PULSED PLASMA THRUSTERS FOR PRIMARY PROPULSION AND ATTITUDE CONTROL OF A SMALL ALL ELECTRICAL SATELLITE

机译：脉冲等离子推进器用于小功率卫星的初步推进和姿态控制

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A small all electrical satellite is planned for a lunar mission scheduled for launch 2008 by the Institute for Space Systems at the University of Stuttgart. Due to its inherent characteristics a Pulsed Plasma Thruster was chosen for propelling the spacecraft. First steps were taken towards building and dimensioning this thruster. In this paper, a summary of the requirements towards the thruster system is given. A design for a modular testing approach is introduced, with which the optimal configuration for the pulsed plasma thruster can be determined. This modular thruster will be installed within the newly established vacuum tank. With this setup different parameters of the thruster will be analyzed. Further, the individual components of the thruster, such as propellant, electrodes, capacitor and igniter, are examined and criteria for evaluation discussed. rnA short description of the physics used for simulation of the thruster dynamics is given.

机译：斯图加特大学空间系统研究所计划在2008年发射一次小型全电子卫星进行登月任务。由于其固有的特性，选择了脉冲等离子推进器来推动航天器。迈出了构建和确定推进器尺寸的第一步。本文总结了对推进器系统的要求。介绍了一种模块化测试方法的设计，通过该设计，可以确定脉冲等离子推进器的最佳配置。该模块化推进器将安装在新建立的真空罐内。通过这种设置，将分析推进器的不同参数。此外，还检查了推进器的各个组成部分，例如推进剂，电极，电容器和点火器，并讨论了评估标准。 rn给出了用于模拟推进器动力学的物理学的简短描述。

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来源
《4th International spacecraft propulsion conference》|2004年|p.1-6|共6页
会议地点 Sardinia(IT)
作者
Anuscheh Nawaz; Monika Auweter-Kurtz; Helmut Kurtz; Henri P. Wagner;
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作者单位

Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany nawaz@irs.uni-stuttgart.de;

Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany nawaz@irs.uni-stuttgart.de;

Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany nawaz@irs.uni-stuttgart.de;

Institut für Raumfahrtsysteme (IRS), Universität Stuttgart, Pfaffenwaldring 31, 70550 Stuttgart, Germany nawaz@irs.uni-stuttgart.de;

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正文语种 eng
中图分类推进系统（发动机、推进器）;
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专利

1. Plasma impulse based peening and decoating of engine parts and pulsed plasma thrusters for small spacecraft propulsion [J] . Wagner HP, Auweter-Kurtz M Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology . 2004,第3a4期

机译：基于等离子脉冲的发动机零件和脉冲等离子推进器的喷丸和脱漆，用于小型航天器推进
2. Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems [J] . A. V. Bogatyi, R. V. El’nikov, I. P. Nazarenko, Russian Aeronautics . 2018,第3期

机译：作为小型航天器推进系统的一部分，先进的脉冲等离子体推进器及其应用
3. Results of the qualification test campaign of a Pulsed Plasma Thruster for Cubesat Propulsion (PPTCUP) [J] . Ciaralli S., Coletti M., Gabriel S. B. Acta astronautica . 2016,第ApraaMay期

机译：立方等离子体推进器脉冲等离子推进器（PPTCUP）资格测试活动的结果
4. PULSED PLASMA THRUSTERS FOR PRIMARY PROPULSION AND ATTITUDE CONTROL OF A SMALL ALL ELECTRICAL SATELLITE [C] . Anuscheh Nawaz, Monika Auweter-Kurtz, Helmut Kurtz, International spacecraft propulsion conference . 2004

机译：脉冲等离子体推动器，用于小型所有电气卫星的主要推进和姿态控制
5. Dynamic neural network-based Pulsed Plasma Thruster (PPT) fault detection and isolation for the Attitude Control Subsystem of formation flying satellites. [D] . Valdes, Arturo. 2008

机译：基于动态神经网络的脉冲等离子推进器（PPT）故障检测和隔离，用于编队飞行卫星的姿态控制子系统。
6. MHz-Order Surface Acoustic Wave Thruster for Underwater Silent Propulsion [O] . Naiqing Zhang, Yue Wen, James Friend 2020

机译：用于水下静音推进的MHz级表面声波推进器
7. Dynamic neural network-based pulsed plasma thruster (PPT) fault detection and isolation for the attitude control subsystem of formation flying satellites [O] . Valdes Arturo 2008

机译：基于动态神经网络的脉冲等离子体推进器（PPT）故障检测与隔离，用于编队飞行卫星姿态控制子系统
8. High Efficiency Pulsed Plasma Thruster for Satellite Attitude Control and Maneuver [R] . Petr, R. , Jacob, J. , Choudhary, P. 2003

机译：用于卫星姿态控制和机动的高效脉冲等离子推力器

PULSED PLASMA THRUSTERS FOR PRIMARY PROPULSION AND ATTITUDE CONTROL OF A SMALL ALL ELECTRICAL SATELLITE

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