Research Status and Key Technology of Electrically Controlled Solid Thruster

被引:0
作者
Xia G.-Q. [1 ,2 ,3 ,4 ]
Guan S.-W. [1 ,2 ]
Lu C. [1 ,2 ,3 ]
Guo F.-N. [1 ,2 ]
Wang X.-G. [3 ,4 ]
Kang H.-F. [3 ,4 ]
机构
[1] State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian
[2] Key Laboratory of Advanced Technology for Aerospace Vehicles of Liaoning Province, Dalian University of Technology, Dalian
[3] Collaborative Innovation Center of Micro and Nano Satellites of Hebei Province, Langfang
[4] Key Laboratory of Micro Spacecraft Technology of Hebei Province, Langfang
来源
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 10期
关键词
Key technology; Review; Solid propellant; Status; Thrust controllable; Thruster;
D O I
10.13675/j.cnki.tjjs.2207050
中图分类号
学科分类号
摘要
The electronically controlled solid thruster has a unique electric control capability and satisfies the technical requirements such as restartable,controllable thrust and simple structure,which has been attracting the attention of domestic and foreign research institutions. Propellant development,working mechanism exploration,thruster structure design and engineering applications are the hot spots of current research. The relevant research progress of electronically controlled solid thrusters have been summarized. The problems of grain structure failure,propellant self-sustaining combustion and the difficulty of controlled combustion in large size grains were identified as the main problems limiting their application and development. The key technologies of electronically controlled solid thruster are summarized and sorted out from four aspects:propellant formulation,propellant preparation,ignition electrode design and thrust control,the research suggestions are put forward,and the development trend is looked forward with the working characteristics and application background of this thruster. © 2023 Journal of Propulsion Technology. All rights reserved.
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共 65 条
  • [51] Nicholas A,Sawka W,Finne T,et al. SpinSat Mission Preliminary Results[C], Hawaii:Advanced Maui Optical and Space Surveillance Technologies Conference, (2014)
  • [52] Nicholas A,Finne T,Galysh I,et al. SpinSat Mission Overview[C], Logan:27th Annual AIAA/USU Conference on Small Satellites, (2013)
  • [53] Glascock M S, Et al., Observation of Late-Time Ablation in Electric Solid Propellant Pulsed Microthrusters[C], Salt Lake City:52nd AIAA/SAE/ASEE Joint Propulsion Conference, (2016)
  • [54] Glascock M S,, Rovey J L,, Williams S,, Et al., Plume Characterization of Electric Solid Propellant Pulsed Microthrusters [J], Journal of Propulsion and Power, 33, 4, pp. 870-880, (2017)
  • [55] Glascock M S, Rovey J L., Ablation Mass Loss of an Electric Solid Propellant in a Pulsed Plasma Thruster[C], Atlanta:The 35th International Electric Propulsion Conference, (2017)
  • [56] Glascock M S,, Drew P D,, Rovey J L,, Et al., Thermodynamic Properties of Hydroxylammonium Nitrate-Based Electric Solid Propellant Plasma[J], Journal of Thermophysics and Heat Transfer, 34, 3, pp. 522-529, (2020)
  • [57] Glascock M S,, Rovey J,, Polzin K A., Impulse Measurements of Electric Solid Propellant in an Electrothermal Ablation-Fed Pulsed Plasma Thruster[C], Indianapolis:AIAA Propulsion and Energy 2019 Forum, (2019)
  • [58] 44, 2, pp. 188-206
  • [59] Rovey J L,, Lyne C T,, Mundahl A J,, Et al., Review of Multimode Space Propulsion[J], Progress in Aerospace Sciences, 118, (2020)
  • [60] 28, 12, pp. 1190-1199