Preliminary results of a high frequency pulsed plasma thruster

• 1. 用于借助高频激励脉冲产生等离子脉冲或激光脉冲的方法和设备、尤其气体放电激光器、以及用于高频激励脉冲发生器的控制单元 [P] . 中国专利： CN108141949A . 2018-06-08
• 2. 高频激励脉冲产生等离子或激光脉冲方法设备和控制单元 [P] . 中国专利： CN108141949B . 2019.11.12
• 3. Method for controlling an AC plasma display panel having a positive preliminary discharge pulse and a negative preliminary discharge pulse [P] . 韩国专利： KR19980025153A . 1998-07-06

  机译： 控制具有正的预放电脉冲和负的预放电脉冲的AC等离子体显示面板的方法

• 4. PULSE PLASMA THRUSTER AND SPACECRAFT USING THIS THRUSTER [P] . 日本专利： JP2007120343A . 2007-05-17

  机译： 脉冲等离子推进器和使用该推进器的航天飞机

• 5. Preliminary pulse generation circuit - is for each pulse of pulse train whose repetition frequency is only constant approximately [P] . 德国专利： DE2519722A1 . 1976-11-11

  机译： 初步的脉冲生成电路-用于脉冲序列的每个脉冲，其重复频率仅近似恒定

• 1. Investigation on plasma characteristics in a laser ablation pulsed plasma thruster by optical emission spectroscopy [J] . Yu ZHANG, Jianjun WU, Yang OU, 等离子体科学和技术（英文版） . 2020,第004期
• 2. Experimental investigation on the evolution of plasma properties in the discharge channel of a pulsed plasma thruster [J] . Yang ZHOU, Ninafei WANG, Xiangyang LIU, 等离子体科学和技术（英文版） . 2020,第006期
• 3. Experimental investigation on the plasma morphology of ablative pulsed plasma thruster with tongue-shaped and flared electrodes [J] . Jianjun WU, Yu ZHANG, Yang OU, 等离子体科学和技术（英文版） . 2020,第009期
• 4. PIC simulation of plasma properties in the discharge channel of a pulsed plasma thruster with flared electrodes [J] . Qi LIU, Lei YANG, Yuping HUANG, 等离子体科学和技术（英文版） . 2019,第007期
• 5. Study on the plasma generation characteristics of an induction-triggered coaxial pulsed plasma thruster [J] . Weisheng CUI, Wenzheng LIU, Jia TIAN, 等离子体科学和技术（英文版） . 2018,第002期
• 6. Preliminary Results of a High Frequency Pulsed Plasma Thruster [C] . R. Marques, S. Gabriel, F. Costa AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2007
• 7. Innovations in Pulsed Plasma Thrusters to Enable CubeSat Science Missions [D] . Northway, Paige. 2020
• 8. Demonstrating a new technology for space debris removal using a bi-directional plasma thruster [O] . Kazunori Takahashi, Christine Charles, Rod W. Boswell, -1
• 9. The plasma morphology of an asymmetric electrode ablative pulsed plasma thruster [O] . Zhe Zhang, William Yeong Liang Ling, Junxue Ren, 2019

• 1. 稳态等离子推进器在超高频波段的电磁辐射特性 [C] . 于达仁 ,武志文 ,毛威 . 中国宇航学会深空探测技术专业委员会第一届学术会议 . 2005
• 2. 脉冲等离子体推进器脉冲电源及推进剂烧蚀特性的实验研究和数值分析 [A] . 邓健 . 2013