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[1]陈琳英,宋仁旺.离子火箭发动机羽流特性分析[J].火箭推进,2010,36(04):7-11.
 Chen Linying,Song Renwang.Analysis on plume characteristics of ion thrusters[J].Journal of Rocket Propulsion,2010,36(04):7-11.
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离子火箭发动机羽流特性分析

参考文献/References:

[1]Robie I Samanta Roy, Daniel E Hastings. Particle-in-Cell and Monte Carlo Modelling of Advanced Plasma Thrusters, AFOSR-TR-9 5[R]. AFOSR/NA, 110 Duncan Ave., Suite B115. Bolling AFB, DC, 1995. [2]Wang J Brophy. 3-D Monte-Carlo Particle-in-Cell Simulations of Ion Thruster Plasma Interactions[R]. AlAA 95-2826. [3]Michael R Nakles. Experimental and Modeling Studies of Low-Energy Ion Sputtering for Ion Thrusters [D] . Blacksburg, Virginia: Virginia Polytechnic Institute and State University, July 8, 2004. [4]John R Brophy, Ira Katz, James E Polk. Numerical Simulations of Ion Thruster Accelerator Grid Erosion [R]. AIAA2002-4261. [5]Cody C Farnell, John D Williams, Paul J Wilbur. Numerical Simulation of Ion Thruster Optics[C]. 28th International Electric Propulsion Conference. Toulouse, France, CR-2003-212305.

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备注/Memo

收稿日期:2010-03-13;修回日期:2010-06-17。基金项目:高等学校博士学科点专项科研基金(批准号:20082001 )资助课题。作者简介: 陈琳英(1976—),女,博士,研究领域为空间电推进技术。
基金项目:高等学校博士学科点专项科研基金(批准号:20082001 )资助课题。作者简介: 陈琳英(1976—),女,博士,研究领域为空间电推进技术。
作者简介: 陈琳英(1976—),女,博士,研究领域为空间电推进技术。

更新日期/Last Update: 1900-01-01