. The mark Ⅵ pulsed inductive thruster[C]//Space Conference and Exhibit. San Diego, California: AIAA20046054, 2004.
[7]ROBERTH F, MIKELLIDES P G. The nuclearelectric pulsed inductive thruster (NuPIT):mission analysis for prometheus[C]//41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit .Tucson, Arizona: AIAA, 2005.
[8]POLZINK A. Faraday accelerator with radiofrequency assisted discharge (FARAD)[D]. New Jersey: Princeton University, 2006.
[9]POLZINK A, CHOUEIRI E Y. Performance optimization criteia for pulsed inductive plasma acceleration[J].IEEE Transactions on Plasma Science, 2006, 34(3): 945953.
[10]POLZINK A, SANKARA K . Inductive pulsed plasma thruster model with time evolution of energy and state properties[D]. NASA Report, Document ID,20130001785, 2012.
[11]POLZIN K A, MARTIN R H, ESKRID G E, et al. Summary of the 2012 inductive pulsed plasma thruster development and testing program[D]. Marshall Space Flight Center. Huntsville, Alabama: NASA/TP 2013 217488, 2013.
[12]WESSEL F J, Bolte N, Kiyashko V, et al. Pulsedinductive thruster[D]. Tri Alpha Energy Inc. Rancho Santa Margarita, CA: 2013.
[13]KOELFGENS J, HAWK C W. A plasmoid thruster for space propulsion[C]//The 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit. Huntsville, Alabama: AIAA, 20033671, 2003.
[14]JEREMYH C,IVANA H. preliminary design and analysis of the purdue university pulsed inductive thruster or PuPIT[C]//The 42nd AIAA/SAE/ASME/ASEE Joint Propulsion Conference. Sacramento, California: AIAA 20064854, 2006.
[15]SLOUGHJ, VOTROUBEK G. Magnetically accelerated plasmoid (MAP) propulsion[C]//The 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Sacramento, CA: AIAA20064654, 2006.
[16]LOVBERGR H, DAILEY C L. Plasma current sheet development in a clamped discharge thruster[D]. ADA204633, 1988.
[17]POYLIOJ H, RUSSELL D, GOLDSTEIN W, et al. pulsed inductive thruster: flightscale proof of concept demonstrator[C]//The 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Fort Lauderdale, Florida: AIAA20043640, 2004.
[18]POLZINK A, ROSE M F, MILLER R, et al. Design of a lowenergy FARAD thruster[C]//The 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Cincinnati, OH: AIAA20075257, 2007.
[19]POLZINK A, ROSE M. F, MILLER R. Laboratorymodel integratedsystem FARAD thruster[C]//The 44th AIAA/SAE/ASME/ASEE Joint Propulsion Conference. Hartford, CT: AIAA 20084821, 2008.
[20]HALLOCKA K, POLZIN K A. Effect of inductive coil geometry on the operating characteristics of a pulsed inductive plasma accelerator[C]//Space Propulsion, Bordeaux, France: SP20122394010, 2012.
[21]MIKELLIDESP G. Numerical simulations of the pulsed inductive thruster[C]//The 38thAIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Indianapolis, Indiana: AIAA 20023807, 2002.
[22]MIKELLIDESP G, NEILLY C. Pulsed inductive thruster, Part 1: modeling, validation and performance analysis[C]//The 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference&Exhibit. Fort Lauderdale, Florida: AIAA 20044091, 2004.
[23]ALLISOND L, MIKELLIDES P G. Pulsed inductive thruster, Part 2: twotemperature thermochemical model for ammonia[C]//The 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Fort Lauderdale, Florida, AIAA 20044092,2004.
[24]MIKELLIDESP G, VILLARREAL J K. High energy pulsed inductive thruster modeling operating with ammonia propellant[C]//The 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH: AIAA 20075285, 2007.
[25]MIKELLIDESP G, VILLARREAL J K. numerical modeling of a low energy pulsed inductive thruster[C]//The 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Hartford, CT: AIAA 20084726, 2008.
[26]VILLARREALJ K. numerical modeling of a high efficiency low energy pulsed inductive thruster for space application[C]//The 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Orlando, Florida, AIAA 2009201,2009 .
[27]成玉国. 感应式等离子体推力器中螺旋波放电与电磁加速数值研究[D]. 长沙:国防科学技术大学研究生院,2015.
[28]GOODMAN M, KAZEMINEZHAD F, OWENS T. Pulsed plasma accelerator modeling[D]. The Institute for Scientific Research, Inc. Fairmont, WV: NASA/CR2009215635, 2009.
[29]车碧轩. 感应式脉冲等离子体推力器感应线圈设计研究[D]. 长沙:国防科学技术大学研究生院, 2015. |