霍尔推力器热模型研究
[1] 张天平.国外离子和霍尔电推进技术最新进展[J].真空与低温, 2006, 12(4):187-190.(Zhang Tianping. Recent international progress in ion and Hall electric propulsions. Vacuum and Cryogenics, 2006, 12(4):187-190)
[2] Filliben J D. Electric thruster systems-technical report[R]. AD-A327009, 1997.
[3] John T Y. Computational modeling of Hall thruster channel wall erosion[D]. Michigan: The University of Michigan, 2008:23-24.
[4] Goebel D M, Katz I. Fundamentals of Electric Propulsion: Ion and Hall thrusters[M]. New Jersey: Wiley, 2008:340-351.
[5] Roche S, Barra S, Bechu S. Thermal analysis of a stationary plasma thruster[R]. AIAA 99-2296, 1992.
[6] Archipov B, Krochak L Z, Maslennikov N Y. Thermal design of the electric propulsion system components[R]. AIAA98-3489, 1998.
[7] Yan Li, Wang Pingyang. Analysis of coupled thermal Hall thruster[C]//Proc of CEPC. 2013, 9:218-221.
[8] Brophy J R, Barnett J W, Sankovic J M. Performance of the stationary plasma thruster: SPT-100[R]. AIAA92-3155, 1992.
[9] Kim V. Main physical features and processes determining the performance of stationary plasma thruster[J]. Journal of Propulsion and Power, 1998, 32(14):5736-5743.
[10] Barral S, Makowski K. Wall material effects in stationary plasma thrusters[J]. Physics of Plasmas, 2003, 10(10):4137-4152.
[11] Hobbs G D, Wesson J A. Heat flow through a Langmuir sheath in the presence of electron emission[J]. Plasma Physics, 1967, 9(7):85-87.
[12] Barano V, Nazarenko Y, Petrosov V. The wear of the channel walls in Hall thruster[R]. IEPC-2001-005, 2001.
[15] 孙明明,张天平,陈娟娟,等.LIPS-200离子推力器热特性模拟分析研究[J].强激光与粒子束, 2014, 26:084002.(Sun Mingming, Zhang Tianping, Chen Juanjuan, et al. Thermal analysis of LIPS-200 ion thruster. High Power Laser and Particle Beams, 2014, 26:084002)
龙建飞, 孙明明, 张天平, 吴先明. 霍尔推力器热模型研究[J]. 强激光与粒子束, 2014, 26(12): 124002. Long Jianfei, Sun Mingming, Zhang Tianping, Wu Xianming. Thermal model of Hall thruster[J]. High Power Laser and Particle Beams, 2014, 26(12): 124002.