DEVELOPMENT OF A PROTOTYPE THRUST STEERING DEVICE FOR HALL-EFFECT THRUSTERS

机译：霍尔效应推力器原型推力转向装置的开发

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摘要

An overview of on-going development activities for a thrust steering device (TSD) applicable to Hall thrusters is presented. The work includes a review of the relevant functional requirements as well as of the applicable concepts. The preferred concept involves a combination of both magnetic steering and local, unsymmetrical propellant injection. The preliminary design is presented, and the results of 2D performance as well as 3D plume modeling for such a device are shown. The results indicate that a theoretical steering capability of up to 11° may be reached with the present design. A prototype is to be built and tested.

机译：概述了适用于霍尔推进器的推力转向装置（TSD）正在进行的开发活动。这项工作包括对相关功能要求以及适用概念的审查。首选概念涉及电磁转向和局部非对称推进剂喷射的结合。介绍了初步设计，并显示了此类设备的2D性能和3D羽流建模结果。结果表明，本设计可以达到11°的理论转向能力。将建立原型并进行测试。

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来源
《4th International spacecraft propulsion conference》|2004年|p.1-7|共7页
会议地点 Sardinia(IT)
作者
O. Duchemin; M. Prioul; H. Illand; S. Banetta; A. Vicini; L. Garrigues; R. Rigollet; D. Estublier;
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作者单位

Snecma Moteurs, Space Propulsion Division, Site de Villaroche Nord – BP 93 77552 Moissy-Cramayel Cedex, France;

contact: olivier.duchemin@snecma.fr;

Snecma Moteurs, Space Propulsion Division, Site de Villaroche Nord – BP 93 77552 Moissy-Cramayel Cedex, France;

Snecma Moteurs, Space Propulsion Division, Site de Villaroche Nord – BP 93 77552 Moissy-Cramayel Cedex, France;

Alta S.p.A., Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy;

Alta S.p.A., Via Gherardesca 5, 56121 Ospedaletto, Pisa, Italy;

CNRS / CPAT, Université Paul Sabatier, bât. 3R2, 118 route de Narbonne, 31062 Toulouse, France;

EADS Astrium SAS, 31 rue des Cosmonautes, 31402 Toulouse Cedex 4, France;

ESA / ESTEC, Keplerlaan 1, Postbus 299, 2200 AG Noordwijk, The Netherlands;

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原文格式 PDF
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. Effects of channel wall material on thrust performance and plasma characteristics of Hall-effect thrusters [J] . Tahara H, Imanaka K, Yuge S Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology . 2006,第11a12期

机译：通道壁材料对霍尔效应推进器推力性能和等离子体特性的影响
2. Thrust performance and plasma features of low-power Hall-effect thrusters [J] . Tahara H., Goto D., Yasui T., Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology . 2002,第3a4期

机译：小功率霍尔效应推进器的推力性能和等离子特性
3. Demonstrating a magnetic steering of the thrust imparted by the magnetic nozzle radiofrequency plasma thruster [J] . Ryoji Imai, Kazunori Takahashi Applied Physics Letters . 2021,第26期

机译：通过磁力喷嘴射频等离子体推进器赋予推动推力的磁力转向
4. DEVELOPMENT OF A PROTOTYPE THRUST STEERING DEVICE FOR HALL-EFFECT THRUSTERS [C] . O. Duchemin, M. Prioul, H. Illand, International spacecraft propulsion conference . 2004

机译：开发霍尔效应推进器的原型推力转向装置
5. Development of an Annular Micro-Hall-effect Thruster and Halbach Permanent Magnet Arrays in Hall-effect Thrusters [D] . Warren, Matthew Lamar 2018

机译：环形微霍尔效应推力器和霍尔效应推力器中的Halbach永磁体阵列的开发
6. Design and Development of a Prototype Electrotherapy Device [O] . J. G. Rocha, V. M. G. Correia, M. S. Martins, 2013

机译：原型电疗仪的设计与开发
7. Diagnostic for Verifying the Thrust Vector Requirement of the AEPS Hall-Effect Thruster and Comparison to the NEXT-C Thrust Vector Diagnostic [O] . Gabriel F. Benavides, Jonathan Mackey, Drew Ahern, 2018

机译：诊断用于验证AEPS Hall效应推进器的推力矢量要求，并与下C推向载体诊断的比较

DEVELOPMENT OF A PROTOTYPE THRUST STEERING DEVICE FOR HALL-EFFECT THRUSTERS

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