磁等离子体动力推力器回顾和认识

Hai Bin Tang; Yi Bai Wang; Yan Ming Wei

doi:10.13675/j.cnki.tjjs.2018.11.001

磁等离子体动力推力器回顾和认识

Hai Bin Tang^*
, Yi Bai Wang
, Yan Ming Wei

^*此作品的通讯作者

宇航学院

CAS - Beijing Institute of Control Engineering

科研成果: 期刊稿件 › 文献综述 › 同行评审

8 引用（Scopus）

摘要

Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

投稿的翻译标题	Review and Understanding on Magnetoplasmadynamic Thrusters Technology
源语言	繁体中文
页（从-至）	2401-2414
页数	14
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	39
期	11
DOI	https://doi.org/10.13675/j.cnki.tjjs.2018.11.001
出版状态	已出版 - 1 11月 2018

关键词

Cathode erosion
Electrode structure
Magnetoplasmadynamic thruster
Onset
Power deposition
Propellant
Thrust mechanism

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10.13675/j.cnki.tjjs.2018.11.001

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引用此

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abstract = "Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.",

keywords = "Cathode erosion, Electrode structure, Magnetoplasmadynamic thruster, Onset, Power deposition, Propellant, Thrust mechanism",

author = "Tang, \{Hai Bin\} and Wang, \{Yi Bai\} and Wei, \{Yan Ming\}",

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T1 - 磁等离子体动力推力器回顾和认识

AU - Tang, Hai Bin

AU - Wang, Yi Bai

AU - Wei, Yan Ming

PY - 2018/11/1

Y1 - 2018/11/1

N2 - Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

AB - Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

KW - Cathode erosion

KW - Electrode structure

KW - Magnetoplasmadynamic thruster

KW - Onset

KW - Power deposition

KW - Propellant

KW - Thrust mechanism

UR - https://www.scopus.com/pages/publications/85059842964

U2 - 10.13675/j.cnki.tjjs.2018.11.001

DO - 10.13675/j.cnki.tjjs.2018.11.001

M3 - 文献综述

AN - SCOPUS:85059842964

SN - 1001-4055

VL - 39

SP - 2401

EP - 2414

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 11

ER -

磁等离子体动力推力器回顾和认识

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