DOUBLE STAGE HALL EFFECT THRUSTER DEVELOPMENT ACTIVITIES AT SNECMA MOTEURS

机译：SNECMA MOTEURS的双阶段大厅影响着推力器的开发活动

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To prepare the development of future versatile thrusters Snecma Moteurs is currently involved in technological research activities on Double Stage Hall Effect Thruster. This concept is based on the separation of the two main functions in Hall effect thrusters : ionisation is performed in the first stage while acceleration is achieved in a second stage. rnFirst promising results obtained with different prototypes DSHET using magnetic ionisation stage are presented as well as the design of a 3kW prototype intended to consolidate the concept and confirm these promising characteristics in cryogenic vacuum conditions.

机译：为了准备未来多功能推进器的开发，斯奈克玛公司目前正在参与双级霍尔效应推进器的技术研究活动。该概念基于霍尔效应推进器中两个主要功能的分离：在第一阶段执行电离，而在第二阶段实现加速。 rn提出了使用磁性电离级在不同原型DSHET上获得的首个有希望的结果，以及旨在巩固这一概念并确认在低温真空条件下这些有希望的特性的3kW原型的设计。

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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
M. Prioul; P. Dumazert; Bugrova A.I; Morozov A.I; Harchevnikov V.K; Desyatscov A.V; Kozintceva M.V; Saveleiev V.V; L.Jolivet; E. Gengembre; E. Chesta; J.P. Boeuf; C. Boniface; R. Rigollet; M. Saverdi; F. Castro; H. Simpson;
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Snecma Moteurs, DPES Site de Villaroche Nord – BP93F -77552 Moissy-Cramayel cedex F);

Snecma Moteurs, DPES Site de Villaroche Nord – BP93F -77552 Moissy-Cramayel cedex F);

Moscow Institute of Radioengennering, Electronics and Automation (MIREA), Moscow, Russia 129110;

Kurchatov’s Russia Research Center, Moscow, Russia 123098;

Moscow Institute of Radioengennering, Electronics and Automation (MIREA), Moscow, Russia 129110;

Moscow Institute of Radioengennering, Electronics and Automation (MIREA), Moscow, Russia 129110;

Moscow Institute of Radioengennering, Electronics and Automation (MIREA), Moscow, Russia 129110;

Moscow Institute of Radioengennering, Electronics and Automation (MIREA), Moscow, Russia 129110;

CNES, 18 avenue Edouard Belin, 31401 Toulouse Cedex 4, France;

European Space Agency;

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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. Experimental characterization of ID-Hall, a double stage Hall thruster with an inductive ionization stage [J] . Ortega A. Martin, Guglielmi A., Gaboriau F., Mathematical research letters: MRL . 2020,第2期

机译：ID-Hall的实验表征，一个具有归纳电离阶段的双级霍尔推进器
2. ID-HALL a new double stage Hall thruster design. I. Principle and hybrid model of ID-HALL [J] . Dubois L., Gaboriau F., Liard L., Physics of plasmas . 2018,第9期

机译：ID-Hall一个新的双级大厅推进器设计。 I. ID-Hall的原则和混合模型
3. The influence of magnetic field strength in ionization stage on ion transport between two stages of a double stage Hall thruster [J] . Yu D., Song M., Li H., Physics of plasmas . 2012,第11期

机译：电离级磁场强度对双级霍尔推力器两级之间离子迁移的影响
4. DOUBLE STAGE HALL EFFECT THRUSTER DEVELOPMENT ACTIVITIES AT SNECMA MOTEURS [C] . M. Prioul, P. Dumazert, Bugrova A.I, International spacecraft propulsion conference . 2004

机译：双级霍尔效应Snecma Moteurs的推动力发展活动
5. The development and characterization of a two-stage hybrid Hall/ion thruster. [D] . Peterson, Peter Young. 2004

机译：两阶段混合式霍尔/离子推进器的开发和特性。
6. Modeling and Experimental Testing of an Unmanned Surface Vehicle with Rudderless Double Thrusters [O] . Chunyue Li, Jiajia Jiang, Fajie Duan, 2019

机译：无舵双推力无人机的建模与试验测试
7. Experimental characterization of ID-Hall, a double stage Hall thruster with an inductive ionization stage [O] . A. Martín Ortega, A. Guglielmi, F. Gaboriau, 2020

机译：ID-HALL的实验表征，具有感应电离阶段的双级霍尔推进器
8. Overview of Iodine Propellant Hall Thruster Development Activities at NASA Glenn Research Center. [R] . Kamhawi, H., Haag, T., Szabo, J., 2016

机译：美国宇航局格伦研究中心的碘推进剂推进器发展活动概述。

DOUBLE STAGE HALL EFFECT THRUSTER DEVELOPMENT ACTIVITIES AT SNECMA MOTEURS

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